is.800.2007.pdf from shubham and team to

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IS 800 (2007): General Construction In Steel - Code of
Practice [CED 7: Structural Engineering and structural
sections]

IS 800:2007
Indian Standard
GENERAL CONSTRUCTION IN
STEEL — CODE OF PRACTICE
( Third Revision)
ICS 77.140.01
0 BIS 2007
BUREAU OF INDIAN STANDARDS
MANAK BHAVAN, 9 BAHADUR SHAH ZAFAR MARG
NEW DELHI 110002
December 2007 Price Rs. 1130.!?!

Structural Engineering and Structural Sections Sectional Committee, CED 7
FOREWORD
This Indian Standard (Third Revision) was adopted by the Bureau of Indian Standards, after the draft finalized
by the Structural Engineering and Structural Sections Sectional Committee had been approved by the Civil
Engineering Division Council.
The steel economy programme was initiated by erstwhile Indian Standards Institution in the year 1950 with the
objective of achieving economy in the use of structural steel by establishing rational, efficient and optimum
standards for structural steel products and their use. IS 800: 1956 was the first in the series of Indian Standards
brought out under this programme. The standard was revised in 1962 and subsequently in 1984, incorporating
certain very importmt changes.
IS 800 is the basic Code for general construction in steel structures and is the prime document for any structural
design and has influence on many other codes governing the design of other special steel structures, such as
towers, bridges, silos, chimneys, etc. Realising the necessity to update the standard to the state of the art of the
steel construction technology and economy, the current revision of the standard was undertaken. Consideration
has been given tO the de~elopments taking place in the country and abroad, and necessary modifications and
additions have been incorporated to make the standard more useful.
The revised standard will enhance the confidence of designers, engineers, contractors, technical institutions,
professional bodies and the industry and will open a new era in safe and economic construction in steel.
In this revision the following major modifications have been effected:
a) In view of’the development and production of new varieties of medium and high tensile structural steels
in the country, the scope of the standard has been modified permitting the use of any variety of structural
steel provided the relevant provisions of the standard are satisfied.
b) The standard has made reference to the Indian Standards now available for rivets; bolts and other fasteners.
c) The standard is based on limit state method, reflecting the latest developments and the state of the art.
The revision of the standard was based on a review carried out and the proposals framed by Indian Institute of
Technology Madras (IIT Madras). The project was supported by Institute of Steel Development and Growth
(INSDAG) Kolkata. There has been considerable contribution from INSDAG and IIT Madras, with assistance
from a number of academic, research, design and contracting institutes/organizations, in the preparation of the
revised standard.
In the formulation of this standard the following publications have also been considered:
AS-4 100-1998 Steel structures (second edition), Standards Australia (Standards Association of Australia),
Homebush, NSW 2140,
BS-5950-2000 Structural use of steelwork in buildings:
Part 1 Code of practice for design in simple and continuous construction: Hot rolled sections, British
Standards Institution, London.
CAN/CSA- Limit states design of steel structures, Canadian Standards Association, Rexdale (Toronto),
S16.1-94 Ontario, Canada M9W 1R3.
ENV [993-1-1: Eurocode 3: Design of steel structures:
1992 Part 1-1 General rules and rules for buildings
The composition of the Committee responsible for the formulation of this standard is given in Annex J.
For the purpose of deciding whether a particular requirement of this standard, is complied with, the final value,
observed or calculated, expressing the result of a test or analysis, shall be rounded off in accordance with
IS 2:1960 ‘Rules for rounding off numerical values (revised)’. The number of significant places retained in the
rounded off value should be the same as that of the specified value in this standard.

1S 800:2007
Contents
SECTION 1 GENERAL
1.1 scope
1.2 References
1.3 Terminology
1,4 Symbols
1.5 Units
1.6 Standard Dimensions, Form and Weight
1.7 Plans and Drawings
1.8 Convention for Member Axes
SECTION 2 MATERIALS
2.1 General
2.2 Structural Steel
2.3 Rivets
2,4 Bolts, Nuts and Washers
2.5 SteeI Casting
2.6 Welding Consumable
2.7 Other Materials
SECTION 3 GENERAL DESIGN REQUIREMENTS
3.1 Basis for Design
3.2 Loads and Forces
3.3 Erection Loads
3.4 Temperature Effects
3.5 Load Combinations
3.6 Geometrical Properties
3.7 Classification of Cross-Sections
3.8 Maximum Effective Slenderness Ratio
3.9 Resistance to Horizontal Forces
3.10 Expansion Joints
SECTION 4 METHODS OF STRUCTURAL ANALYSIS
4.1 Methods of Determining Action Effects
4.2 Forms of Construction Assumed for Structural Analysis
4,3 Assumptions in Analysis
4.4 Elastic Analysis
4.5 Plastic Analysis
4.6 Frame Buckling Analysis
SECTION 5 LIMIT STATE DESIGN
5.2 Limit State Design
5.3 Actions
5.4 Strength
5,5 Factors Governing the Ultimate Strength
5.6 Limit State of Serviceability
SECTION 6 DESIGN OF TENSION MEMBERS
6.1 Tension Members
6.2 Design Strength Due to Yielding of Gross Section
6.3 Design Strength Due to Rupture of Critical Section
6.4 Design Strength Due to Block Shear
1
1
1
1
5
11
11
11
12
12
12
12
12
15
15
15
15
15
15
15
16
16
16
17
17
20
20
21
22
22
22
23
24
25
26
27
27
28
28
29
30
30
32
.,
32
32
32
33
i

IS 800:2007
SECTION 7 DESIGN OF COMPRESS1ON MEMBERS
7.1 Design Strength
7.2 Effective Length of Compression Members
7.3 Design Details
7.4 Column Bases
7.5 Angle Struts
7.6 Laced Columns
7.7 Battened Columns
7.8 Compression Members Composed of Two Components Back-to-Back
SECTION 8 DESIGN OF MEMBERS SUBJECTED TO BENDING
8.1 General
8.2 Design Strength in Bending (Flexure)
8.3 Effective Length for Lateral Torsional Buckling
8.4 Shear
8.5 Stiffened Web Panels
8.6 Design of Beams and Plate Girders with Solid Webs
8.7 Stiffener Design
8.8 Box Girders
8.9 Purlins and Sheeting Rails (Girts)
8.10 Bending in a Non-Principal Plane
SECTION 9 MEMBER SUBJECTED TO COMBINED FORCES
9.1 General
9.2 Combined Shear and Bending
9.3 Combined Axial Force and Bending Moment
SECTION 10 CONNECTIONS
10.1 General
10.2 Location Details of Fasteners
10.3 Bearing Type Bolts
10.4 Friction Grip Type Bolting
10.5 Welds and Welding
10.6 Design of Connections
10.7 Minimum Design Action on Connection
10.8 Intersections
10.9 Choice of Fasteners
10.10 Connection Components
10.11 Analysis of a Bolt/Weld Group
10.12 Lug Angles
SECTION 11 WORKING STRESS DESIGN
11.1 General
11.2 Tension Members
11.3 Compression Members
11.4 Members Subjected to Bending
11.5 Combined Stresses
11.6 Connections
SECTION 12 DESIGN AND DETAILING FOR EARTHQUAKE LOADS
12.1 General
12.2 Load and Load Combinations
12.3 Response Reduction Factor
12.4 Connections, Joints and Fasteners
12.5 Columns
12.6 Storey Drift
12.7 Ordinary Concentrically Braced Frames (OCBF)
34
34
35
46
46
47
48
50
52
52
52
52
54
59
60
63
65
69
69
69
69
69
69
70
73
73
73
74
76
78
81
82
82
82
82
83
83
84
84
84
84
85
85
86
87
87
87
87
87
87
88
88
ii

12.8 Special Concentrically Braced Frames (SCBF)
12.9 Eccentrically Braced Frames (EBF)
1~.10 Ordinav Moment Frames (OMF)
12.11 Special Moment Frames (SMF)
12.12 Column Bases
SECTION 13 FATIGUE
13.1 General
13.2 Design
13.3 Detail Category
13.4 Fatigue Strength
13.5 Fatigue Assessment
13.6 Necessity for Fatigue Assessment
SECTION 14 DESIGN ASSISTED BY TESTING
14.1 Need for Testing
14.2 Types of Test
14.3 Test Conditions
14.4 Test Loading
14.5 Criteria for Acceptance
SECTION 15 DURABILITY
15.1 General
15.2 Requirements for Durability
SECTION 16 FIRE RESISTANCE
16.1 Requirements
16.2 Fire Resistance Level
16.3 Period of Structural Adequacy (PSA)
16.4 Variation of Mechanical Properties of Steel with Temperature
16.5 Limiting Steel Temperature
16.6 Temperature Increase with Time in Protected Members
16.7 Temperature Increase with Time in Unprotected Members
16.8 Determination of PSA from a Single Test
16.9 Three-Sided Fire Exposure Condition
16.10 Special Considerations
16.11 Fire Resistance Rating
SECTION 17 FABRICATION AND ERECTION
17.1 General
17.2 Fabrication Procedures
17.3 Assembly
17.4 Riveting
17.5 Bolting
17.6 Welding
17.7 Machining of Butts, Caps and Bases
17.8 Painting
17.9 Marking
17.10 Shop Erection
17.11 Packing
17.12 Inspection and Testing
17.13 Site Erection
17.14 Painting After Erection
17.16 Steelwork Tenders and Contracts
..
111
IS 8~0 :2007
88
89
89
90
90
91
91
91
92
93
99
100
100
100
101
102
102
103
103
103
103
105
105
105
106
106
106
107
108
108
108
108
109
110
110
110
112
113
113
113
113
113
114
114
114
114
114
116
116

IS 800:2007
ANNEX A LIST OF REFERRED INDIAN STANDARDS 117
ANNEX B ANALYSIS AND DESIGN METHODS
B-1 Advanced Structural Analysis and Design
B-2 Second Order Elastic Analysis and Design
B-3 Frame Instability Analysis
ANNEX C DESIGN AGAINST FLOOR VIBRATION
C-1 General
C-2 Annoyance Criteria
C-3 Floor Frequency
C-4 Damping
C-5 Acceleration
ANNEX D DETERMINATION OF EFFECTIVE LENGTH OF COLUMNS
D-1 Method for Determining Effective Length of Columns in Frames
D-2 Method for Determining Effective Length for Stepped Columns (see 7.2.2)
D-3 Effective Length for Double Stepped Columns
ANNEX E ELASTIC LATERAL TORSIONAL BUCKLING
E-1 Elastic Critical Moment
ANNEX F CONNECTIONS
F-1 General
F-2 Beam Splices
F-3 Column Splice
F-4 Beam-to-Column Connections
F-5 Column Bases
ANNEX G GENERAL RECOMMENDATIONS FOR STEELWORK TENDERS
AND CONTRACTS
G-1 General
G-2 Exchange of Information
G-3 Information Required by the Steelwork Designer
G+4 Information Required by Tenderer (If Not Also Designer)
G-5 Detailing
G-6 Time Schedule
G-7 Procedure on Site
G-8 Inspection
G-9 Maintenance
ANNEX H PLASTIC PROPERTIES OF BEAMS
120
120
120
120
121
121
121
121
122
122
122
122
124
124
128
128
130
130
130
130
131
134
135
135
135
135
136
137
137
137
137
137
138
iv

AMENDMENT NO. 1 JANUARY 2012
TO
IS 800 : 2007 GENERAL CONSTRUCTION IN STEEL —
CODE OF PRACTICE
(Third Revision)
[(Page (iii), Section 17] — Insert the following new item, as appropriate:
‘17.15 Bedding Requirement 116’
(Page 6, line 38) — Delete the symbols ‘Cmy, Cmz’ and the corresponding explanation.
(Page 8, line 33) — Insert the following symbols and explanations after this line:
‘Ky, Kz, KLT — Moment amplification factors (see 4.4.2, 4.4.3.1, 4.4.3.3 and 9.3.2.2)’
(Page 18, Table 2, col 2) — Substitute ‘d/t’ for ‘D/tf’ for entry against ‘Stem of a T-section, rolled or cut
from a rolled I- or H-section’.
(Page 18, Table 2, col 3, 4 and 5) — Substitute ‘but ≥ 42ε’ for ‘but ≤ 42 ε’ for entries against ‘Web of an I,
H or box section’.
(Page 18, Table 2, Notes, last line) — Substitute ‘overall’ for ‘overll’.
(Page 19, Fig. 2, ROLLED CHANNELS) — Substitute ‘d’ for ‘h’ in the figure.
(Page 24, clause 4.4.2, line 10) — Substitute ‘Ky, Kz’ for ‘Cy, Cz’.
(Page 24, clause 4.4.3.1, line 9) — Substitute ‘Ky and Kz’ for ‘Cy and Cz’.
(Page 24, clause 4.4.3.3, line 3) — Substitute ‘(Ky, Kz)’ for ‘(Cmy, Cmz)’.
(Page 25, clause 4.5.2, line 19) — Insert ‘less’ between ‘be’ and ‘than’.
(Page 31, clause 5.6.1, line 6) — Substitute ‘using load factors of Table 4.’ for ‘using a load factor of 1.0.’
(Page 31, clause 5.6.1, third sentence) — Insert the following at the end:
‘In Table 6, live load should include all post construction loads including superimposed dead loads.’
(Page 33, clause 6.3.3, line 6) — Substitute ‘0.9 fu γm0/fy γm1’ for ‘fu γm0/fy γm1’.
(Page 34, clause 7.1.2, line 1) — Substitute the following for the existing:
‘The factored design compression, P in members shall satisfy the following requirement:
P < Pd’
(Page 34, clause 7.1.2.1, line 20) — Substitute ‘γm0’ for ‘λm0’.
Price Group 3
1

Amend No. 1 to IS 800 : 2007
(Page 35, Fig. 8) — Insert ‘λ’ as the title of the abscissa (x-axis).
(Page 44, Table 10, col 2, line 3) — Substitute ‘40 mm < tf ≤ 100 mm’ for ‘40 ≤ mm < tf ≤ 100 mm’.
(Page 45, Table 11, second row, col 1 and 2) — Substitute the following for the existing entries:
(1) (2)
Restrained Free
(Page 48, clause 7.5.1.2, line 4) — Add the following in the end:
“, in place of λ in 7.1.2.1 and using curve ‘c’ (α = 0.49)”
(Page 48, clause 7.5.1.2, line 9, formula) — Substitute the following for the existing:
‘
 
1 2
2 2
/ 2
and
250 250
vv
vv
l
b b t
r
E E

 
 
 


 
 
   ’
(Page 49, Fig. 10) — Substitute the following figure for the existing as appropriate, and substitute
‘Members’ for ‘Numbers’ in the sub-title of Fig. 10C and substitute the existing title of Fig. 10 with ‘TOP
RESTRAINT CONDITIONS’:
(Page 53, clause 8.2.1.1, line 3) — Substitute ‘ d/tw > 67ε’ for ‘d/tw ≤ 67ε’.
(Page 54, clause 8.3.1, second para) — Substitute the following for the existing:
‘In simply supported beams with intermediate lateral restraints against lateral torsional buckling, the effective
length for lateral torsional buckling, LLT to be used in 8.2.2.1 shall be taken as the length of the relevant segment
in between the lateral restraints. In the case of intermediate partial lateral restraints, the effective length, LLT
shall be taken as equal to 1.2 times the length of the relevant segment in between the partial lateral restraints.’
(Page 57, Table 14) — Substitute ‘LLT/ry’ and ‘hf/tf’ for ‘KL/r’ and ‘h/tf’.
(Page 58, clause 8.3.2, line 9) — Insert ‘centre’ between ‘shear’ and ‘and’.
(Page 58, Table 15, col 3, first row) — Substitute ‘Both flanges partially restrained’ for ‘Both flanges fully
restrained’.
2

Amend No. 1 to IS 800 : 2007
(Page 59, clause 8.4.2.1) — Substitute ‘ε w’ for ‘ε’ and ‘fyw’ for ‘fy’, wherever appearing.
(Page 60, clause 8.4.2.2, col 1, line 18 from top) — Substitute cr,e cr,e
‘
τ ’ ‘t ’
for .
(Page 60, clause 8.4.2.2, col 2, line 52) — Substitute ‘nearly = tan-1
1.5
d
c
 
 
 
’ for ‘ = tan-1
d
c
 
 
  ’.
(Page 60, clause 8.4.2.2, col 2, line 55) — Substitute ‘= d cosф – (c – sc – st) sinф, for the existing.
(Page 60, clause 8.4.2.2, col 2, lines 59 and 60) — Delete the lines.
(Page 60, clause 8.5.1, line 3) — Insert ‘out’ between ‘carried’ and ‘in’.
(Page 61, Table 16, last row, col 1) — Substitute the following for the existing figure:
(Page 62, Fig. 12) — Substitute the following for the existing figure:
NOTES
1 Panel A is designed utilizing tension field action as given in 8.4.2.2(b).
2 Panel B is designed using simple post critical method as given in 8.4.2.2(a).
3 Bearing stiffener is designed for the compressive force due to bearing plus compressive force due to the
moment Mtf as given in 8.5.3.
FIG. 12 END PANEL DESIGNED NOT USING TENSION FIELD ACTION
(Page 63, Fig. 13, Notes) — Delete NOTE 2 and renumber the subsequent Note accordingly.
(Page 63, clause 8.6.1.1) — Substitute ‘εw’ for ‘ε’ wherever appearing.
(Page 63, clause 8.6.1.1, line 13) — Substitute ‘c < 0.74d’ for ‘c < d’.
3

Amend No. 1 to IS 800 : 2007
(Page 64, clause 8.6.1.2, line 15) — Substitute ‘εf = yield stress ratio of flange =
yf
250
f
’ for ‘εf = yield
stress ratio of web =
yf
250
f
’.
(Page 65, clause 8.7.1.2, second para, line 1) — Insert ‘stiffener’ between the words ‘web’ and ‘is’.
[Page 70, clause 9.3.1.2(c)] — Substitute the following for the existing:
‘c) For standard I or H sections
Mndz = 1.11 Mdz (1 – n) ≤ Mdz
for n ≤ 0.2, Mndy = Mdy
for n > 0.2, Mndy = 1.56 Mdy (1 - n) (n + 0.6)’
(Page 72, Table 18) — Substitute the following for the existing table:
Cmy, Cmz, CmLT
Bending Moment Diagram
(1)
Range
(2) Uniform Loading
(3)
Concentrated Load
(4)
−1 ≤ ψ ≤ 1 0.6 + 0.4 ψ ≥ 0.4
0 ≤ αs≤ 1 −1 ≤ ψ ≤ 1 0.2 + 0.8 αs ≥ 0.4 0.2 + 0.8 αs ≥ 0.4
0 ≤ ψ ≤ 1 0.1 − 0.8 αs ≥ 0.4 − 0.8 αs ≥ 0.4
−1 ≤ αs ≤ 0
−1 ≤ ψ ≤ 0 0.1(1−ψ) − 0.8 αs ≥ 0.4 0.2(−ψ) −0.8 αs ≥ 0.4
0 ≤ αh ≤ 1 −1 ≤ ψ ≤ 1 0.95 − 0.05 αh
0.90 + 0.10 αh
0 ≤ ψ ≤ 1 0.95 + 0.05 αh 0.90 + 0.10 αh
−1 ≤ αh ≤ 0
−1 ≤ ψ ≤ 0 0.95 + 0.05 αh (1+2 ψ) 0.90 + 0.1αh (1+2 ψ)
For members with sway buckling mode, the equivalent uniform moment factor Cmy = Cmz = 0.9.
Cmy, Cmz, CmLT shall be obtained according to the bending moment diagram between the relevant braced points
Moment factor Bending axis Points braced in direction
Cmy z – z y – y
Cmz y – y z – z
CmLT z – z z – z
4
M
M
Mh
Ms
Mh
αs = Ms/ Mh
Mh
Mh
Ms
αh = Mh/ Ms
My for Cmy
Mz
for Cmz
for CmLT

Amend No. 1 to IS 800 : 2007
(Page 75, clause 10.3.2, line 3) — Substitute the following for the existing:
‘Vsb ≤ Vdb’
(Page 76, clause 10.4.3, first sentence) — Substitute the following for the existing:
‘Design for friction type bolting, where slip resistance is required at factored design force Vsf, shall satisfy the
following:’
(Page 76, clause 10.4.3, line 14) — Substitute ‘μf ≤ 0.55’ for ‘μf = 0.55’.
(Page 76, clause 10.4.3, Note, line 1) — Substitute ‘Vnsf’ for ‘Vns’.
(Page 77, clause 10.4.5, col 1, line 6, from top, formula) — Substitute ‘0.9 fub An ≤ fyb Asb(γm1/γm0)’ for ‘0.9
fub An ≤ fyb Asb(γm1/γm)’.
(Page 80, clause 10.5.10.2.2, line 7, formula) — Substitute ‘ 2
br
f ’ for ‘ 2
bf
f ’.
(Page 89, clause 12.8.2.1, first sentence) — Substitute the following for the existing:
‘Bracing members shall be made of E250B steel of IS 2062 or of steel having Charpy V-notch energy, E > 27J.’
(Page 90, clause 12.11.1, line 2) — Insert ‘or of steel having Charpy V-notch energy, E > 27J’ between
‘IS 2062’ and ‘and’.
(Page 106, clause 16.4.1, line 4, formula) — Substitute ‘
 
 
y
y
T 905 –
= 1.0
690
20
f T
f
 for the existing.
(Page 121, Annex B, clause B-3.2, line 10 from top, formula) — Substitute ‘фsi =
i
Li
ui
h

 
’ for ‘фs =
h
L
u 
 
’.
(Page 121, Annex B, clause B-3.2, lines 12, 13 and 16 from top) – Substitute ‘hi’, ‘δui’ and ‘δLi’ for ‘h’, ‘δu’
and ‘δL’.
(Page 128, Annex E, clause E-1.2, line 5, formula) — Substitute ‘(LLT)2
’ for ‘(LLT)’.
(Page 128, Annex E, clause E-1.2, line 30) — Substitute ‘(z2
+ y2
)2
’ for ‘(z2
– y2
)’.
(Page 129, Annex E, clause E-1.2, col 1, line 18 from top) — Insert ‘St. Venant’s’ before ‘torsion’.
(Page 130, Table 42, col 5, row 7) — Substitute ‘1.267’ for ‘1.257’.
(Page 129, Table 42, col 6, rows 5 and 10) — Substitute ‘1.730’ for ‘1.780’ and ‘1.890’ for ‘1.390’,
respectively.
(CED 7)
Reprography Unit, BIS, New Delhi, India
5

. .. .... . -=
IS 800:2007
Indian Standard
GENERAL CONSTRUCTION IN
STEEL — CODE OF PRACTICE
( Third Revision)
SECTION 1
GENERAL
1.1 Scope
1.1.1 This standard applies to general construction
using hot rolled steel sections joined using riveting,
bolting and welding. Specific provisions for bridges,
chimneys, cranes, tanks, transmission line towers, bulk
storage structures, tubular structures, cold formed light
gauge steel sections, etc, are covered in separate
standards.
1.1.2 This standard gives only general guidance as regards
the various loads to be considered in design. For the actual
loads and load combinations to be used, reference may
be made to IS 875 for dead, live, snow and wind loads
and to IS 1893 (Part 1) for earthquake loads.
1.1.3 Fabrication and erection requirements covered
in this standard are general and the minimum necessary
quality of material and workmanship consistent with
assumptions in the design rules. The actual
requirements may be further developed as per other
standards or the project specification, the type of
structure and the method of construction.
1.1.4 For seismic design, recommendations pertaining
to steel frames only are covered in this standard. For
more detailed information on seismic design of other
structural and non-structural components, refrence
should be made to IS 1893 (Part 1) and other special
publications on the subject.
1.2 References
The standards listed in Annex A contain provisions
which through reference in this text, constitute
provisions of this standard. At the time of publication,
the editions indicated were valid. All standards are
subject to revision and parties to agreements based on
this standard are encouraged to investigate the
possibility of applying the most recent editions of the
standards indicated in Annex A.
1.3 Terminology
For the purpose of this standard, the following
definitions shall apply.
1.3.1 Accidental Loads — Loads due to explosion,
impact of vehicles, or other rare loads for which the
structure is considered to be vulnerable as per the user.
1.3.2 Accompanying Load — Live (imposed) load
acting along with leading imposed load but causing
lower actions and/or deflections.
1.3.3 Action Effect or Load Effect — The internal force,
axial, shear, bending or twisting moment, due to
external actions and temperature loads,
1.3.4 Action — The primary cause for stress or
deformations in a structure such as dead, live, wind,
seismic or temperature loads.
1.3.5 Actual Length — The length between centre-to-
centre of intersection points, with supporting members
or the cantilever length in the case of a free standing
member.
1.3.6 Beam — A member subjected predominantly to
bending.
1.3.7 Bearing Type Connection — A connection made
using bolts in ‘snug-tight’ condition, or rivets where
the load is transferred by bearing of bolts or rivets
against plate inside the bolt hole.
1.3.8 Braced Member — A member in which the
relative transverse displacement is effectively prevented
by bracing.
1.3.9 Brittle Cladding — Claddings, such as asbestos
cement sheets which get damaged before undergoing
considerable deformation.
1.3.10 Buckling Load— The load at which an element,
a member or a structure as a whole, either collapses in
service or buckles in a load test and develops excessive
lateral (out of plane) deformation or instability.
1.3.11 Buckling Strength or Resistance — Force or
moment, which a member can withstand without
buckling.
1.3.12 Bui/t-ap Section — A member fabricated by
interconnecting more than one element to form a
compound section acting as a single member.
1.3.13 Camber- Intentionally introduced pre-curving
(usually upwards) in a system, member or any portion
1

IS 800:2007
of a member with respect to its chord. Frequently,
camber is introduced to compensate for deflections at
a specific level of loads.
1.3.14 Characteristic Load (Action) — The value of
specified load (action), above which not more than a
specified percentage (usually 5 percent) of samples of
corresponding load are expected to be encountered.
1.3.15 Characteristic Yield/Ultimate Stress — The
minimum value of stress, below which not more than
a specified percentage (usually 5 percent) of
corresponding stresses of samples tested are expected
to occur.
1.3.16 Column — A member in upright (vertical)
position which supports a roof or floor system and
predominantly subjected to compression.
1.3.17 Compact Section —A cross-section, which can
develop plastic moment, but has inadequate plastic
rotation capacity needed for formation of a plastic
collapse mechanism of the member or structure.
1.3.18 Constant Stress Range — The amplitude
between which the stress ranges under cyclic loading
is constant during the life of the structure or a structural
element.
1.3.19 Corrosion — An electrochemical process over
the surface of steel, leading to oxidation of the metal.
1.3.20 Crane Load — Horizontal and vertical loads
from cranes.
1.3.21 Cumulative Fatigue — Total damage due to
fatigue loading of varying stress ranges.
1.3.22 Cut-o~Limit — The stress range, corresponding
to the particular detail, below which cyclic loading need
not be considered in cumulative fatigue damage
evaluation (corresponds to 108 numbers of cycles in
most cases).
1.3.23 Dead Loads — The self-weights of all
permanent constructions and installations including the
self-weight of all walls, partitions, floors, roofs, and
other permanent fixtures acting on a member.
1.3.24 Dejection — It is the deviation from the
standard position of a member or structure.
1.3.25 Design Life — Time period for which a structure
or a structural element is required to perform its
function without damage.
1.3.26 Design Load/Factored Load — A load value
ob~~ined by multiplying the characteristic load with a
load factor.
1.3.27 Design Spectrum — Frequency distribution of
the stress ranges from all the nominal loading events
during the design life (stress spectrum).
1.3.28 Detail Category — Designation given to a
particular detail to indicate the S-N curve to be used in
fatigue assessment.
1.3.29 Discontinuity — A sudden change in cross-
section of a loaded member, causing a stress
concentration at the location.
1.3.30 Ductility — It is the property of the material or
a structure indicating the extent to which it can deform
beyond the limit of yield deformation before failure or
fracture. The ratio of ultimate to yield deformation is
usually termed as ductility.
1.3.31 Durability — It is the ability of a material to
resist deterioration over long periods of time.
1.3.32 Earthquake Loads — The inertia forces
produced in a structure due to the ground movement
during an earthquake.
1.3.33 Edge Distance — Distance from the centre of a
fastener hole to the nearest edge of an element
measured perpendicular to the direction of load
transfer.
1.3.34 Eflective Lateral Restraint — Restraint, that
produces sufficient resistance to prevent deformation
in the lateral direction.
1.3.35 Effective Length — Actual length of a member
between points of effective restraint or effective
restraint and free end, multiplied by a factor to take
account of the end conditions in buckling strength
calculations.
1.3.36 Elastic Cladding — Claddings, such as metal
sheets, that can undergo considerable deformation
without damage.
1.3.37 Elastic Critical Moment —The elastic moment,
which initiates lateral-torsional buckling of a laterally
unsupported beam.
1.3.38 Elastic Design — Design, which assumes elastic
behaviour of materials throughout the service load
range.
1.3.39 Elastic Limit — It is the stress below which the
material regains its original size and shape when the
load is removed. In steel design, it is taken as the yield
stress.
1.3.40 End Distance — Distance from the centre of a
fastener hole to the edge of an element measured
parallel to the direction of load transfer.
1.3.41 Erection Loads — The actions (loads and
deformations) experienced by the structure exclusively
during erection.
1.3.42 Erection Tolerance — Amount of deviation
related to the plumbness, alignment, and level of the
2

. ... . —...,
element as a whole in the erected position. The
deviations are determined by considering the locations
of the ends of the element.
1.3.43 Exposed Surface Area to Mass Ratio — The
ratio of the surface area exposed to the fire (in mm2) to
the mass of steel (in kg).
NOTE — In the case of members with tire protection material
applied, the exposed surface area is to be taken as the internal
sur~acearea of the fire protection material.
1.3.44 Fabrication Tolerance — Amount of deviation
allowed in the nominal dimensions and geometry in
fabrication activities, such as cutting to length, finishing
of ends, cutting of bevel angles, etc.
1.3.45 Factor of Safety — The factor by which the yield
stress of the material of a member is divided to arrive
at the permissible stress in the material.
1.3.46 Fatigue — Damage caused by repeated
fluctuations of stress, leading to progressive cmcking
of a structural element.
1.3.47 Fatigue Loading — Set of nominal loading
events, cyclic in nature, described by the distribution
of the loads, their magnitudes and the number of
applications in each nominal loading event.
1.3.48 Fatigue Strength — The stress range for a
category of detail, depending upon the number of
cycles it is required to withstand during design life.
1.3.49 Fire Exposure Condition
a) Three-sidedfire exposure condition — Steel
member incorporated in or in contact with a
concrete or masonry floor or wall (at least
against one surface).
NOTES
1Three-sided fire exposure condition is to be considered
separately unless otherwise specified (see 16.10).
2 Members with more than one face in contact with a
concrete or masonry floor or wall may be treated as
three-sided tire exposure.
b) Four-sided jire exposure condition — Steel
member, which may be exposed to fire on all
sides.
1.3.50 Fire Protection System — The fire protection
material and its method of attachment to the steel
member.
1.3.51 Fire Resistance — The ability of an element,
component or structure, to fulfil for a stated period of
time, the required stability, integrity, thermal insulation
and/or other expected performance specified in a
standard fire test.
1.3.52 Fire Resistance Level —The fwe resistance grading
period for a structural element or system, in minutes,
which is required to be attained in the standard fire test.
IS 800:2007
1.3.53 Flexural Stiffness — Stiffness of a member
against rotation as evaluated by the value of bending
deformation moment required to cause a unit rotation
while all other degrees of freedom of the joints of the
member except the rotated one are assumed to be
restrained.
1.3.54 Friction Type Connection — Connection
effected by using pre-tensioned high strength bolts
where shear force transfer is due to mobilisation of
friction between the connected plates due to clamping
force developed at the interface of connected plates
by the bolt pre-tension.
1.3.55 Gauge — The spacing between adjacent parallel
lines of fasteners, transverse to the direction of load/
stress.
1.3.56 Gravity Load — Loads arising due to
gravitational effects.
1,3.57 Gwsset Plate — The plate to which the members
intersecting at a joint are connected.
1.3.58 High Shear — High shear condition is caused
when the actual shear due to factored load is greater
than a certain fraction of design shear resistance
(see 9.2.2).
1.3.59 Imposed (Live) Load — The load assumed to
be produced by the intended use or occupancy
including distributed, concentrated, impact, vibration
and snow loads but excluding, wind, earthquake and
temperature loads.
1.3.60 Instability — The phenomenon which disables
an element, member or a structure to carry further load
due to excessive deflection lateral to the direction of
loading and vanishing stiffness.
1.3.61 Lateral Restraint for a Beam (see 1.3.34)
1.3.62 Leading Imposed Load— Imposed load causing
higher action and/or deflection.
1.3.63 Limit State — Any limiting condition beyond
which the structure ceases to fulfil its intended function
(see also 1.3.86).
1.3.64 Live Load (see 1.3.59)
1.3.65 Load — An externally applied force or action
(see also 1.3.4).
1.3.66 Main Member — A structural member, which
is primarily responsible for carrying and distributing
the applied load or action.
1.3,67 Mill Tolerance — Amount of variation allowed
from the nominal dimensions and geometry, with
respect to cross-sectional area, non-parallelism of
3

IS 800:2007
flanges, and out of straightness such as sweep or
camber, in a product, as manufactured in a steel mill.
1.3.68 Normal Stress — Stress component acting
normal to the face, plane or section.
1.3,69 Partial Safety Factor — The factor normally
greater than unity by which either the loads (actions)
are multiplied or the resistances are divided to obtain
the design values.
1.3.70 Period of Structural Adequacy under Fire ——
The time (t), in minutes, for the member to reach the
limit state of structural inadequacy in a standard fire
test.
1.3.71 Permissible S~rcss — When a structure is being
designed by the working stress method, the maximum
stress that is permitted to be experienced in elements,
members or structures under the nominal/service load
(action).
1.3.72 Pitch — The centre-to-centre distance between
individual fasteners in a line, in the direction of load/
stress.
1.3.73 Plastic Collapse — The failure stage at which
sufficient number of plastic hinges have formed due
to the loads (actions) in a structure leading to a failure
mechanism.
1.3.74 Plastic IMsi,gn — Design against the limit state
of plastic collapse.
1.3.75 Plastic Hinge — A yielding zone with
significant inelastic rotation, which forms in a member,
when the plastic moment is reached at a section.
1.3.76 Plastic Mo~nent — Moment capacity of a cross-
section when the entire cross-section has yielded due
to bending moment.
1.3.77 Plastic Section — Cross-section, which can
develop a plastic hinge and sustain piastic moment over
sufficient plastic rotation required for formation of
plastic failure mechanism of the member or structure.
1,3.78 Poisson’s Ratio — It is the absolute value of
the ratio of lateral strain to longitudinal strain under
uni-axial Ioading.
1.3.79 Proof Stress — The stress to which high strength
friction grip (HSFG) bolts are pre-tensioned.
1.3,80 Proof Testing — The application of test loads
to a structure, sub-structure, member or connection to
ascertain the structural characteristics of only that
specific unit.
1.3.81 Prototype Testing — Testing of structure, sub-
structure, members or connections to ascertain the
structural characteristics of that class of structures, sub-
structures, members or connections that are nominally
identical (full scale) to the units tested.
1.3.82 Prying Force — Additional tensile force
developed in a bolt as a result of the flexing of a
connection component such as a beam end plate or leg
of an angle.
1.3.83 Rotatiort — The change in angle at a joint
between the original orientation of two linear member
and their final position under Ioadlng.
1.3.84 Secondary Member — Member which is
provided for overall stability and or for restraining the
main members from buckling or similar modes of
failure.
1.3.85 Semi-compact Section — Cross-section, which
can attain the yield moment, but not the plastic moment
before failure by plate buckling.
1.3.86 Serviceability .Lirnit State — A limit state of
acceptable service condition exceedence of which
causes serviceability failure.
1.3.87 Shear Force — The inplane force at any
transverse cross-section of a straight member of a
column or beam.
1.3.88 Shear Lag — The in plane shear deformation
effect by which concentrated forces tangential to the
surface of a plate gets distributed over the entire section
perpendicular to the load over a finite length of the
plate along the direction of the load.
1.3.89 Shear Stress — The stress component acting
parallel to a face, plane or cross-section.
1.3.90 Slender Section — Cross-section in which the
elements buckle locally before reaching yield moment.
1.3.91 Slenderness Ratio — The ratio of the effective
length of a member to the radius of gyration of the
cross-section about the axis under consideration.
1.3.92 Slip Resistance — Limit shear that can be
applied in a friction grip connection before slip occurs.
1.3.93 S-N Curve —The curve defining the relationship
between the number of stress cycles to failure (N,c) at
a constant stress range (SC), during fatigue loading of
a structure.
1.3.94 Snow Load — Load on a structure due to the
accumulation of snow and ice on surfaces such as roof.
1.3.95 Snug i’ight ——
The tightness of a bolt achieved
by a few impacts of an impact wrench or by the full
effort of a person using a standard spanner.
1.3.96 Stability Limit State — A limit state
corresponding to the loss of static equilibrium of a
structure by excessive deflection transverse to the
direction of predominant loads.
4

1.3.97 Stackability — The ability of the fire protection
system to remain in place as the member deflects under
load during a fire test.
1.3.98 St~ffener — An element used to retain or prevent
the out-of-plane deformations of plates.
1.3.99 Strain — Deformation per unit length or unit
angle.
1.3.100 Strain Hardening — The phenomenon of
increase in stress with increase in strain beyond
yielding.
1.3.101 Strength — Resistance to failure by yielding
or buckling.
1.3.102 Strength Limir State — A limit state of collapse
or loss of structural integrity.
1.3.103 Stress — The internal force per unit area of
the original cross-section,
1.3.104 Stress Analysis —The analysis of the internal
force and stress condition in an element, member or
structure.
I.3.105 Stress Cycle Counting — Sum of individual
stress cycles from stress history arrived at using any
rational method.
1.3.106 Stress Range — Algebraic difference between
two extremes of stresses in a cycle of loading.
1.3.107 Stress Spectrum — Histogram of stress cycles
produced by a nominal loading event design spectrum,
during design life.
1.3.108 Structural Adequacy for Fire — The ability of
the member to carry the test load exposed to the
standard fire test.
1.3.109 Structural Analysis — The analysis of stress,
strain, and deflection characteristics of a structure.
1.3.110 Strut — A compression member, which may
be oriented in any direction.
1.3.111 Sway — The lateral deflection of a frame.
1.3.112 Sway Member — A member in which the
transverse displacement of one end, relative to the other
is not effectively prevented.
1.3.113 Tensile Stress — The characteristic stress
corresponding to rupture in tension, specified for the
grade of steel in the appropriate Indian Standard, as
listed in Table 1.
1.3.114 Test Load — The factored load, equivalent to
a specified load combination appropriate for the type
of test being performed.
IS 800:2007
1.3.115 Transverse — Direction atong the stronger axes
of the cross-section of the member.
1.3.116 Ultimate Limit State — The state which, if
exceeded can cause collapse of a part or the whole of
the structure.
1.3.117 Ultimate Stress (see 1.3.113)
1.3.118 Wind Loads — Load experienced by member
or structure due to wind pressure acting on the surfaces.
1.3.119 Yield Stress — The characteristic stress of the
material in tension before the elastic limit of the
material is exceeded, as specified in the appropriate
Indian Stwdard, as listed in Table 1.
1.4 Symbols
Symbols used in this standard shall have the following
meanings with respect to the structure or member or
condition. unless otherwise defined elsewhere in this
Code.
A
AC
A.
AC,
A,
A,
A,,
A,O
A,
An,
A,,C
An,
A,O
A,,
A,
A,
A,,
At,
—
—
—
—
—
—
—
—
—
—
—
—
—
—
Area of cross-section
Area at root of threads
Effective cross-sectional area
Reduced effective flange area
Total flange area
Gross cross-sectional area
Gross cross-sectional area of flange
Gross cross-sectional area of
outstanding (not connected) leg of a
member
Net area of the total cross-section
Net tensile cross-sectional area of bolt
Net cross-sectional area of the
connected leg of a member
Net cross-sectional area of each
flange
Net cross-sectional area of
outstanding (not connected) leg of a
member
Nominal bearing area of bolt on any
plate
— Cross-sectional area of a bearing
(load carrying) stiffener in contact
with the flange
— Tensile stress area
— Gross cross-sectional area of a bolt
at the shank
— Gross sectional area in tension from
the centre of the hole to the toe of
the angle section/channel section, etc
(see 6.4) perpendicular to the line of
force
5

IS 800:2007
A,n
Av
Av,
A,,
a, b
aO
al
B
b
b,
be
b,
b,
b,,
b,
b,
b,
b.
c
cm
— Net sectional area in tension from the
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
Cn,y,
Cmz—
c
Ch
C,n
c,
D
d
d,
—
—
—
—
—
—
—
centre of the hole to the toe of
the angle perpendicular to the line
of force (see 6.4)
Shear area
Gross cross-sectional area in shear
along the line of transmitted force
(see 6.4)
Net cross-sectional area in shear
along the line of transmitted force
(se: 6.4 )
Larger and smaller projection of the
slab base beyond the rectangle
circumscribing the column,
respectively (see 7.4)
Peak acceleration
Unsupported length of individual
elements being laced between lacing
points
Length of side of cap or base plate of
a column
Outstand/width of the element
Stiff bearing length, Stiffener bearing
length
Effective width of flange between
pair of bolts
Width of the flange
Width of flange as an internal element
Width of flange outstand
Panel zone width between column
flanges at beam-column junction
Shear lag distance
Width of tension field
Width of outstanding leg
Centre-to-centre longitudinal
distance of battens
Coefficient of thermal expansion
Moment amplification factor about
respective axes
Spacing of transverse stiffener
Moment amplification factor for
braced member
Moment reduction factor for lateral
torsional buckling strength
calculation
Moment amplification factor for
sway frame
Overall depth/diameter of the cross-
section
Depth of web, Nominal diameter
Twice the clear distance from the
d,
dO
dP
E
E (~
E (20)
E,
Fcd
w
Fd
F.
FO
F,,,
F~
F,,,
Flest
F,~,,,,
Ftest,
Mm
Ftesl,R
Ftest,
s
FW
F,
FXd
f
f,
f,
L
k.
J,c
“&(
.fipb
J,,,
compression flange angles, plates or
tongue plates to the neutral axis
— Diameter of a bolt/ rivet hole
— Nominal diameter of the pipe column
or the dimensions of the column in
the depth direction of the base plate
— Panel zone depth in the beam-column
junction
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
-—
—
—
—
—
—
—
Modulus of elasticity for steel
Modulus of elasticity of steel at T “C
Modulus of elasticity of steel at 20”C
Modulus of elasticity of the panel
material
Buckling strength of un-stiffened
beam web under concentrated load
Factored design load
Normal force
Minimum proof pretension in high
strength friction grip bolts.
Bearing capacity of load carrying
stiffener
Stiffener force
Stiffener buckling resistance
Test load
Load for acceptance test
Minimum test load from the test to
failure
Test load resistance
Strength test load
Design capacity of the web in bearing
External load, force or reaction
Buckling resistance of load carrying
web stiffener
Actual normal stress range for the
detail category
Frequency for a simply supported one
way system
Frequency of floor supported on steel
girder perpendicular to the joist
Calculated stress due to axial force
at service load
Permissible bending stress in
compression at service load
Permissible compressive stress at
service load
Permissible bending stress in tension
at service load
Permissible bearing stress of the bolt
at service load
Permissible stress of the bolt in shear
at service load
6

—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
.
—
—
—
—
—
—
—
—
—
—
—
—
1
1
1
1
permissible tensile stress at service
,oad
Permissible tensile stress of the bolt
it service load
Permissible stress of the weld at
service load
Actual bending stress at service load
Actual bending stress in compression
at service load
Design bending compressive stress
corresponding to lateral buckling
Actual bearing stress due to bending
at service load
Actual bending stress in tension at
service load
Permissible bending stress in column
base at service load
Actual axial compressive stress at
service load
Elastic buckling stress of a column,
Euler buckling stress
Design compressive stress
Extreme fibre compressive stress
corresponding elastic lateral buckling
moment
Equivalent stress at service load
Fatigue stress range corresponding to
5 x 10’ cycles of loading
Equivalent constant amplitude stress
Design normal fatigue strength
Highest normal stress range
Normal fatigue stress range
Normal stress in weld at service load
Proof stress
Actual bearing stress at service load
Actual bearing stress in bending at
service load
Bearing strength of the stiffeners
Frequency
Actual shear stress in bolt at service
load
Actual tensile stress at service load
Actual tensile stress of the bolt at
service load
Characteristic ultimate tensile stress
of the bolt
Average ultimate stress of the
material as obtained from test
of the connected plate
7
f“
f
.W
fwj
f w“
fx
&
fy(n
fy(20)
f,,
f,,
f ym
f,,
f,,
f Yw
G
g
h
IIb
hC
he
h,
hi
h,
h,
h,
I
Ifc
If,
I,
1,
I,.
.
—
—
.
—
—
—
—
—
—
.
—
—
—
—
—
—
—
—
—
—
—
—
.
—
—
—
—
—
—
—
IS 800:2007
Applied shear stress in the panel
designed utilizing tension field action
Actual stress of weld at service load
Design stress of weld at service load
Nominal strength of fillet weld
Maximum longitudinal stress under
combined axial force and bending
Characteristic yield stress
Yield stress of steel at T ‘C
Yield stress of steel at 20°C
Characteristic yield stress of bolt
Characteristic yield stress of flange
Average yield stress as obtained from
test
Characteristic yield stress of
connected plate
Characteristic yield stress of stiffener
material
Characteristic yield stress of the web
material
Modulus of rigidity for steel
Gauge length between centre of the
holes perpendicular to the load
direction, acceleration due to gravity
Depth of the section
Total height from the base to the floor
level concerned
Height of the column
Effective thickness
Cenre-to-centre distance of flanges
Thickness of fire protection material
Height of the lip
Storey height
Distance between shear centre of the
two flanges of a cross-section
Moment of inertia of the member
about an axis perpendicular to the
plane of the frame
Moment of inertia of the compression
flange of the beam about the axis
parallel to the web
Moment of inertia of the tension
flange of the beam about minor axis
Moment of inertia of a pair of
stiffener about the centre of the web,
or a single stiffener about the face of
the web
Second moment of inertia
Second moment of inertia of the
stiffener about the face of the element
perpendicular to the web

IS 800:2007
[T
1,
Iw
IV
I,
K,
K,
KL
KL(r
KLJry
KLlrz
— Transformed moment of inertia of the
one way system (in terms of
equivalent steel, assuming the
concrete flange of width equal to the
—
—
.
—
—
—
—
—
—
—
(1
KL
——
r 0
(“-) -
KL
r<
K, —
K,V —
k—
k—
sm
L—
L, —
LLT —
L. —
LO —
spacing of the beam to be effective)
St. Venant’s torsion constant
Warping constant
Moment of inertia about the minor
axis of the cross-section
Moment of inertia about the major
axis of the cross-section
Effective stiffness of the beam and
column
Reduction factor to account for the
high strength friction grip connection
bolts in over sized and slotted holes
Effective length of the member
Appropriate effective slenderness
ratio of the section
Effective slenderness ratio of the
section about the minor axis of the
section
section about the major axis of the
section
Actual maximum effective
slenderness ratio of the laced column
laced column accounting for shear
deformation
Shear buckling co-efficient
Warping restraint factor
Regression coefficient
Exposed surface area to mass ratio
Actual length, unsupported length,
Length centre-to-centre distance of
the intersecting members, Cantilever
length
Length of end connection in bolted
and welded members, taken as the
distance between outermost fasteners
in the end connection, or the length
of the end weld, measured along the
length of the member
Effective length for lateral torsional
buckling
Maximum distance from the restraint
to the compression flange at the
plastic hinge to an adjacent restraint
(limiting distance)
Length between points of zero
moment (inflection) in the span
8
1
1,
lg
li
1,
1,
lw
M
M,
MC,
M,
M,,
A’ldy
M&
M~fi
M,,
M,,
Mn,
—
—
—
—
—
—
—
—
—
—
—
—
—
Centre-to-centre length of the
supporting member
Distance between prying force and
bolt centre line
Grip length of bolts in a connection
Length of the joint
Length between points of lateral
support to the compression flange in
a beam
Distance from bolt centre line to the
toe of fillet weld or to half the root
radius for a rolled section
Length of weld
Bending moment
Applied bending moment
Elastic critical moment
corresponding to lateral torsional
buckling of the beam
Design flexural strength
Moment capacity of the section under
high shear
Design bending strength about the
minor axis of the cross-section
— Design bending strength about the
major axis of the cross-section
— Reduced effective moment
— Reduced plastic moment capacity of
the flange plate
— Design piastic resistance of the flange
alone
— Design bending strength under
combined axial force and uniaxial
moment
M,~Y,M“~Z—Design bending strength under
M, —
M,, —
M. —
M@ —
MP~~ —
M~ —
M, —
M,, —
MY —
combined axial force and the
respective uniaxial moment acting
alone
Plastic moment capacity of the
section
Moment in the beam at the
intersection of the beam and column
centre lines
Moments in the column above and
below the beam surfaces
Plastic design strength
Plastic design strength of flanges only
Applied moment on the stiffener
Moment at service (working) load
Moment resistance of tension flange
Factored applied moment about the
minor axis of the cross-section

M,,
M,
N
N,
N,
N,c
n
n,
n,
n,
P
P<..
P,
.
—
—
—
—
.
—
—
—
—
—
—
P,,, Pdz—
P,
PMm
P,
P,
P,
P
P,
Q
Q,
Q,
Q,
Q,
Q,
9
R
R,
—
—
—
—
—
—
—
—
—
—
—
—
.
—
—
—
Moment capacity of the stiffener
based on its elastic modulus
Factored applied moment about the
major axis of the cross-section
Number of parallel planes of battens
Design strength in tension or in
compression
Axial force in the flange
Numberof stress cycles
Number of bolts in the bolt group/
critical section
Number of effective interfaces
offering frictional resistance to slip
Number of shear planes with the
threads intercepting the shear plane
in the bolted connection
Number of shear planes without
threads intercepting the shear plane
in the bolted connection
Factored applied axial force
Elastic buckling load
Design axial compressive strength
Design compression strength as
governed by flexural buckling about
the respective axis
Elastic Euler buckling load
Minimum required strength for each
flange splice
Required compressive strength
Actual compression at service load
Yield strength of the cross-section
under axial compression
Pitch length between centres of holes
parallel to the direction of the
load
Staggered pitch length along the
direction of the load between lines of
the bolt holes (see Fig. 5)
Prying force
Accidental load (Action)
Characteristic loads (Action)
Design load (Action)
Permanent loads (Action)
Variable loads (Action)
Shear stress at service load
Ratio of the mean compressive stress
in the web (equal to stress at
mid depth) to yield stress of the web;
reaction of the beam at support
Design strength of the member at
room temperature
R,
R,
R,,
RU
r
rl
r~
r““
ry
r,
s
s,
s,
so
s,
s“
s,
s,
s,
T
T,
T,,
T~
T4
Tdn
Tdb
T.
T,
T,
T,b
T,d
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
IS 800:2007
Net shear in bolt group at bolt “i”
Response reduction factor
Flange shear resistance
Ultimate strength of the member at
room temperature
Appropriate radius of gyration
Minimum radius of gyration of the
individual element being laced
together
Ratio of the design action on the
member under fire to the design
capacity
Radius of gyration about the minor
axis (v-v) of angle section.
Radius of gyration about the minor
axis
Radius of gyration about the major
axis
Minimum transverse distance
between the centroid of the rivet or
bolt group or weld group
Constant stress range
Design strength
Original cross-sectional area of the
test specimen
Spring stiffness
Ultimate strength
Anchorage length of tension field
along the compression flange
Anchorage length of tension field
along the tension flange
Actual stiffener spacing
Temperature in degree Celsius;
Factored tension
Applied tension in bolt
Thickness of compression flange
Design strength under axial tension
Yielding strength of gross section
under axial tension
Rupture strength of net section under
axial tension
Design strength of bolt under axial
tension; Block shear strength at
end connection
Externally applied tension
Factored tension force of friction type
bolt
Limiting temperature of the steel
Nominal strength of bolt under axial
tension
Design tension capacity
9

IS 800:2007
Tndf
T,,,
T,
t
$
$
1pk
tq
t
t,
t
;
v,
vhf
v,,
Vd
vdb
Vnb
v,,,
Vp
v,
vnpb
vmb
v,,,
v,
V,h
v,,,
V,d,
v,,
v,
v,,
w
w
Wtf
.Xt
z,
z,,
.
—
—
—
.
—
—
.
—
—
—
—
—
—
.
—
.
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
Design tension capacity of friction
type bolt
Nominal tensile strength of friction
type bolt
Actual tension under service load
Thickness of element/angle, time in
minutes
Thickness of flange
Thickness of plate
Thickness of packing
Thickness of stiffener
Thickness of base slab
Effective throat thickness of welds
Thickness of web,
Factored applied shear force
Shear in batten plate
Factored frictional shear force in
friction type connection
Critical shear strength corresponding
to web buckling
Design shear strength
Block shear strength
Nominal shear strength of bolt
Bearing capacity of bolt for friction
type connection
Plastic shear resistance under pure
shear
Nominal shear strength
Nominal bearing strength of bolt
Nominal shear capacity of a bolt
Nominal shear capacity of bolt as
governed by slip in friction type
connection
Transverse shear at service load
Factored shear force in the bolt
Design shear capacity
Design shear strength in friction type
bolt
Factored design shear force of
friction bolts
Applied transverse shear
Shear resistance in tension field
Total load
Uniform pressure from below on the
slab base due to axial compression
under the factored load
Width of tension field
Torsional index
Elastic section modulus
Elastic section modulus of the
10
z,., —
Zp —
z“ —
Y, —
Y, —
ct—
q —
!-34 –
Lfyl ELI, —
ILL,
x
Xm
Xcr
6
a,
6P
q
$
Y
x
Y.
Y.10
x,,,
‘inb
X“,
—
—
.
—
—
—
—
—
—
—
.
—
—
—
—
—
member with respect to extreme
compression fibre
Elastic section modulus of the
member with respect to extreme
tension flbre
Plastic section modulus
Contribution to the plastic section
modulus of the total shear area of the
cross-section
Distance between point of application
of the load and shear centre of
the cross-section
Co-ordinate of the shear centre in
respect to centroid
Imperfection factor for buckling
strength in columns and beams
Coefficient of thermal expansion
Ratio of smaller to the larger bending
moment at the ends of a beam
column
Equivalent uniform moment factor
for flexural buckling for y-y and z-z
axes respectively
Equivalent uniform moment factor
for lateral torsional buckling
Strength reduction factor to account
for buckling under compression
Strength reduction factor, X, at~,n
Strength reduction factor to account
for lateral torsional buckling of
beams
Storey deflection
Horizontal deflection of the bottom
of storey due to combined gravity
and notional load
Load amplification factor
Horizontal deflection of the top of
storey due to combined gravity and
notional load
Inclination of the tension field stress
in web
Unit weight of steel
Partial safety factor for load
Partial safety factor for material
Partial safety factor against yield
stress and buckling
Partial safety factor against ultimate
stress
Partial safety factor for bolted
connection with bearing type bolts
Partial safety factor for bolted
connection with High Strength
Friction Grip bolts

Yff,
Ymft
Y
mv
1’
m.
&
A
A,,
:T
L,,r
P
P,
P,
/’4
e
P
‘r
Tb
T*b
rCr,e
7,
‘rf, Max
‘rfd
‘rf.
‘r,
v
r
—
—
—
—
—
Partial safety factor for fatigue load
Partial safety factor for fatigue
strength
Partial safety factor against shear
failure
Partial safety factor for strength of
weld
Yield stress ratio (250 /~,) ‘n
— Non-dimensional slenderness ratio =
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
@ii7FE. a =
w
Elastic buckling load factor
Equivalent slenderness ratio
Non-dimensional slenderness ratio in
lateral bending
Elastic buckling load factor of each
storey
Poisson’s ratio
Correction factor
Coefficient of friction (slip factor)
Capacity reduction factor
Ratio of the rotation at the hinge point
to the relative elastic rotation of the
far end of the beam segment
containing plastic hinge
Unit mass of steel
Actual shear stress range for the detail
category
Buckling shear stress
Permissible shear stress at the service
load
Elastic critical shear stress
Fatigue shear stress range
Highest shear stress range
Design shear fatigue strength
Fatigue shear stress range at N~Ccycle
for the detail category
Actual shear stress at service load
Ratio of the moments at the ends of
the laterally unsupported length of
a beam
Frame buckling load factor
NOTE — The subscripts y, : denote the y-y and Z-Zaxes of the
section, respectively. For symmetrical sections, y-y denotes the
minor principal axis whilst z-z denotes the major principal axis
(see 1.8).
1.5 Units
For the purpose of design calculations the following
units are recommended:
IS 800:2007
a) Forces and loads, in kN, kN/m, kN/m2;
b) Unit mass, in kg/mJ;
c) Unit weight, in kN/ms;
d) Stresses and strengths, in N/mm* (MN/m2 or
MPa); and
e) Moments (bending, etc), in kNm.
For conversion of one system of units to another
system, IS 786 (Supplement) may be referred.
1.6 Standard Dimensions, Form and Weight
The dimensions, form, weight, tolerances of all rolled
shapes, all rivets, bolts, nuts, studs, and welds and other
members used in any steel structure shall conform to
IS 808 and IS 1852, wherever applicable.
1.7 Plans and Drawings
1.7.1 Plans, drawings and stress sheet shall be prepared
according to IS 8000 (Parts 1 to 4), IS 8976 and IS 962.
1.7.1.1 Plans
The plans (design drawings) shall show the sizes,
sections, and the relative locations of the various
members. Floor levels, column centres, and offsets
shall be dimensioned. Plans shall be drawn to a scale
large enough to convey the information adequately.
Plans shall indicate the type of construction to be
employed; and shall be supplemented by such data on
the assumed loads, shears, moments and axial forces
to be resisted by all members and their connections, as
may be required for the proper preparation of shop
drawings. Any special precaution to be taken in the
erection of structure, from the design consideration
shall also be indicated in the drawing.
1.7.1.2 Shop drawings
Shop drawings, giving complete information
necessary for the fabrication of the component parts
of the structure including the location, type, size,
length and detail of all welds and fasteners shall be
prepared in advance of the actual fabrication. They
shall clearly distinguish between shop and field rivets,
bolts and welds. For additional information to be
included on drawings for designs based on the use of
welding, reference shall be made to appropriate Indian
Standards. Shop drawings shall be made in
conformity with IS 962. A marking diagram allotting
distinct identification marks to each separate part of
steel work shall be prepared. The diagram shall be
sufficient to ensure convenient assembly and erection
at site.
1.7.2 Symbols used for welding on plans and shop
drawings shall be according to IS 813.
11

IS 800:2007
1.8 Convention for Member Axes
Unless otherwise specified convention used for
member axes is as follows (see Fig. l):
a) x-.x along the member.
b) y-y an axis of the cross-section.
1) perpendicular to the flanges, and
2) perpendicular to the smaller leg in an
angle section.
c) Z-Z an axis of the cross-section
1) axis parallel to flanges, and
2) axis parallel to smaller leg in angle
section.
d) u-u major axis (when it does not coincide with
z-z axis).
e) v-v minor axis (when it does not coincide with
y-y axis).
SECTION 2
MATERIALS
2.1 General
The material properties given in this section are
nominal values, to be accepted as characteristic values
in design calculations.
2.2 Structural Steel
2.2.1 The provisions in this section are applicable to
the steels commonly used in steel construction, namely,
structural mild steel and high tensile structural steel.
2.2.2 All the structural steel used in general
construction, coming under the purview of this standard
shall before fabrication conform to IS 2062.
2.2.3 Structural steel other than those specified in 2.2.2
may also be used provided that the permissible stresses
and other design provisions are suitably modified and
the steel is also suitable for the type of fabrication
adopted.
~Y
I
i
;
Ziz
----- ,------ .
i
i
i
iY
I
2.2.3.1 Steel that is not supported by mill test result
may be used only in unimportant members and details,
where their properties such as ductility and weldability
would not affect the performance requirements of the
members and the structure as a whole.
However, such steels may be used in structural system
after confirming their quality by carrying out
appropriate tests in accordance with the method
specified in IS 1608.
2.2.4 Properties
The properties of structural steel for use in design, may
be taken as given in 2.2.4.1 and 2.2.4.2.
2.2.4.1 Physical properties of structural steel
irrespective of its grade may be taken as:
a)
b)
c)
d)
e)
Unit mass of steel, p = 7850 kg/m~
Modulus of elasticity, E = 2.0 x 10s N/mm2
(MPa)
Poisson ratio, p = 0.3
Modulus of rigidity, G = 0.769 x 10s N/mm2
(MPa)
Co-efficient of thermal expansion cx.= 12 x
10’ /“c
2.2.4.2 Mechanical properties of structural steel
The principaI mechanical properties of the structural
steel important in design are the yield stress, fy; the
tensile or ultimate stress, fu; the maximum percent
elongation on a standard gauge length and notch
toughness. Except for notch toughness, the other
properties are determined by conducting tensile tests
on samples cut from the plates, sections, etc, in
accordance with IS 1608. Commonly used properties
for the common steel products of different
specifications are summarized in Table 1.
2.3 Rivets
2.3.1 Rivets shall be manufactured from steel
Y! y’
‘Y
FIG. 1 AXM OFMEMBERS
12

IS 800:2007
Table 1 Tensile Properties of Structural Steel Products
(Clauses 1.3.113, 1.3.119 and 2.2.4.2)
sl Indian Grade/Classification Properties
No. Standard
F >
Yield Stress Ultimate Tensile Stress Elongation,
MI%,&tin hfPa. .%% Percent,
Min
(1) (2) (3) (4) (5} (6)
i) 1S513
{
ii) lS 814
1
0
D
DD
EDD
EX40XX
EX41xx
EX42XX
EX43XX
EX44XX
Exwxx
lh5 Ixx
EX52XX
EX53XX
lsx54xx
EX55XX
EX36XX
o
D
DD
EDD
[
3.6
4.6
4.8
5.6
1
5.8
6.8
iv) IS 1367
(Part 3)
8.8 (d< 16 mm)
8.8 (d> 16 mm)
9.s
[
10.9
12.9
(
1
1A
2
1
2A
3
V) 1S 1875
3A
4
5
6
vi) IS i 990
{
s, 37
S, 42
{
1
vii) IS 2002 2
3
—
280
250
2Z0
330
330
330
330
330
360
360
360
360
360
360
360
—
—
—.
—
--
—
—
—
640 ‘)
660 ‘)
720 ‘)
940 ‘)
i 100’)
200
220
230
250
270
280
320
350
370
dor(
A
r- -1
520 >20
220 200
250 240
t
A
,= ?
<16 >16 and >40 and >60 and >100 and
S40 s60 <1oo <350
270-410
270-370
270-350
410-540
410-540
410-540
410-540
410-540
510-610
510-610
510-610
510-6!0
510-610
S1O-61O
510-610
—
240-400
260-390
260-380
330
400
420
500
520
600
800
830
900
1040
1220
370
410
430
460
490
540
620
710
740
—
28
32
35
16
20
22
24
24
16
18
18
20
20
20
20
—
25
28
32
25
22
—.
20
—
—
12
12
10
9
8
26
25
24
22
21
20
15
13
10
360-440 26
410-500 23
t
&
(
Go >60 and >100
Sloo and and
S350 S350
235 225 215 200 185 360-480 360-480 350-480 24 23
265 255 245 215 200 410-530410-530400-530 22 21
290 285 280 255 230 460-580 450-570440-570 21 20
13

IS 800:2007
Table 1 (Concluded)
SI Indian Grade/Classification Properties
No. Standard
YieldStress UltimateTensile Stress Elongation,
MPa, Min MPa, Min Pereent, Min
(1) (2) (3) (4) (5) (6)

E 165(Fe 290)
E250(Fe410W)A
E250(Fe 410 W)B
E250(Fe 410 W)C
viii) IS 2062 E 300 (Fe 440)
E 350 (Fe 490)
E 410 (Fe 540)
E 450 (Fe 570) D
E 450 (Fe 590) E
dort
~———l
<20 20-40 >40
165 165 165
250 240 230
250 240 230
250 240 230
300 290 280
350 330 320
410 390 380
450 430 420
450 430 420
dorr
290
410
410
410
440
490
540
570
590
23
23
23
23
22
22
20
20
20
{
1 s 25 >25 ands 50
ix) 1s 3039 11 230 220
11[
400-490 22
235 235 400-490
235
22
235 400-490 22
{
Grade 1 240 350-450 25
~) IS 6240
Grade 2 245 360-450 34
f Annealed Condition 160 330-410 30
xi) Is 7557
t
As-Drawn Condition I90 410-490 20
[
HFC 210/CDS 210 330 20
2! OIERW21O
{
HFC 240/CDS
xii) IS 9295 2401ERW240
[
HFC 310/CDS
3Io/ERw31 o
240
310
410 18
450 15
{
1 170 290 30
2 210 330 28
xiii) 1S10748 3 240 410 25
4 275 430 20
5 310 490 15
NOTES
1 Percent of elongation shall be taken over the gauge length 5.65 & where So= Original cross-sectional area of the test specimen.
2 Abbreviations: O = Ordinary, D = Drawing, DD = Deep Drawing, EDD = Extra Deep Drawing.
I) Stress at 0.2 percent non-proportional elongation, Min.
14

conforming to IS 7557. They may also be
manufactured from steel conforming to IS 2062
provided that the steel meets the requirements given
in IS 1148.
2,3.2 Rivets shall conform to IS 1929 and IS 2155 as
appropriate.
2.3.3 High Tensile Steel Rivets
High tensile steel rivets, shall be manufactured from
steel conforming to IS 1149.
2.4 Bolts, Nuts and Washers
Bolts, nuts and washers shall conform as appropriate
to IS 1363 (Parts 1 to 3), IS 1364 (Parts 1 to 5), IS 1367
(Parts 1 to 20), IS 3640, IS 3757, IS 4000, IS 5369,
IS 5370, IS 5372, IS 5374, IS 5624, IS 6610, IS 6623,
IS 6639, and IS 6649. The recommendations in IS 4000
shall be followed.
2.5 Steel Casting
Steel casting shall conform to IS 1030 or IS 2708.
2.6 Welding Consumable
2.6.1 Covered electrodes shall conform to IS 814 or
IS 1395, as appropriate.
2.6.2 Filler rods and wires for gas welding shall
conform to IS 1278.
2.6.3 The supply of solid filler wires for submerged
arc welding of structural steels shall conform to
IS 1387.
2.6.4 The bare wire electrodes for submerged arc
welding shall conform to IS 7280. The combination
of wire and flux shall satisfy the requirements of
IS 3613.
2.6.5 Filler rods and bare electrodes for gas shielded
metal arc welding shall conform to IS 6419 and
IS 6560, as appropriate.
2.7 Other Materials
Other materials used in association with structural steel
work shall conform to appropriate Indian Standards.
SECTION 3
GENERAL DESIGN REQUIREMENTS
3.1.1 Design Objective
The objective of design is the achievement of an
acceptable probability that structures will perform
satisfactorily for the intended purpose duriug the design
life. With an appropriate degree of safety, they should
sustain all the loads and deformations, during
IS 800:2007
construction and use and have adequate resistance to
certain expected accidental loads and tire. Structure
should be stable and have alternate load paths to prevent
disproportionate overall collapse under accidental
loading.
3.1.2 Methods of Design
3.1.2.1 Structure and its elements shall normally, be
designed by the limit state method. Account should be
taken of accepted theories, experimental information
and experience and the need to design for dumbi]ity.
Calculations alone may not produce Safe, serviceable
and durable structures. Suitable materials, quality
control, adequate detailing and good supervision are
equally important.
3.1.2.2 Where the limit states method cannot be
conveniently adopted; the working stress design (sef~
Section 11) may be used.
3.1.3 Design Process
Structural design, including design for durability,
construction and use should be considered as a whole.
The realization of design objectives requires
compliance with clearly defined standards for
materials, fabrication, erection and in-service
maintenance.
3.2 Loads and Forces
3.2.1 For the purpose of designing any element,
member or a structure, the following loads (actions)
and their effects shall be taken into account, where
applicable, with partial safety factors find combinations
(see 5.3.3):
a)
b)
c)
d)
e)
t]
g)
Dead loads;
Imposed loads (live load, crane load, snow
load, dust load, wave load, earth pressures,
etc);
Wind loads;
Earthquake loads;
Erection loads;
Accidental loads such as those due to blast,
impact of vehicles, etc; and
Secondary effects due to contraction or
expansion resulting from temperature
changes, differential settlements of the
structure as a whole or of its components,
eccentric connections, rigidity of joints
differing from design assumptions.
3.2.1.1 Dead loads should be assumed in design as
specified in 1S 875 (Part 1).
3.2.1.2 Imposed loads for different types of occupancy
and function of structures shall be taken as
recommended in IS 875 (Part 2). Imposed loads arising
15

IS 800:2007
from equipment, such as cranes and machines should
be assumed in design as per manufacturers/suppliers
data (see 3.5.4). Snow load shall be taken as per
IS 875 (Part 4).
3.2.1.3 Wind loads on structures shall be taken as per
the recommendations of IS 875 (Part 3).
3.2.1.4 Earthquake loads shall be assumed as per the
recommendations of IS 1893 (Part 1).
3.2.1.5 The erection loads and temperature effects shall
be considered as specified in 3.3 and 3.4 respectively.
3.3 Erection Loads
All loads required to be carried by the structure or any
part of it due to storage or positioning of construction
material and erection equipment, including all loads
due to operation of such equipment shall be considered
as erection loads. Proper provision shall be made,
including temporary bracings, to take care of all stresses
developed during erection. Dead load, wind load and
also such parts of the live load as would be imposed
on the stricture during the period of erection shall be
taken as acting together with the erection loads. The
structure as a whole and all parts of the structure in
conjunction with the temporary bracings shall be
capable of sustaining these loads during erection.
3.4 Temperature Effects
3.4.1 Expansion and contraction due to changes in
temperature of the members and elements of a structure
shall be considered and adequate provision made for
such effect.
3.4.2 The temperature range varies for different
localities and under different diurnal and seasonal
conditions. The absolute maximum and minimum
temperatures, which may be expected in different
localities of the country, may be obtained from the
Indian Metrological Department and used in assessing
the maximum variations of temperature for which
provision for expansion and contraction has to be made
in the structure.
3.4.3 The range of variation in temperature of the
building materials may be appreciably greater or lesser
than the variation of air temperature and is influenced
by the condition of exposure and the rate at which the
materials composing the structure absorb or radiate
heat. This difference in temperature variations of the
material and air shall be given due consideration. The
effect of differential temperature within an element or
member, due to part exposure to direct sunlight shall
also be considered.
3.4.4 The co-efficient of thermal expansion for steel is
as given in 2.2.4 .l(e).
3,5 Load Combinations
3.5.1 Load combinations for design purposes shall be
those that produce maximum forces and effects and
consequently maximum stresses and deformations.
The following combination of loads with appropriate
partial safety factors (see Table 4) maybe considered.
a) Dead load + imposed load,
b) Dead load + imposed load + wind or
earthquake load,
c) Dead load + wind or earthquake load, and
d) Dead load+ erection load.
NOTE — In the case of structures supporting crmres, imposed
loads shall include the crane effects as given in 3.5.4.
3.5.2 Wind load and earthquake loads shall not be
assumed to act simultaneously. The effect of each shall
be considered separately.
3,5.3 The effect of cranes to be considered under
imposed loads shall include the vertical loads,
eccentricity effects induced by the vertical loads,
impact factors, lateral (surge) and longitudinal
(horizontal) thrusts, not acting simultaneously, across
and along the crane rail, respectively [see 1S 875
(Part 2)].
3.5.4 The crane loads and their combinations to be
considered shall be as indicated by the customer. In
the absence of any specific indications, the load
combinations shall be in accordance with the
provisions in IS 875 (Part 2) or as given below:
a)
b)
c)
d)
Vertical loads with full impact from one
loaded crane or two cranes in case of tandem
operation, together with vertical loads without
impact from as many loaded cranes as may
be positioned for maximum effect, along with
maximum horizontal thrust from one crane
only or two in case of tandem operation;
Loads as specified in 3.5.4(a), subject to
cranes in maximum of any two bays of the
building cross-section shaIl be considered for
multi-bay multi-crane gantries;
The longitudinal thrust on a crane track rail
shall be considered for a maximum of two
loaded cranes on the track; and
Lateral thrust (surge) and longitudinal thrust
acting across and along the crane rail
respectively, shall be assumed not to act
simultaneously. The effect of each force, shall
however be investigated separately.
3.5.5 While investigating the effect of earthquake
forces, the resulting effect from dead loads of all cranes
parked in each bay, positioned to cause maximum effect
shall be considered.
16

‘“”” —–-—~
IS 800:2007
3.5.6 The crane runway girders supporting bumpers
shall be checked for bumper impact loads also, as
specified by the manufacturers.
3.5.7 Stresses developed due to secondary effects such
as handling; erection, temperature and settlement of
foundations, if any, shall be appropriately added to the
stresses calculated from the combination of loads stated
in 3.5.1, with appropriate partial safety factors.
3.6 Geometrical Properties
3.6.1 General
The geometrical properties of the gross and the
effective cross-sections of a member or part thereof,
shall be calculated on the following basis:
a)
b)
The properties of the gross cross-section shall
be calculated from the specified size of the
member or part thereof or read from
appr~priate tablet
The properties of the effective cross-section
shall be calculated by deducting from the area
of the gross cross-section, the following:
1) The sectional area in excess of effective
plate width, in case of slender sections
(see 3.7.2).
2) The sectional areas of all holes in the section
except for parts in compression. In case of
punched holes, hole size 2 mm in excess
of the actual diameter may be deducted.
3.7 Classification of Cross-Sections
3.7.1 Plate elements of a cross-section may buckle
locally due to compressive stresses. The local buckling
can be avoided before the limit state is achieved by
limiting the width to thickness ratio of each element
of a cross-section subjected to compression due to axial
force, moment or shear.
3.7.1.1 When plastic analysis is used, the members ihall
be capable of forming plastic hinges with sufficient
rotation capacity (ductility) without local buckling, to
enable the redistribution of bending moment required
before formation of the failure mechanism.
3.7.1.2 When elastic analysis is used, the member shall
be capable of developing the yield stress under
compression without local buckling.
3.7.2 On basis of the above, four classes of sections
are defined as follows:
a) Class 1 (Plastic) — Cross-sections, which
can develop plastic hinges and have the
rotation capacity required for failure of the
structure by formation of plastic mechanism.
The width to thickness ratio of plate elements
shall be less than that specified under Class 1
(Plastic), in Table 2.
b) Class 2 (Compact) — Cross-sections, which
can develop plastic moment of resistance, but
have inadequate plastic hinge rotation
capacity for formation of plastic mechanism,
due to local buckling. The width to thickness
ratio of plate elements shall be less than that
specified under Class 2 (Compact), but greater
than that specified under Class 1 (Plastic), in
Table 2.
c) Class 3 (Semi-compact) — Cross-sections,
in which the extreme fiber in compression can
reach yield stress, but cannot develop the
plastic moment of resistance, due to local
buckling. The width to thickness ratio of plate
elements shall be less than that specified under
Class 3 (Semi-compact), but greater than that
specified under Class 2 (Compact), in Table 2.
d) Class 4 (Slender) — Cross-sections in which
the elements buckle locally even before
reaching yield stress. The width to thickness
ratio of plate elements shall be greater than
that specified under Class 3 (Semi-compact),
in Table 2. In such cases, the effective sections
for design shall be calculated either by
following the provisions of IS 801 to account
for the post-local-buckling strength or by
deducting width of the compression plate
element in excess of the semi-compact section
limit.
When different elements of a cross-section fall under
different classes, the section shall be classified as
governed by the most critical element.
The maximum value of limiting width to thickness
ratios of elements for different classifications of
sections are given in Table 2.
3.7,3 Types of Elements
a)
b)
c)
17
Internal elements — These are elements
attached along both longitudinal edges to
other elements or to longitudinal stiffeners
connected at suitable intervals to transverse
stiffeners, for example, web of I-section and
flanges and web of box section.
Outside elements or outstands – These are
elements attached along only one of the
longitudinal edges to an adjacent element, the
other edge being free to displace out of plane,
for example flange overhang of an I-section,
stem of T-section and legs of an angle section.
Tapered elements — These maybe treated as
flat elements having average thickness as
defined in SP 6 (Part 1).

Table 2 Limiting Width to Thickness Ratio
(Clauses 3.’7.2 and 3.7.4)
.—
Compression Element
(1)
)utstandirig element of
compressionflange
P
t--
Ifrl is negative:
Webof an 1,
1or box Generally
iwtion
If r, is positive :
Axial compression
Webof a channel
4ngle, compression due to bending (Both criteria should
)e satisfied)
$ingle angle, or double angles with the components
;eparated, axial compression (All three criteria should be
;atistied)
lrtstanding leg of an angle in contact back-to-back in a
louble angle member
outstanding leg of an angle with its back in continuous
:ontactwith another component
$tem of a T-section, rolled or cut from a rolled I-or H-
;ection
hular hollow tube, including welded tube subjected to:
a) moment
b) axial compression
Ratio Class of Section
Class 1 Class’2
Class3
Plastic Compact
Semi-compact
(2) (3) (4) (5)
b/t~ 9.4& 10.5s 15.7E
b/If 8.4& 9.4& 13.6s
b/ tf 29.3s 33.5 &
42s
b/ ff Not applicable
C2YCw 84& 105s 126z
105.0&
dkq
84E 1+< 126.0&
1+~ 105$OC 1+ 2r*
dk+ but s 42E —
1+1.5~
but <426
but s 42.s
dtw Not applicable 42c
L//t. 42s 42c I 42E
b/t 9.4& lo.5& 15.7E
d/t 9.4 & 10.56 15.7&
b/t 15.7&
I Not applicable
I
15.7.$
(b?;)/t 25z
d/t I 9.4s I 10.5s I 15.7E
dlt 9.4& 10.5C 15.7&
D/t~ 8.4& 9.4.? 18.9e
D/f I 42.? I 52.? ] 146.#
D/t I Not applicable I 88/
NOTES
1Elements which exceed semi-compact limits are to be taken as of slender cross-section.
26= (250 /~) ’n.
3 Websshall be checked for shear buckling in accordance with 8,4.2 when d/t> 67E, where, b is the width of the element (may be
taken as clear distance between lateral supports or between lateral support and free edge, as appropriate), t is the thickness of
element, d isthe depth of the web, D is the outer diameter of the element (see Fig. 2,3.7.3 and 3.7.4).
4 Different elements of a cross-section can be in different classes. In such cases the section is classified based on the least
favorable classification.
5 The stress ratio r, and r~are defined as:
Actual average axial stress (negative if tensile)
r, =
Design compressive stress of web alone
Actual average axial stress (negative if tensile)
r2=
Design compressive stress of ovedl section
18

——
IS 800:2007
The design of slender compression element (Class 4)
considering the strength beyond elastic local buckling
of element is outside the scope of this standard.
Reference may be made to IS 801 for such design
provisions. The design of slender web elements may
be made as given in 8.2.1.1 for flexure and 8.4.2.2 for
shear,
tf
CIE
d
tw
L-d
ROLLEDBEAMS
ANDCOLUMNS
SINGLEANGLES
t,
1
l---u
be b, ‘f
--ml
T
+
d
L ,t
tf
iE
r tw
h
L
b
ROLLED
CHANNELS
r%?
r-f
d
T
~t
TEES
3.7.4 Compound Elements in Built-up Section
(see Fig. 2)
In case of compound elements consisting of two or
more elements bolted or welded together, the limiting
width to thickness ratios as given in Table 2 should be
considered on basis of the following:
l-=---i
u
D d
b--
m
D d
RECTANGULAR CIRCULAR
HOLLOW HOLLOW
SECTIONS SECTIONS
DOUBLEANGLES
(BACKTO BACK)
t,
T
rbl
d tw
l!
BUILT-UP
SECTIONS
COMPOUNDELEMENTS
bi — Internal Element Width
b, — External Element Width
FIG. 2 DIMENSIONS
OFSECTIONS
19

IS 800:2007
a) Outstanding width ofcompound element (b,)
to its own thickness.
b) The internal width of each added plate
between the lines of welds or fasteners
connecting it to the original section to its own
thickness.
c) Any outstand of the added plates beyond the
line of welds or fasteners connecting it to
original section to its own thickness.
3.8 Maximum Effective Slenderness Ratio
The maximum effective slenderness ratio, KZlr values
of a beam, strut or tension member shall not exceed
those given in Table 3. ‘KL’ is the effective length of
the member and ‘r‘ is appropriate radius of gyration
based on the effective section as defined in 3.6.1.
Table 3 Maximum Values of Effective
Slenderness Ratios
s} Member Maximum
No. Effective
Slenderness
Ratio
(KU-)
(1) (2) (3)
i)
ii)
iii)
iv)
v)
vi)
A member carrying compressive loads 180
resulting from dead loads and imposed
loads
A tension member in which a reversal 180
of direct stress occurs due to loads other
than wind or seismic forces
A member subjected to compression 250
forces resulting only from combination
with wind/earthquake actions, provided
the deformation of such member does
not adversely affect tbe stress in any
part of the structure
Compression flange of a beam against 300
lateral torsional buckling
A member normally acting m a tie in a 350
roof truss or a bracing system not
considered effective when subject to
possible reversal of stress into
compression resulting from the action
of wind or earthquake forces]]
Members always under tension’) (other 400
than pre-tensioned members)
I) Tension members, such as bracing’s, pre-tensioned to avoid
sag, need not satisfy tbe maximum slenderness ratio limits.
3.9 Resistance to Horizontal Forces
3.9.1 In designing the steel frame work of a building,
provision shall be made (by adequate moment
connections or by a system of bracing) to effectively
transmit to the foundations all the horizontal forces,
giving due allowance for the stiffening effect of the
walls and floors, where applicable.
3.9.2 When the walls, or walls and floors and/or roofs
20
are capable of effectively transmitting all the horizontal
forces directly to the foundations, the structural steel
framework may be designed without considering the
effect of wind or earthquake.
3.9.3 Wind and earthquake forces are reversible and
therefore call for rigidity and strength under force
reversal in both longitudinal and transverse directions.
To resist torsional effects of wind and earthquake
forces, bracings in plan should be provided and
integrally connected with the longitudinal and
transverse bracings, to impart adequate torsional
resistance to the structure.
3.9.3.1 In shed type steel mill buildings, adequate
bracings shall be provided to transfer the wind or
earthquake loads from their points of action to the
appropriate supporting members. Where the
connections to the interior columns or frames are
designed such that the wind or earthquake loads will
not be transferred to the interior columns, the
exterior columns or frames shall be designed to resist
the total wind or earthquake loads. Where the
connections to the interior columns and frames are
designed such that the wind or earthquake effects
are transferred to the interior columns also, and
where adequate rigid diaphragm action can be
mobilized as in the case of the cast-in place RC slab,
both exterior and interior columns and frames may
be designed on the assumption that the wind or
earthquake load is divided among them in proportion
to their relative stiffness. Columns also should be
designed to withstand the net uplifting effect caused
by excessive wind or earthquake. Additional axial
forces arising in adjacent columns due to the vertical
component of bracings or due to frame action shall
also be accounted for.
3.9.3.2 Earthquake forces are proportional to the
seismic mass as defined in IS 1893. Earthquake forces
should be applied at the centre of gravity of all such
components of mass and their transfer to the foundation
should be ensured. Other construction details,
stipulated in IS 4326 should also be followed.
3.9.3.3 In buildings where high-speed traveling cranes
are supported or where a building or structure is
otherwise subjected to vibration or sway, triangulated
bracing or rigid portal systems shall be provided to
reduce the vibration or sway to an acceptable
minimum.
3.9.4 Foundations
The foundations of a building or other structures shall
be designed to provide the rigidity and strength that
has been assumed in the analysis and design of the
superstructure.

IS 800:2007
3.9.5 Eccentrically Placed Loads
Where a wall, or other gravity load, is placed
eccentrically upon the flange of a supporting steel
beam, the beam and its connections shall be designed
for torsion, unless the beam is restrained laterally in
such a way as to prevent the twisting of the beam.
3.10 Expansion Joints
3.10.1 In view of the large number of factors involved
in deciding the location, spacing and nature of
expansion joints, the decision regarding provision of
expansion joints shall be left to the discretion of the
designer.
3.10.2 Structures in which marked changes in plan
dimensions take place abruptly, shall be provided with
expansion joints at the section where such changes
occur. Expansion joints shall be so provided that the
necessary movement occurs with minimum resistance
at the joint. The gap at the expansion joint should be
such that:
a)
b)
It accommodates the expected expansion
contraction due to seasonal and durinal
variation of temperature, and
It avoids pounding of adjacent units under
earthquake. The structure adjacent to the joint
should preferably be supported on separate
columns but not necessarily on separate
foundations.
3.10.3 The details as to the length of a structure where
expansion jdints have to be provided may be
determined after taking into consideration various
factors such as temperature, exposure to weather and
structural design. The provisions in 3.10.3.1 to 3.10.3.3
are given as general guidance.
3.10.3.1 If one bay of longitudinal bracing is provided
at the centre of the building or building section, the
length of the building section may be restricted to
180 m in case of covered buildings and 120 m in case
of open gantries (see Fig. 3).
L--.-——,,om~
END OF COVERED BUILDING/SECTION
FIG. 3 MAXIMUMLENGTHOF BUILDINGWITHONE
BAYOFBRACING
3.10.3.2 If more than one bay of longitudinal bracing
is provided near the centre of the buildinglsection, the
maximum centre line distance between the two lines
of bracing may be restricted to 50 m for covered
buildings (and 30 m for open gantries) and the
maximum distance between the centre of the bracing
to the nearest expansion jointiend of building or section
may be restricted to 90 m (60 m in case of open
gantries). The maximum length of the building section
thus may be restricted to 230 m for covered buildings
(150 m for open gantries). Beyond this, suitable
expansion joints shall be provided (see Fig. 4).
3.10.3.3 The maximum width of the covered building
section should preferably be restricted to 150 m beyond
which suitable provisions for the expansion joint may
be made.
3.10.4 When the provisions of these sections are met
for a building or open structure, the stress analysis due
to temperature is not required.
+ EXPANSION
JOINT
i
i
i
i
: ‘D
i
—90m —50m~ “ 90 m
I
FIG. 4 MAXIMUMLENGTHOFBUILDING/SECTION
WITHTwo BAYSOFBRACINGS
21

IS 800:2007
SECTiON 4
METHODS OF STRUCTURAL ANALYSIS
4.1 Methods of Determining Action Effects
4.1.1 General
For the purpose of complying with the requirements
of the limit states of stability, strength and serviceability
specified in Section 5, effects of design actions on a
structure and its members and connections, shall be
determined by structural analysis using the assumptions
of 4.2 and 4.3 and one of the following methods of
analysis:
a)
b)
c)
d)
Elastic analysis in accordance with 4.4,
Plastic analysis in accordance with 4.5,
Advanced analysis in accordance with
Annex B, and
Dynamic analysis in accordance with IS 1893
(Part 1).
The design action effects for design basis earthquake
loads shall be obtained only by an elastic analysis. The
maximum credible earthquake loads shall be assumed
to correspond to the load at which significant plastic
hinges are formed in the structure and the
corresponding effects shall be obtained by plastic or
advanced analysis. More information on analysis and
design to resist earthquake is given in Section 12 and
IS 1893 (Part 1).
4.1.2 Non-sway and Sway Frames
For the purpose of analysis and design, the structural
frames are classified as non-sway and sway frames as
given below:
a)
b)
c)
Non-sway frame — One in which the
transverse displacement of one end of the
member relative to the other end is effectively
prevented. This applies to triangulated frames
and trusses or to frames where in-plane
stiffness is provided by bracings, or by shear
walls, or by floor slabs and roof decks secured
horizontally to walls or to bracing systems
parallel to the plane of loading and bending
of the frame.
Sway frame — One in which the transverse
displacement of one end of the member
relative to the other end is not effectively
prevented. Such members and frames occur
in structures which depend on flexural action
of members to resist lateral loads and sway,
as in moment resisting frames.
A rigid jointed multi-storey frame may be
considered as a non-sway frame if in every
individual storey, the deflection 6, over a
storey height h,, due to the notional horizontal
loading given in 4.3.6 satisfies the following
criteria:
1) For clad frames, when the stiffening
effect of the cladding is not taken into
account in the deflection calculations:
65A
2 000
2) For unclad frame or clad frames, when
the stiffening effect of the cladding is
taken into account in the deflection
calculations:
65A
4000
3) A frame, which when analyzed
considering all the lateral supporting
system does not comply with the above
criteria, should be classified as a sway
frame. even if it is braced or otherwise
laterally stiffened.
4.2 Forms of Construction Assumed for Structural
Analysis
4.2.1 The effects of design action in the members and
connections of a structure shall be determined by
assuming singly or in combination of the following
forms of construction (see 10.6.1).
4.2.1.1 Rigid construction
In rigid construction, the connections between
members (beam and column) at their junction shall be
assumed to have sufficient rigidity to hold the original
angles between the members connected at a joint
unchanged under loading.
4.2S.2 Semi-rigid construction
In semi-rigid construction, the connections between
members (beam and column) at their junction may not
have sufficient rigidity to hold the original angles
between the members at a joint unchanged, but shall
be assumed to have the capacity to furnish a dependable
and known degree of flexural restraint. The relationship
between the degree of flexural restraint and the level
of the load effects shall be established by any rational
method or based on test results (see Annex F).
4.2.1.3 Simple construction
In simple construction, the connections between
members (beam and column) at their junction will not
resist any appreciable moment and shall be assumed
to be hinged.
4.2.2 Design of Connections
The design of all connections shall be consistent with
22

the form of construction, and the behaviour of the
connections shall not adversely affect any other part
of the structure beyond what is allowed for in design.
Connections shall be designed in accordance with
Section 10.
4.3 Assumptions in Analysis
4.3.1 The structure shall be analyzed in its entirety
except as follows:
a)
b)
c)
Regular building structures, with orthogonal
frames in plan, may be analyzed as a series
of parallel two-dimensional sub-structures
(part of a structure), the analysis being carried
out in each of the two directions, at right
angles to each other, except when there is
significant load redistribution between the
sub-structures (part of a structure). For
earthquake loading three dimensional analysis
may be necessary to account for effects of
torsion and also for multi-component
earthquake forces [see IS 1893 (Part 1)].
For vertical loading in a multi-storey building
structure, provided with bracing or shear walls
to resist all lateral forces, each level thereof,
together with the columns immediately above
and below, may be considered as a sub-
structure, the columns being assumed fixed
at the ends remote from the level under
consideration.
Where beams at a floor level in a multi-bay
building structure tu-e considered as a sub-
structure (part of a structure), the bending
moment at the support of the beam due to
gravity loads may be determined based on the
assumption that the beam is fixed at the i%
end support, one span away from the span
under consideration, provided that the floor
beam is continuous beyond that support point.
4.3.2 Spun Length
The span length of a flexural member iu a continuous
frame system shall be taken as the dlsiance between
centre-to-centre of the supports.
4.3.3 Arrangements of Imposed Loads in Bui[ding.s
For building structures, the various arrangements of
imposed loads considered for the analysis, shall include
at least the following:
a)
b)
Where the loading pattern is fixed, the
arrangement concerned.
Where the imposed load is variable and not
greater than three-quarters of the dead load,
the live load may be taken to be acting on all
spans.
IS 800:2007
c) Where the imposed load is variable and
exceeds three-quarters of the dead load,
arrangements of live load acting on the floor
under consideration shall include the
following cases:
1) Imposed load on alternate spans,
2) Imposed load on two adjacent spans, and
- 3) Imposed load on all the spans.
4.3.4 Base Sti@ess
In the analysis of all structures the appropriate base
stiffness about the axis under consideration shall be
used. In the absence of the knowledge of the pedestal
and foundation stiffness, the following may be
assumed:
a)
b)
c)
d)
When the column is rigidly connected to a
suitable foundation, the stiffness of the
pedestal shall be taken as the stiffness of the
column above base plate. However in case of
very stiff pedestals and foundations the
column may be assumed as fixed at base.
When the column is nominally connected
to the foundation, a pedestal stiffness of
10 percent of the column stiffness may be
assumed.
When an actual pin or rocker is provided in
the connection between the steel column and
pedestal, the column is assumed as hinged at
base and the pedesrdl and foundation maybe
appropriately designed for the reactions from
the column.
In case of (a) and (b), the bottom of the
pedestal shall be assumed to have the
following boundary condition in the absence
of any derailed procedure based on theory or
tests:
1)
2)
3)
When the foundation consist of a group
of piles with a pile cap, raft foundation
or an isolated footing resting on rock or
very hard soil, the pedestal shall be
assumed to be fixed at the level of the
bottom of footing or at the top of pile
cap.
When the foundation consist of an
isolated footing resting on other soils,
pedestal shall be assumed to be hinged
at the level of the bottom of footing.
When the pedestal is supported by a
single pile, which is laterally surrounded
by soil providing passive resistance, the
pile shall be assumed to be fixed at a
depth of 5 times the diameter of the pile
23

IS 800:2007
below the ground level in case of compact
ground or the top level of compact soil
in case of poor soil overlying compact
soil.
4) When the column is founded into rock,
it may be assumed to be fixed at the
interface of the column and rock.
4.3.5 Simple Construction
Bending members may be assumed to have their ends
connected for shear only and to be free to rotate. In
triangulated structures, axial [orces maybe determined
by assuming that all members are pin connected. The
eccentricity for stanchion and column shall be assumed
in accordance with 7.3.3.
4.3.6 Notional Horizontal Loads
To analyze a frame subjected to gravity loads,
considering the sway stability of the frame, notional
horizontal forces should be applied. These notional
horizontal forces account for practical imperfections
and should be taken at each level as being equal to 0.5
percent of factored dead load plus vertical imposed
loads applied at that level. The notional load should
not be applied along with other lateral loads such as
wind and earthquake loads in the analysis.
4.3.6.1 The notional forces should be applied on the
whole structure, in both orthogonal directions, in one
direction at a time, at roof and all floor levels or their
equivalent, They should be taken as acting
simultaneously with factored gravity loads.
------ . . . . .
4.3.6 ..4
a)
b)
c)
d)
1he nohonal force should nOt be,
applied when considering overturning or
overall instability;
combined with other horizontal (lateral)
loads;
combined with temperature effects; and
taken to contribute to the net shear on the
foundation.
4.3.6.3 The sway effect using notional load under
gantry load case need not be considered if the ratio of
height to lateral width of the building is less than unity.
4,4 Elastic Analysis
4.4.1 Assumptions
Individual members shall be assumed to remain elastic
under the action of the factored design loads for all
limit states.
The effect of haunching or any variation of the cross-
section along the axis of a member shall be considered,
and where significant, shall be taken into account in
the determination of the member stiffness,
4.4.2 First-Order Elastic Analysis
In a first-order elastic analysis, the equilibrium of the
frame in the undeformed geometry is considered, the
changes in the geometry of the frame due to the loading
are not accounted for, and changes in the effective
stiffness of the members due to axial force are
neglected. The effects of these on the first-order
bending moments shall be allowed for by using one of
the methods of moment amplification of 4.4.3.2
or 4.4.3.3 as appropriate. Where the moment
amplification factor CY, CZ, calculated in accordance
with 4.4.3.2 or 4.4.3.3 as appropriate, is greater than
1.4, a second-order elastic analysis in accordance with
Annex B shall be carried out.
4.4.3 Second-Order Elastic Analysis
4.4.3.1 The analysis shall allow for the effects of the
design loads acting on the structure and its members
in their displaced and deformed configuration. These
second-order effects shall be taken into account by
using eithe~
a) A first-order elastic analysis with moment
amplification in accordance with 4.4.2,
provided the moment amplification factors,
C, and C, are not greater than 1.4; or
b) A second-order elastic analysis in accordance
with Annex B.
4.4.3.2 Moment amplification for members in non-sway
frames
For a member with zero axial compression or a member
subject to axial tension, the design bending moment is
that obtained from the first order analysis for factored
loads, without any amplification.
For a braced member with a design axial compressive
force P~ as determined by the first order analysis, the
design bending moment shall be calculated considering
moment amplification as in 9.3.2.2.
4.4.3.3 Moment amplification for members in sway
frames
The design bending moment shall be calculated as the
product of moment amplification factor [see 9.3.2.2
(C~Y, Cm,)] and the moment obtained from the first
order analysis of the sway frame, unless analysis
considering second order effects is carried out
(see 4.4.3).
4.4.3.4 The calculated bending moments from the first
order elastic analysis may be modified by redistribution
upto 15 percent of the peak calculated moment of the
member under factored load, provided that:
a) the internal forces and moments in the
24

members of the frame are in equilibrium with
applied loads.
b) all the members in which the moments are
reduced shall belong to plastic or compact
section classification (see 3.7).
4.5 Plastic Analysis
4.5.1 Application
The effects of design action throughout or on part of a
structure may be determined by a plastic analysis,
provided that the requirements of 4.5.2 are met. The
distribution of design action effects shall satisfy
equilibrium and the boundary conditions.
4.5.2 Requirements
When a plastic method of analysis is used, all of the
following conditions shall be satisfied, unless adequate
ductility of the structure and plastic rotation capacity
of its members and connections are established for the
design loading conditions by other means of evaluation:
a)
b)
c)
d)
e)
f)
$4
The yield stress of the grade of the steel used
shall not exceed 450 MPa.
The stress-strain characteristics of the steel
shall not be significantly different from those
obtained for steels complying with IS 2062
or equivalent and shall be such as to ensure
complete plastic moment redistribution. The
stress-strain diagram shall have a plateau at
the yield stress, extending for at least six times
the yield strain. The ratio of the tensile
strength to the yield stress specified for the
grade of the steel shall not be less than 1.2.
The elongation on a gauge length complying
with IS 2062 shall not be than 15 percent, and
the steel shall exhibit strain-hardening
capability. Steels conforming to IS 2062 shall
be deemed to satisfy the above requirements.
The members used shall be hot-rolled or
fabricated using hot-rolled plates and sections.
The cross-section of members not containing
plastic hinges should be at least that of
compact section (see 3.7.2), unless the
members meet the strength requirements from
elastic analysis.
Where plastic hinges occur in a member, the
proportions of its cross-section should not
exceed the limiting values for plastic section
given in 3.7.2.
The cross-section should be symmetrical
about its axis perpendicular to the axis of the
plastic hinge rotation.
The members shall not be subject to impact
loading, requiring fracture assessment or
IS 800:2007
fluctuating loading, requiring a fatigue
assessment (see Section 13).
4.5.2.1 Restraints
If practicable, torsional restraint (against lateral
buckling) should be provided at all plastic hinge
locations. Where not feasible, the restraint should be
provided within a distance of D/2 of the plastic hinge
location, where D is the total depth of section.
The torsional restraint requirement at a section as
above, need not be met at the last plastic hinge to form,
provided it can be clearly identified.
Within a member containing a plastic hinge, the
maximum distance L~ from the restraint at the plastic
hinge to an adjacent restraint should be calculated by
any rational method or the conservative method given
below, so as to prevent lateral buckling.
Conservatively L~ (ht mm) may be taken as
where
f=
f, =
‘Y =
Xt =
A=
Iw, Iy, It =
actual compressive stress on the cross-
section due to axial load, in N/mm*;
yield stress, in N/mm2;
radius of gyration about the minor axis, in
mm;
torsional index, x, =1.132 (Alw/IylJ0”5;
area of cross-section; and
warping constant, second moment of the
cross section above the minor axes and
St. Venant’s torsion constant, respectively.
Where the member has unequal flanges, rY should be
taken as the lesser of the values of the compression
flange only or the whole section.
Where the cross-section of the member varies within
the length L~, the maximum value of rY and the
minimum value of xl should be used.
The spacing of restraints to member lengths not
containing a plastic hinge should satisfy the
recommendations of section on lateral buckling
strength of beams (see 8.2.2). Where the restraints are
placed at the limiting distance L~, no further checks
are required.
4.5.2.2 Stiffeners at plastic hinge locations
Web stiffeners should be provided where a concentrated
load, which exceeds 10 percent of the shear capacity
25

IS 800:2007
of the member, is applied within D2 of a plastic hinge
location (see 8.2.1.2). The stiffener should be provided
within a distance of half the depth of the member on
either side of the hinge location and be designed to
carry the applied load in accordance with 8.7.4. If the
stiffeners are flat plates, the outstand width to the
thickness ratio, b/t, should not exceed the values given
in the plastic section (see 3.7, Table 2). Where other
[)
I
m
sections are used the ratio ~
It
should not exceed
the values given for plastic section (for simple outstand,
as in 3.7);
where
Iso = second moment of area of the stiffener about
‘the face of the element perpendicular to the
web; and
I, = St. Venant’s torsion constant of the stiffener.
4.5.2.3 The frame shall be adequately supported against
sway and out-of-plane buckling, by bracings, moment
resisting frame or an independent system such as shear
wall.
4.5.2.4 Fabrication restriction
Within a length equal to the member depth, on either
side of a plastic hinge location, the following
restrictions should be applied to the tension flange and
noted in the design drawings. Holes if required, should
be drilled or else punched 2 mm undersize and reamed.
All sheared or hand flame cut edges should be finished
smooth by grinding, chipping or planning.
4.5.3 Assumptions in Analysis
The design action effects shall be determined using a
rigid-plastic analysis.
It shall be permissible to assume full strength or partial
strength connections, provided the capacities of these
are used in the analysis, and provided that
a) in a full strength connection, the moment
capacity of the connection shall be not less
than that of the member being connected;
b) in a partial strength connection, the moment
capacity of the connection may be less than
that of the member being connected; and
c) in both cases the behaviour of the connection
shall be such as to allow all plastic hinges
necessary for the collapse mechanism to
develop, and shall be such that the required
plastic hinge rotation does not exceed the
rotation capacity at any of the plastic hinges
in the collapse mechanism.
In the case of building structures, it is not normally
necessary to consider the effect of alternating plasticity.
4.5.4 Second-Order Elastic Analysis
Any second-order effects of the loads acting on the
structure in its deformed configuration may be
neglected, provided the following are satisfied:
a)
b)
For clad frames, provided the stiffening effects
of masonry infill wall panels or diaphragms of
profiled wall panel is not taken into account,
and where elastic buckling load factor, JC,
(see 4.6) satisfies J,jAP> 10.
[f10>2C{IP24,6 the second-order effects may
be considered by ampli~ing the design load
effects obtained from plastic analysis by a
factor 6,= {0.9 2,, /( 2=,- l)}.
If ACj JP < 4.6, second-order elasto-plastic
analysis or second-order elastic analysis
(see 4.4.3) is to be carried out.
For un-clad frames or for clad frames where
the stiffening effects of masonry infill or dia-
phragms of profiled wall panel is taken into
account, where elastic buckling load factor, 2<,
(see 4.6) satisfies J=j 2,220
If 20> AC]AP
25.75 the second-order effects
may be considered by ampli~ing the design
load effects obtained from plastic analysis by
a factor iSP= {0.9 2,,/( J,,–I)}.
If IC{ LP<5.75, second-order elasto-plastic
analysis or second-order elastic analysis
(see 4.4.3) shall be carried out.
4.6 Frame Buckling Analysis
4.6.1 The elastic buckling load factor ().C,)shall be the
ratio of the elastic buckling load set of the frame to the
design load set for the frame, and shall be determined
in accordance with 4.6.2.
NOTE— The value of lC, depends on the load set and has to
be evaluated for each possible set of load combination.
4.6.2 In-plane Frame Buckling
The elastic buckling load factor (hC,) of a rigid-jointed
frame shall be determined by using:
a) One of the approximate methods of 4.6.2.1
and 4.6.2.2 or
b) A rational elastic buckling analysis of the
whole frame.
4.6.2.1 Regular non-sway frames (see 4.1.2)
In a rectangular non-sway frame with regular loading
and negligible axial forces in the beams, the Euler
buckling stressfCC,for each column shall be determined
in accordance with 7.1.2.1. The elastic buckling load
factor (L,,) for the whole frame shall be taken as the
lowest of the ratio of (&/fed) for all the columns, where
26

fC~is the axial compressive stress in the column from
the factored load analysis.
4.6.2.2 Regular sway frames
In a rectangular sway frame with regular loading and
negligible axial forces in the beams, the buckling load,
PC,,,for each column shall be determined as P,, = A~C
wherefCCis the elastic buckling stress of the column in
the plane of frame, obtained in accordance with 7.1.2.1.
The elastic buckling load factor AC,,
for the whole frame
shall be taken as the lowest of all the ratios, k,,,,
calculated for each storey of the building, as given
below:
where
P=
L=
~ _ ~(PCC/L)
‘c’ - ~(P/L)
member axial force from the factored load
analysis, with tension taken as negative; and
column length and the summation includes
all columns in the plane frame within a
storey.
SECTION 5
LIMIT STATE DESIGN
5.1.1 In the limit state design method, the structure
shall be designed to withstand safely all loads likely to
act on it throughout its life. It shall not suffer total
collapse under accidental loads such as from explosions
or impact or due to consequences of human error to an
extent beyond the local damages. The objective of the
design is to achieve a structure that will remain fit for
use during its life with acceptable target reliability. In
other words, the probability of a limit state being
reached during its lifetime should be very low. The
acceptable limit for the safety and serviceability
requirements before failure occurs is called a limit state.
In general, the structure shall be designed on the basis
of the most critical limit state and shall be checked for
other limit states.
5.L2 Steel structures are to be designed and constructed
to satisfy the design requirements with regard to
stability, strength, serviceability, brittle fracture,
fatigue, fire, and durability such that they meet the
following:
a) Remain fit with adequate reliability and be
able to sustain all actions (loads) and other
influences experienced during construction
and use;
b) Have adequate durability under normal
maintenance;
c) Do not suffer overall damage or collapse
IS 800:2007
disproportionately under accidental events
like explosions, vehicle impact or due to
consequences of human error to an extent
beyond local damage. The potential for
catastrophic damage shall be limited or
avoided by appropriate choice of one or more
of the following:
1) Avoiding, eliminating or reducing
exposure to hazards, which the structure
is likely to sustain.
2) Choosing structural forms, layouts and
details and designing such that:
i) the structure has low sensitivity to
hazardous conditions; and
ii) the structure survives with only local
damage even after serious damage
to any one individual element by the
hazard.
3) Choosing suitable material, design and
detailing procedure, construction
specifications, and control procedures for
shop fabrication and field construction as
relevant to the particular structure.
The following conditions may be satisfied to avoid a
disproportionate collapse:
a) The building should be effectively tied
together at each principal floor level and each
column should be effectively held in position
by means of continuous ties (beams) nearly
orthogonal, except where the steel work
supports only cladding weighing not more
than 0.7 kN/m~ along with imposed and wind
loads. These ties must be steel members such
as beams, which may be designed for other
purposes, steel bar reinforcement anchoring
the steel frame to concrete floor or steel mesh
reinforcement in composite slab with steel
profiled sheeting directly connected to beam
with shear connectors. These steel ties and
their end connections should be capable of
resisting factored tensile force not less than
the factored dead and imposed loads acting
on the floor area tributary to the tie nor less
than 75 kN. Such connection of ties to edge
column should also be capable of resisting
1 percent of the maximum axial compression
in the column at the level due to factored dead
and imposed loads. All column splices should
be capable of resisting a tensile force equal
to the largest of a factored dead and live load
reaction from a single floor level located
between that column splice and the next
column splice below that splice. Lateral load
system to resist notional horizontal loads
prescribed in 4.3.6 should be distributed
27

IS 800:2007
b)
c)
throughout the building in nearly orthogonal
directions so that no substantial portions is
connected at only one point to such a system.
Precast concrete or other heavy floor or roof
units should be effectively anchored in the
direction of their span either to each other over
the support or directly to the support.
Where the above conditions to tie the columns
to the floor adequately are not satisfied each
storey of the building should be checked to
ensure that disproportionate collapse would
not precipitate by the notional removal, one
at a time, of each column.
Where each floor is not laterally supported
by more than one system, check should be
made at each storey by removing one such
lateral support system at a time to ensure that
disproportionate collapse would not occur.
The collapse is considered disproportionate,
if more than 15 percent of the floor or roof
area of 70 mz collapse at that level and at one
adjoining level either above or below it, under
a load equal to 1.05 or 0.9 times the dead load,
0.33 times temporary or full imposed load of
permanent nature (as in storage buildings) and
0.33 times wind load acting together.
5.1.3 Structures designed for unusual or special
functions shall comply with any other relevant
additional limit state considered appropriate to that
structure.
5.1.4 Generally structures and elements shall be
designed by limit state method. Where limit state
method cannot be conveniently adopted, working stress
design (see Section 11) may be used.
5.2 Limit State Design
5.2.1 For achieving the design objectives, the design
shall be based on characteristic values for material
strengths and applied loads (actions), which take into
account the probability of variations in the material
strengths and in the loads to be supported. The
characteristic values shall be based on statistical data,
if available. Where such data is not available, these
shall be based on experience. The design values are
derived from the characteristic values through the use
of partial safety factors, both for material strengths and
for loads. In the absence of special considerations, these
factors shall have the values given in this section
according to the material, the type of load and the limit
state being considered. The reliability of design is
ensured by satisfying the requirement:
Design action S Design strength
5.2.2 Limit states are the states beyond which the structure
no longer satisfies the performance requirements
specified. The limit states are classified as:
a) Limit state of strength; and
b) Limit state of serviceability.
t
5.2.2.1 The limit states of strength are those associated
with failures (or imminent failure), under the action of
probable and most unfavorable combination of loads
on the structure using the appropriate partial safety
factors, which may endanger the safety of life and
property. The limit state of strength includes:
a) Loss of equilibrium of the structure as a whole
or any of its parts or components.
b) Loss of stability of the structure (including
the effect of sway where appropriate and
overturning) or any of its parts including
supports and foundations.
c) Failure by excessive deformation, rupture of
the structure or any of its parts or components,
d) Fracture due to fatigue,
e) Brittle fracture.
5.2.2.2 The limit state of serviceability include:
a)
b)
c)
d)
e)
Deformation and deflections, which may
adversely affect the appearance or effective
use of the structure or may cause improper
functioning of equipment or services or may
cause damages to finishes and non-structural
members.
Vibrations in the structure or any of its
components causing discomfort to people,
damages to the structure, its contents or which
may limit its functional effectiveness. Special
consideration shall be given to systems
susceptible to vibration, such as large open
floor areas free of partitions to ensure that
such vibrations are acceptable for the intended
use and occupancy (see Annex C).
Repairable damage or crack due to fatigue.
Corrosion, durability.
Fire.
5.3 Actions
The actions (loads) to be considered in design include
direct actions (loads) experienced by the structure due
to self weight, external actions etc., and imposed
deformations such as that due to temperature and
settlements.
5.3.1 Classification ofActions
Actions are classified by their variation with time as
given below:
a) Permanent actions (Q ): Actions due to self-
!
weight of structura and non-structural
28

. ._,.___ —
b)
c)
components, fittings, ancillaries, and fixed
equipment, etc.
Variable actions (Qv): Actions due to
construction and service stage loads such as
imposed (live) loads (crane loads, snow loads,
etc.), wind loads, and earthquake loads, etc.
Accidental actions (Q,): Actions expected due
to explosions, and impact of vehicles, etc.
5.3.2 Characteristic Actions (Loads)
5.3.2.1 The Characteristic Actions, QC,are the values
of the different actions that are not expected to be
exceeded with more than 5 percent probability, during
the life of the structure and they are taken as:
a)
b)
c)
d)
the self-weight, in most cases calculated on
the basis of nominal dimensions and unit
weights [see 1S 875 (Part 1)].
the variable loads, values of which are
specified in relevant standard [see IS 875 (all
Parts) and IS 1893 (Part l)].
the upper limit with a specified probability
(usually 5 percent) not exceeding during some
reference period (design life).
specified by client, or by designer in
consultation with client, provided they satisfy
the minimum provisions of the relevant
loading standard.
5.3.2.2 The characteristic values of accidental loads
generally correspond to the value specified by relevant
code, standard or client. The design for accidental load
LS 800:2007
is generally not required in building unless it is required
by client or approving authority in which case,
generally recommendation in 5.1.2 c) or specialist
literature shall be followed.
5.3.3 Design Actions
The Design Actions, Q~,is expressed as Qd = ~?’. Q,k
k
where
yk = partial safety factor for different loads k,
given in Table 4 to account for:
a) Possibility of unfavorable deviation of
the load from the characteristic value,
b) Possibility of inaccurate assessment of
the load,
c) Uncertainty in the assessment of effects
of the load, and
d) Uncertainty in the assessment of the
limit states being considered.
The loads or load effects shall be multiplied by the
relevant ~f factors, given in Table 4, to get the design
loads or design load effects.
5.4 Strength
The ultimate strength calculation may require
consideration of the following:
a) Loss of equilibrium of the structure or any
part of it, considered as a rigid body; and
b) Failure by excessive deformation, rupture or
Table 4 Partial Safety Factors for Loads, y~,for Limit States
(Clauses 3.5.1 and 5.3.3)
Combination Limit State of Strength Limit State of Serviceability
F Y 7
“ ~ ‘“L “
T
“ & ‘m’
Leading Accompanying Accompanying
(1) (2) (3) (4) (5) (6) (7) (8) (9) (lo)
DL+LL+CL 1.5 1.5 1.05 — — 1.0 1.0 1.0 —
DL+LL+CL+ 1.2 1.2 1.05 0.6 — 1.0 0.8 0.8 0.8
WLJEL 1’.2 1.2 0.53 1.2
DL+WLfEL 1.5(0.9)2’ — — 1.5 — 1.0 — — 1.0
DL+ER 1.2 — — —— — — —
~~;)z)
DL+LL+AL 1.0 0.35 0.35 — 1.0 — — — —
‘)When action of different live loads is simultaneously considered, the leading live load shall be considered to be the one causing the
higher load effects in the member/section.
‘)This value is to be considered when the dead load contributes to stability against overturning is critical or the dead load causes
reduction in stress due to other loads.
Abbreviations:
DL= Dead load, LL= Imposed load (Live loads), WL = Wind load, CL = Crane load (VerticaVHorizontal), AL = Accidental load, ER =
Erection load, EL= Earthquake load.
NOTE — The effects of actions (loads) in terms of stresses or stress resultants may be obtained from an appropriate method of analysis
m in 4.
29

IS 800:2007
loss of stability of the structure or any part of
it including support and foundation.
5.4.1 Design Strength
The Design Strength, S~, is obtained as given below
from ultimate strength, SUand partial safety factors for
materials, y~ given in Table 5.
Sd=s,lym
where partial safety factor for materials, y~ account
for:
a)
b)
c)
d)
Possibility of unfavorable deviation of
material strength from the characteristic value,
Possibility of unfavorable variation of
member sizes,
Possibility of unfavorable reduction in
member strength due to fabrication and
tolerances, and
Uncertainty in the calculation of strength of
the members.
5.5 Factors Governing the Ultimate Strength
5.5.1 Stability
Stability shall be ensured for the structure as a whole
and for each of its elements. This should include,
overall frame stability against overturning and sway,
as given in 5.5.1.1 and 5.5.1.2.
5.5.1.1 Stability against overturning
The structure as a whole or any part of it shall be
designed to prevent instability due to overturning, uplift
or sliding under factored load as given below:
a)
b)
The Actions shall be divided into components
aiding instability and components resisting
instability.
The permanent and variable actions and their
effects causing instability shall be combined
using appropriate load factors as per the Limit
State requirements, to obtain maximum
destabilizing effect.
c)
d)
The permanent actions (loads) and effects
contributing to resistance shall be multiplied
with a partial safety factor 0.9 and added
together with design resistance (after
multiplying with appropriate partial safety
factor). Variable actions and their effects
contributing to resistance shall be disregarded.
The resistance effect shall be greater than or
equal to the destabilizing effect. Combination
of imposed and dead loads should be such as
to cause most severe effect on overall stability.
5.5.1.2 Sway stability
The whole structure, including portions between
expansion joints, shall be adequately stiff against sway.
To ensure this, in addition to designing for applied
horizontal loads, a separate check should be carried
out for notional horizontal loads such as given in 4.3.6
to evaluate the sway under gravity loads.
5.5.2 Fatigue
Generally fatigue need not be considered unless a
structure or element is subjected to numerous
significant fluctuations of stress. Stress changes due
to fluctuations in wind loading normally need not be
considered. Fatigue design shall be in accordance with
Section 13. When designing for fatigue, the partial
safety factor for load, yf,equal to unity shall be used
for the load causing stress fluctuation and stress range.
5.5.3 Plastic Collapse
Plastic analysis and design may be used, if the
requirement specified under the plastic method of
analysis (see 4.5) are satisfied.
5.6 Limit State of Serviceability
Serviceability limit state is related to the criteria
governing normal use. Serviceability limit state is limit
state beyond which the service criteria specified below,
are no longer met:
a) Deflection limit,
Table 5 Partial Safety Factor for Materials, y~
(Clause 5.4. 1)
SI Definition Partial Safety Factor
No.
i) Resistance, governed by yielding, Ymo 1.10
ii) Resistance of member to buckling, ymo 1.10
iii) Resistance, governed by ultimate stress, y~t 1.25
iv) Resistance of connection: ShopFabrications FieldFabrications
a) Bolts-Friction Type, y~r 1.25 1.25
b) Bolts-Bearing Type, ym~ 1.25 1.25
c) Rivets, Ym, 1.25 1.25
d) Welds, ymW 1.25 1.50
30

IS 800:2007
b) Vibration limit,
c) Durability consideration, and
d) Fire resistance.
Unless specified otherwise, partial safety factor for
loads, y~,of value equal to unity shall be used for all
loads leading to serviceability limit states to check the
adequacy of the structure under serviceability limit
states.
5.6.1 Dejection
The deflection under serviceability loads of a building
or a building component should not impair the strength
of the structure or components or cause damage to
finishings. Deflections are to be checked for the most
adverse but realistic combination of service loads and
their arrangement, by elastic analysis, using a load
factor of 1.0. Table 6 gives recommended limits of
deflections for certain structural members and systems.
Circumstances may arise where greater or lesser values
would be more appropriate depending upon the nature
of material in element to be supported (vulnerable to
cracking or not) and intended use of the structure, as
required by client.
Table 6 Deflection Limits
Typeof Deflection DesignLoad Member Supporthtg Maximum
Building Deflection
(1) (2) (3) (4) (5) (6)
Live load/ Whrd load
t,iVC load
LNe load
L!ve load/Wind load
Crane load (Manual
operation)
Crane load (Electric
operation up to 50 t)
Crane load (Electric
operationover50t)
No cranes
Crane + wind
Crane+wind
Live load
Live load
Whrd
Wind
PurlinsandGirts
Simplespan
Cantilever span
Rafter supporting
Gantry
Gantry
Gantry
Column
Gantry (lateral)
Column/frame
Floor and Roof
Cantilever
Building
Inter storey drift
[
Elastic cladding
Brittle cladding
Elastic cladding
Brittle cladding
Elastic cladding
Brittle cladding
Profiled Metal Sheeting
Plastered Sheeting
Crane
Crane
Crane
Elastic cladding
Masonry/Brittle cladding
Crane (absolute)
Relative displacement
between rails supporting
crane
Gantry (Elastic cladding;
pendent operated)
Gantry (Brittle cladding; cab
operated)
Elements not susceptible to
cracking
Elements susceptible to
cracking
Elements not susceptible to
cracking
Elements susceptible to
cracking
Elastic cladding
Brittle cladding
—
Span/150
Span/l 80
Span/240
Spatr/300
Span/120
Span/150
Sparr/180
Sparr1240
Spaa/500
Spanl150
Span/l 000
Height/l 50
Height/240
SpanMOO
IOmm
Height/200
Height/400
Sparr/300
Spsm/360
Span/l 50
Span/180
Height/300
Height/500
Storey height/300
31

IS 800:2007
5.6.1.1 Where the deflection due to the combination
of dead load and Iive load is likely to be excessive,
consideration should be given to pre-camber the beams,
trusses and girders. The value of desired camber shall
be specified in design drawing. Generally, for spans
greater than 25 m, a camber approximately equal to
the deflection due to dead loads plus half the live load
may be used. The deflection of a member shall be
calculated without considering the impact factor or
dynamic effect of the loads on deflection. Roofs, which
are very flexible, shall be designed to withstand any
additional load that is likely to occur as a result of
pending of water or accumulation of snow or ice.
5.6.2 Vibration
Suitable provisions in the design shall be made for
the dynamic effects of live loads, impact loads and
vibrdti on due to machinery operating loads. In severe
cases possibility of resonance, fatigue or
unacceptable vibrations shall be investigated.
Unusually flexible structures (generally the height
to effective width of lateral load resistance system
exceeding 5:1) shall be investigated for lateral
vibration under dynamic wind loads. Structures
subjected to large number of cycles of loading shall
be designed against fatigue failure, as specified in
Section 13. Floor vibration effect shall be considered
using specialist literature (see Annex C),
5.6.3 Durabi[i(y
Factors that affect the durability of the buildings, under
conditions relevant to their intended life, are listed
below:
a) Environment,
b) Degree of exposure,
c) Shape of the member and the structural detail,
d) Protective measure, and
e) Ease of maintenance.
5.6.3.1 The durability of steel structures shall be
ensured by following recommendations in Section 15.
Specialist literature may be referred to for more detailed
and additional information in design for durability.
5.6.4 Fire Resistance
Fire resistance of a steel member is a function of its
mass, its geometry, the actions to which it is subjected,
its structural support condition, fire protection
measures adopted and the fire to which it is exposed.
Design provisioris to resist fire are briefly discussed in
Section 16. Specialist literature may be referred to for
more detailed information in design of fire resistance
of steel structures.
SECTION 6
DESIGN OF TENSION MEMBERS
6.1 Tension Members
Tension members are linear members in which axial
forces act to cause elongation (stretch). Such members
can sustain loads upto the ultimate load, at which stage
they may fail by rupture at a critical section. However,
if the gross area of the member yields over a major
portion of its length before the rupture load is reached,
the member may become non-functional due to
excessive elongation. Plates and other rolled sections
in tension may also fail by block shear of end bolted
regions (see 6.4.1).
The factored design tension 1“,in the members shall
satisfy the following requirement:
T<T~
where
T~ = design strength of the member.
The design strength of a member under axial tension,
T~,is the lowest of the design strength due to yielding
of gross section, T~g rupture strength of critical section,
T~n, and block shear T~~,given in 6.2, 6.3 and 6.4,
respectively.
6.2 Design Strength Due to Yielding of Gross Section
The design strength of members under axial tension,
T~~,as governed by yielding of gross section, is given
by
Tdg= Agfy Mno
where
f, = yield stress of the material,
A~ = gross area of cross-section, and
y~o = partial safety factor for failure in tension by
yielding (see Table 5).
6.3 Design Strength Due to Rupture of Critical
Section
6.3.1 Plates
The design strength in tension of a plate, T~n, as
governed by rupture of net cross-sectional area, An, at
the holes is given by
T~n= 0.9 AnfU/ ‘y~,
where
‘Yml=
f“ =
An =
32
partial safety factor for failure at ultimate
stress (see Table 5),
ultimate stress of the material, and
net effective area of tbe member given by,

.. ._,_,
____
[ 1
An= b-rid, + ~$- t
it
where
b, t = width and thickness of the plate,
d~ =
g =
P, =
n=
i=
respective y,
diameter of the bolt hole (2 mm in addition
to the diameter of the hole, in case the
directly punched holes),
gauge length between the bolt holes, as
shown in Fig. 5,
staggered-pitch length between line of bolt
holes, as shown in Fig. 5,
number of bolt holes in the critical section,
and
subscript for summation of all the inclined
4
FIG. 5 PLATESWITHBOLTSHOLESINTENSION
6.3.2 Threaded Rods
The design strength of threaded rods in tension, Tdn,as
governed by rupture is given by
Tdn= 0.9 An ful ym,
where
Am = net root area at the threaded section.
6.3.3 Single Angles
The rupture strength of an angle connected through
one leg is affected by shear lag. The design strength,
Tdn,as governed by rupture at net section is given by:
7’dn=0.9 AnC~u/ ‘y~l + ~ A~O fY/Y~O
where
where
w = outstand leg width,
b, = shear lag width, as shown in Fig. 6, and
LC =
IS 800:2007
length of the end connection, that is the
distance between the outermost bolts in the
end joint measured along the load direction
or length of the weld along the load
direction.
For preliminary sizing, the rupture strength of net
section may be approximately taken as:
where
cf. =
An =
An, =
AgO =
t .
Itv
0.6 for one or two bolts, 0.7 for three bolts
and 0.8 for four or more bolts along the
length in the end connection or equivalent
weld length;
net area of the total cross-section;
net area of the connected leg;
gross area of the outstanding leg; and
thickness of the leg.
r]
w
+E- --.
T .-k---
———
-------
J L—-—.—--————————— 2
-.-Yd
b~=w
bs=w+w, -t
FIG. 6 ANGLESWITHSINGLELEG CONNECTIONS
6.3,4 Other Section
The rupture strength, Tdn, of the double angles,
channels, I-sections and other rolled steel sections,
connected by one or more elements to an end gusset is
also governed by shear lag effects. The design tensile
strength of such sections as governed by tearing of net
section may also be calculated using equation in 6.3.3,
where ~ is calculated based on the shear lag distance,
b,, taken from the farthest edge of the outstanding leg
to the nearest bolt/weld line in the connected leg of
the cross-section.
6.4 Design Strength Due to Block Shear
The strength as governed by block shear at an end
connection of plates and angles is calculated as given
in 6.4.1.
6.4.1 Bolted Connections
The block shear strength, Td~ of connection shall be
taken as the smaller of,
or
Td~= (0.944,. f. /( $ ~ml) + Atgfy %0 )
33

IS 800:2007
where
Av~,Avn= minimum gross and net area in shear along
bolt line parallel to external force,
respectively (1-2 and 3-4 as shown in
Fig. 7A and 1-2 as shown in Fig. 7B),
At~, A,fl = minimum gross and net area in tension
from the bolt hole to the toe of the angle,
end bolt line, perpendicular to the line of
force, respectively (2-3 as shown in
Fig. 7B), and
~u,~Y = ultimate and yield stress of the material,
respectively.
6.4.2 Welded Connection
The block shear strength, Td~ shall be checked for
welded end connections by taking an appropriate
section in the member around the end weld, which can
shear off as a block.
SECTION 7
DESIGN OF COMPRESSION MEMBERS
7.1 Design Strength
7.1.1 Common hot rolled and built-up steel members
used for carrying axial compression, usually fail by
flexural buckling. The buckling strength of these
members is affected by residual stresses, initial bow
and accidental eccentricities of load. To account for
all these factors, the strength of members subjected to
axial compression is defined by buckling class a, b, c,
or d as given Table 7.
7.1.2 The design compressive strength Pd, of a member
is given by:
P<Pd
where
P~ = A,fCd
--EEm--
4—0- -
[ E–
+—*
-
—
where
A. = effective sectional area as defined
in 7.3.2, and
Id = design compressive stress, obtained
as per 7.1.2.1.
7.1.2.1 The design compressive stress, ~d, of axially
loaded compression members shrdl be calculated using
the following equation:
f., =
f, /ymo
= Xfy/Ymo ~ fy/Yti
(j+[&-q’
0.5 [1 + a (x – 0.2)+ az]
non-dimensional effective slenderness ratio
Xx =
where
X2 E
Euler buckling stress = (KL/2
( /r]
KL/r =
a=
x’=
=
AmO =
effective slenderness ratio or ratio
of effective length, KL to
appropriate radius of gyration, E
imperfection factor given in
Table 7;
stress reduction factor (see Table 8)
for different buckling class,
slenderness ratio and yield stress
[o+($z~a’r’]
partial safety factor for material
strength.
,
1
--*--72 I
4* *3 I
—
1 I
“-”~
‘L’
7A Plate 7B Angle
FIG. 7 BLOCKSHEARFAILURE
34

. ._.
_ , . b.
IS 800:2007
NOTE — Calculated values of design compressive stress,.fi~
for different buckling classes are given in Table 9.
7.1.2.2 The classification of different sections under
different buckling class a, b, c or d, is given in Table
10. The stress reduction factor X, and the design
compressive stress~,~, for different buckling class, yield
stress, and effective slenderness ratio is given in Table
8 for convenience. The curves corresponding to
different buckling class are presented in non-
dimensional form, in Fig. 8.
Table 7 Imperfection Factor, et
(Chzuse.s7.l.l arzd7.1.2.1)
Buckling Class a b c d
a 0.21 0.34 0.49 0.76
7.2 Effective Length of Compression Members
7.2.1 The effective length KL, is calculated from the
actual length L, of the member, considering the
rotational and relative translational boundary
conditions at the ends. The actual length shall be taken
as the length from centre-to-centre of its intersections
with the supporting members in the plane of the
buckling deformation. In the case of a member with a
free end, the free standing length from the center of
the intersecting member at the supported end, shall be
taken as the actual length.
7.2.2 Effective Length
Where the boundary conditions in the plane of buckling
1.0
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
can be assessed, the effective length, KL can be
calculated on the basis of Table 11. Where frame
analysis does not consider the equilibrium of a framed
structure in the deformed shape (second-order analysis
or advanced analysis), the effective length of
compression members in such cases can be calculated
using the procedure given in D-1. The effective length
of stepped column in single storey buildings can be
calculated using the procedure given in D-2.
7.2.3 Eccentric Beam Connection
In cases where the beam connections are eccentric in
plan with respect to the axes of the column, the same
conditions of restraint as in concentric connection shall
be deemed to apply, provided the connections are
carried across the flange or web of the columns as the
case may be, and the web of the beam lies within, or in
direct contact with the column section, Where practical
difficulties prevent this, the effective length shall be
taken as equal to the distance between points of
restraint, in non-sway frames.
7.2.4 Compression Members in Trusses
In the case of bolted, riveted or welded trusses and
braced frames, the effective length, KL, of the
compression members shall be taken as 0.7 to 1.0 times
the distance between centres of connections, depending
on the degree of end restraint provided. In the case of
members of trusses, buckling in the plane perpendicular
to the plane of the truss, the effective length, KL shall
be taken as the distance between the centres of
intersection. The design of angle struts shall be as
specified in 7.5.
0 0.5 1.0 1,5 2:0 2;5 3;0
FIG. 8 COLUMNBUCKLING
CURVES
35

a
Table 8(a) Stress Reduction Factor, x for Column Buckling Class a
00
0
0
(Clauses 7.1.2.1 and 7.1.2.2)
..
N
=
L
KM
Yield Stress,J (MPa)
1. 200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000
20 1.000 0.999 0.998 0.997 0.995 0.994 0.993 0.993 0.990 0.988 0.986 0.984 0.983 0.981 0.979 0.977 0.975 0.972 0.970
30 0.977 0.975 0.974 0.972 0.970 0.969 0.967 0.965 0.961 0.957 0.954 0.951 0.948 0.946 0.943 0.938 0.934 0.930 0.925
40 0.952 0.949 0,947 0.944 0.942 0.939 0.937 0.934 0.926 0.921 0.916 0.911 0.906 0.901 0.896 0.888 0.881 0.873 0.865
50 0.923 0.919 0.915 0.911 0.908 0.904 0.900 0.896 0.884 0.876 0.867 0.859 0.851 0.842 0.834 0.820 0.807 0.794 0.780
60 0.888 0.883 0.877 0.871 0.865 0.859 0.853 0.847 0.828 0.816 0.803 0.790 0.777 0.763 0.750 0.730 0.710 0.690 0.671
70 0.846 0.837 0.829 0.820 0.811 0.803 0.794 0.785 0.758 0.740 0.722 0.703 0.686 0.668 0.651 0.626 0.602 0.579 0.557
80 0.793 0.781 0.769 0.757 0.746 0.734 0.722 0.710 0.675 0.653 0.631 0.610 0.589 0.570 0.551 0.525 0.501 0.478 0.458
90 0.730 0.715 0.700 0.685 0.671 0.657 0.643 0.628 0.590 0.565 0.542 0.520 0.500 0.481 0.463 0.439 0.416 0.396 0.377
100 0.661 0.644 0.627 0.610 0.594 0.579 0.564 0.549 0.510 0.486 0.463 0.443 0.424 0.407 0.390 0.368 0.348 0.331 0.314
I 10 0.591 0.573 0.555 0.538 0.522 0.507 0.492 0.478 0.440 0.418 0.397 0.379 Q.362 0.346 0.332 0.312 0.295 0.279 0.265
120 0.525 0.507 0.489 0.473 0.458 0.443 0.429 0.416 0.381 0.361 0.343 0.326 0.311 0.297 0.284 0.267 0.252 0.238 0.226
130 0.466 0.448 0.432 0.416 0.402 0.388 0.376 0.364 0.332 0.314 0.298 0.283 0.269 0.257 0.246 0.231 0.217 U.206 0.195
140 0.413 0.397 0.382 0.368 0.355 0.342 0.331 0.320 0.291 0.275 0.260 0.247 0.235 0.224 0.214 0.201 0.189 0.179 0.170
150 0.368 0.353 0.339 0.326 0.314 0.303 0.293 0.283 0.257 0.243 0.229 0.218 0.207 0.197 0.189 0.177 0.166 0.157 0.149
160_ 0.329 0.316 0.303 0.291 0.280 0.270 0.261 0.252 0.229 0.215 0.204 0.193 0.184 0.175 0.167 0.157 0.147 0.139 0.132
170 0.296 0.283 0.272 0.261 0.251 0.242 0.233 0.225 0.204 0.192 0.182 0.172 0.164 0.156 0.149 0.140 0.131 0.124 0.117
180 0.267 0.255 0.245 0.235 0.226 0.218 0.210 0.203 0.184 0.173 0.163 0.155 0.147 0.140 0.134 0.125 0.118 0.111 0.105
190 0.242 0.231 0.222 0.213 0.205 0.197 0.190 0.183 0.166 0.156 0.147 0.140 0.133 0.126 0.121 0.113 0.106 0.100 0.095
200 0.220 0.210 0.202 0.193 0.186 0.179 0.172 0.166 0.151 0.142 0.134 0.127 0.120 0.115 0.109 0.102 0.096 0.091 0,086
210 0.201 0.192 0.184 0.177 0.170 0.163 0.157 0.152 0.137 0,129 0.122 0.115 0.110 0.104 0.099 0.093 0.087 0.083 0.078
220 0.184 0.176 0.169 0.162 0.155 0.149 0.144 0.139 0.126 0.118 0.111 0.106 0.100 0.095 0.091 0.085 0.080 0.075 0.071
230 0.170 0.162 0.155 0.149 0.143 0.137 0.132 0.128 0.115 0.108 0.102 0.097 0.092 0.088 0.083 0.078 0.073 0.069 0.065
240 0.157 0.149 0.143 0.137 0.132 0.127 0.122 0.118 0.106 0.100 0.094 0.089 0.085 0.081 0.077 0.072 0.068 0.064 0.060
250 0.145 0.138 0.132 0.127 0.122 0.117 0.113 0.109 0.098 0.092 0.087 0.082 0.078 0.074 0.071 0.066 0.062 0.059 0.056

Table 8(b) Stress Reduction Factor, ~ for Column Buckling Class b
(Clauses 7.1.2.1 and 7. 1.2.2)
KL/r Yield Stress, A (MPa)
4 200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 I.000 1.000 1.000 1.000 1.000 1.000 1,000 I.000 1.000
20 1.000 0.998 0.996 0.994 0.993 0.991 0.990 0.986 0.983 0.981 0.978 0.975 0.972 0.970 0.967 0.963 0.960 0.956 0.953
30 0.963 0.961 0.958 0.955 0.953 0.950 0.948 0.943 0.938 0.933 0.929 0.924 0.920 0.915 0.91I 0.904 0.898 0.892 0.886
40 0.925 0.921 0.917 0.913 0.909 0.906 0.902 0.895 0.887 0.880 0.873 0.866 0.859 0.852 0.845 0.835 0.825 0.815 0.805
50 0,883 0.877 0.872 0.866 0.861 0.855 0.850 0.839 0.829 0.818 0.808 0.798 0.787 0.777 0.767 0.752 0.737 0.722 0.708
60 0.835 0.827 0.820 0.812 0.805 0.798 0.790 0.775 0.761 0.746 0.732 0.718 0.704 0.691 0.677 0.657 0.638 0.620 0.602
70 0.781 0.771 0.761 0.751 0.742 0.732 0.722 0.703 0.685 0.667 0.649 0.632 0.615 0.599 0.584 0.561 0.540 0.520 0.502
80 0.721 0.709 0.697 0.685 0.673 0.661 0.650 0.627 0.606 0.585 0.566 0.547 0.529 0.512 0.496 0.474 0.453 0.434 0.416
90 0.657 0.643 0.629 0.615 0.602 0.589 0.576 0.552 0.530 0.508 0.488 0.470 0.452 0.436 0.421 0.400 0.380 0.363 0.346
100 0.593 0.577 0.562 0.548 0.534 0.520 0.507 0.483 0.461 0.440 0.421 0.403 0.387 0.372 0.358 0.339 0.321 0.306 0.291
110 0.531 0.515 0.500 0.485 0.471 0.458 0.445 0.422 0.401 0.381 0.364 0.348 0.333 0.319 0.306 0.289 0.274 0.260 0.247
120 0.474 0.458 0.443 0.429 0.416 0.403 0.391 0.370 0.350 0.332 0.316 0.30I 0.288 0.276 0.265 0.249 0.236 0.223 0.212
130 0.423 0.408 0.394 0.380 0.368 0.356 0.345 0.325 0.307 0.291 0.276 0.263 0.251 0.240 0.230 0.217 0.204 0.194 0.184
140 0.378 0.364 0.350 0.338 0.327 0.316 0.306 0.287 0.271 0.256 0.243 0.23 I 0.221 0.21I 0.202 0.190 0.I79 0.169 0.161
150 0.339 0.325 0.313 0.302 0.291 0.281 0.272 0.255 0.241 0.227 0.215 0.205 0.195 0.186 0.178 0.167 0.158 0.149 0.142
160 0.305 0.292 0.281 0.271 0.261 0.252 0.243 0.228 0.215 0.203 0.192 0.182 0.L74 o.166 0.158 0.149 0.140 0.133 0.126
170 0.275 0.264 0.253 0.244 0.235 0.227 0.219 0.205 0.193 0.182 0.172 0.163 0.155 0.148 0.142 0.133 0.125 0.118 0.112
180 0.249 0.239 0.229 0.220 0.212 0.205 0.198 0.185 0.174 0.164 0.155 0.147 0.140 0.133 0.128 0.120 0.113 0.106 0.101
190 0.227 0.217 0.208 0.200 0.193 0.186 0.179 0.168 0.157 0.148 0.140 0.133 0.127 0.121 0.115 0.108 0.102 0.096 0.091
200 0.207 0.198 0.190 0.183 0.176 0.169 0.163 0.153 0.143 0.135 0.128 0.121 0.[15 0.110 0.105 0.098 0.092 0.087 0.083
2}0 0.190 0.182 0.174 0.167 0.161 0.155 0.149 0.140 0.131 0.123 0.117 0.110 0.105 0.100 0.096 0.090 0.084 0.080 0.075
220 0.174 0.167 0.160 0.154 0.148 0.142 0.137 0.128 0.120 0.113 0.107 0.101 0.096 0.092 0.088 0.082 0.077 0.073 0.069
230 0.161 0.154 0.147 0.141 0.136 0.131 0.126 0.118 0.111 0.104 0.098 0.093 0.088 0.084 0.080 0.075 0.071 0.067 0.063
240 0.149 0.142 0.136 0.131 0.126 0.121 0.117 0.109 0.102 0.096 0.091 0.086 0.082 0.078 0.074 0.070 0.065 0.062 0.058
250 0.138 0.132 0.126 0.121 0.117 0.112 0.108 0.101 0.095 0.089 0.084 0.080 0.076 0.072 0.069 0.064 0.060 0.057 0.054
E
00
0
0

Table 8(c) Stress Reduction Factor, ~ for Column Buckling Class c %
m
(Clauses 7.1.2.1 and 7.1.2.2) o
0
..
KLlr Yield Stress, f, (MPa)
4 200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 I.000 1.000 1.000 I.000
20 0.999 0.997 0.994 0.992 0.990 0.987 0.985 0.981 0.976 0.972 0,968 0.964 0.961 0.957 0.953 0.948 0.943 0.938 0.933
30 0.948 0.944 0.941 0.937 0.933 0,930 0.926 0.920 0.913 0.907 0.901 0.895 0.S89 0.883 0.877 0.869 0.861 0.853 0.845
40 0.896 0.891 0.885 0.880 0.875 0.870 0.866 0.856 0.847 0.838 0.829 0.820 0.812 0.803 0.795 0.783 0.771 0.760 0.748
50 0.841 0.834 0.827 0.821 0.814 0.807 0.801 0.788 0.776 0.763 0.752 0.740 0.729 0.717 0.706 0.690 0.675 0.660 0.645
60 0.783 0.774 0.765 0.757 0.748 0.740 0.732 0.716 0.700 0.685 0.670 0.656 0.642 0.628 0.615 0.596 0.578 0.561 0.544
70 0.722 0.711 0.700 0.690 0.680 0.670 0.660 0.641 0.623 0.605 0.588 0.572 0.557 0.542 0.528 0.508 0.489 0.471 0.454
80 0.659 0.646 0.634 0.622 0.611 0.600 0.589 0.568 0.548 0.529 0.512 0.495 0.479 0.464 0.450 0.430 0.412 0.395 0.379
90 0.596 0.583 0.569 0.557 0.544 0.533 0.521 0.499 0.479 0.460 0.443 0.426 0.411 0.397 0.383 0.365 0.348 0.332 0.318
I00 0.536 0.522 0.508 0.495 0.483 0.47I 0.459 0.438 0.418 0.400 0.384 0.368 0.354 0.341 0.328 0.3I 1 0.296 0.282 0.269
110 0.480 0.466 0.453 0.440 0.428 0.416 0.405 0.385 0.366 0.349 0.333 0.3I9 0.306 0.294 0.283 0.268 0.254 0.242 0.230
120 0.430 0.416 0.403 0.391 0..379 0.368 0.358 0.339 0.321 0.306 0.291 0.278 0.267 0.256 0.246 0.232 0.220 0.209 0.199
130 0.385 0.372 0.360 0.348 0.337 0.327 0.317 0.299 0.283 0.269 0.256 0.244 0.234 0.224 0.215 0.203 0.192 0.182 0.173
140 0.346 0.333 0.322 0.311 0.301 0.291 0.282 0.266 0.25I 0.238 0.227 0.216 0.206 0.197 0.189 0.178 0.168 0.160 0.152
150 0.31I 0.300 0.289 0.279 0.269 0.261 0.252 0.237 0.224 0.212 0.202 0.192 0.183 0.175 0.168 0.158 0.149 0.141 0.134
160 0.28I 0.270 0.260 0.251 0.242 0.234 0.227 0.213 0.201 0,190 0.180 0.172 0.164 0.156 0.150 0.141 0.133 0.126 0.120
170 0.255 0.245 0.236 0.227 0.219 0.212 0.205 0.192 0.181 0.171 0.162 0.154 0.147 0.140 0.134 0.126 0.119 0.113 0.107
180 0.232 0.223 0.214 0.206 0.199 0.192 0.186 0.174 0.164 0.155 0.147 0.139 0.133 0.127 0.121 0.114 0.107 0.102 0.096
190 0.212 0.203 0.195 0.188 0.181 0.175 0.169 0.158 0.149 0.140 0.133 0.126 0.120 0.115 0.110 0.103 0.097 0.092 0.087
200 0.194 0.186 0.179 0.172 0.166 0.160 0.154 0.144 0.136 0.128 0.121 0.115 0.110 0.105 0.100 0.094 0.089 0.084 0.079
210 0.178 0.171 0.164 0.158 0.152 0.146 0.141 0.132 0.124 0.117 0.111 0.105 0.100 0.096 0.092 0.086 0.081 0.076 0.072
220 O.!64 0.157 0.151 0.145 0.I40 0.135 0.130 0.122 0.114 0.108 0.102 0.097 0.092 0.088 0.084 0.079 0.074 0.070 0.066
230 0.152 0.145 0.140 0.134 0.129 0.124 0.120 0.112 0.105 0.099 0.094 0.089 0.085 0.081 0.077 0.073 0.068 0.065 0.061
240 0.141 0.135 0.129 0.124 0.120 0.115 0.111 0.104 0.098 0.092 0.087 0.082 0.078 0.075 0.071 0.067 0.063 0.060 0.056
250 0.131 0.125 0.120 0.115 0.111 0.I07 0.103 0.096 0.090 0.085 0.081 0.076 0.073 0.069 0.066 0.062 0.058 0.055 0.052

Table 8(d) Stress Reduction Factor, ~ for Column Buckling C lass d
(Clauses 7.1.2.1 and 7.1 .2.2)
IA Yield Stress, JY(MPa)
4
200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 I.000 1.000 1.000 1.000 1.000 1.000 1.000 i.000 1.000
20 0.999 0.995 0.991 0.988 0.984 0.980 0.977 0.970 0.964 0.958 0.952 0.946 0.940 0.935 0.930 0.922 0.915 0.908 0.901
30 0.922 0.916 0.91I 0.906 0.901 0.896 0.891 0.881 0.872 0.863 0.855 0.847 0.839 0.831 0.823 0.813 0.802 0.792 0.782
40 0.848 0.841 0.834 0.828 0.821 0.815 0.808 0.796 0.784 0.773 0.762 0.751 o.74i 0.731 0.721 0.707 0.694 0.681 0.668
50 0.777 0.768 0.760 0.752 0.744 0.736 0.728 0.713 0.699 0.685 0.672 0.659 0.647 0.635 0.624 0.608 0.592 0.577 0.563
60 0.707 0.697 0.687 0.678 0.668 0.659 0.651 0.634 0.617 0.602 0.587 0.573 0.560 0.547 0.535 0.517 0.501 0.486 0.471
70 0.640 0.629 0.618 0.607 0.597 0.587 0.578 0.559 0.542 0.526 0.510 0.496 0.482 0.469 0.456 0.439 0.423 0.408 0.394
80 0.576 0.564 0.553 0.542 0.531 0.521 0.511 0.492 0.474 0.458 0.442 0.428 0.414 0.402 0.390 0.373 0.358 0.344 0.330
90 0.517 0.505 0.493 0.482 0.471 0.461 0.451 0.432 0.415 0.399 0.384 0.370 0.357 0.345 0.334 0.319 0.304 0.292 0.280
00 0.464 0.451 0.440 0.428 0.418 0.408 0.398 0,380 0.363 0.348 0.334 0.321 0.309 0.298 0.288 0,274 0.261 o,~49 0.239
10 0.416 0.404 0.392 0.381 0.371 0.361 0.352 0.335 0.319 0.305 0.292 0.281 0.270 0.259 0.250 o.~37 0.226 0.215 0.206
20 0.373 0.361 0.350 0.340 0.330 0.321 0.313 0.297 0.282 0.269 0.257 0.246 0.236 0.227 0.219 0.207 0.197 0.187 0.179
30 0.336 0.325 0.314 0.305 0.295 0.287 0.279 0.264 0.251 0.239 0.228 0.218 0.209 0.200 0.193 0.182 0.173 0.164 0.157
40 0.303 0.292 0.283 0.274 0.265 0.257 0.250 0.236 0.224 0.213 0.203 0.194 0.185 0.178 0.171 0.161 0.153 0.145 0.138
50 0.274 0.264 0.255 0.247 0.239 0.231 0.224 0.212 0.201 0.190 0.181 0.173 0.165 0.159 0.152 0.144 0.136 0.129 0.123
60 0.249 0.240 0.231 0.223 0.216 0.209 0.203 0.191 0.181 0.171 0.163 0.155 0.149 0.142 0.137 0.129 0.122 0.116 0.110
70 0.227 0.218 0.210 0.203 0.196 0.190 0.184 0.173 0.164 0.155 0.147 0.140 0.134 0.128 0.123 0.116 0.110 0.104 0.099
80 0.207 0.199 0.192 0.185 0.179 0.173 0.167 0.157 0.149 0.141 0.134 0.127 0.122 0.1)6 0.111 0.105 0.099 0.094 0.089
90 0.190 0.183 0.176 0.169 0.164 0.158 0.153 0.144 0.136 0.128 0.122 0.116 0.111 0.106 0.101 0.095 0.090 0.085 0.081
00 0.175 0.168 0.162 0.156 0.150 0.145 0.140 0.132 0.124 0.118 0.112 0.106 0.101 0.097 0.093 0.087 0.082 0.078 0.074
10 0.161 0.155 0.149 0.143 0.138 0.134 0.129 0.121 0.114 0.108 0.102 0.097 0.093 0.089 0.085 0.080 0.075 0.071 0.068
20 0.149 0.143 0.138 0.133 0.128 0.123 0.119 0.112 0.105 0.100 0.094 0.090 0.086 0.082 0.078” 0.074 0.069 0.066 0.062
30 0.138 0.133 0.128 0.123 0.118 0.114 0.110 0.104 0.097 0.092 0.087 0.083 0.079 0.075 0.072 0.068 0.064 0.061 0.058
40 0.129 0.123 0.119 0.114 0.11o 0.106 0.103 0.096 0.090 0.085 0.081 0.077 0.073 0.070 0.067 0.063 0.059 0.056 0.053
50 0.120 0.115 0.110 0.106 0.102 0.099 0.095 0.089 0.084 0.079 0.075 0.071 0.068 0.065 0.062 0.058 0.055 0.052 0.049
%
00
0
0
. .
~
o
4

Table 9(a) Design Compressive Stress,~C~ (MPa) for Column Buckling Class a E
(Ckzuse 7.1.2.1)
m
o
0
..
KLlr Yield Stress, & (MPa)
J
200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10 182 191 200 213 218 227 236 255 273 291 309 327 34s 364 382 409 436 464 491
20 182 191 200 208 217 226 235 252 270 287 305 322 339 357 374 400 425 451 476
30 178 186 195 203 212 220 229 245 262 279 295 311 328 344 360 384 408 431 454
40 173 181 189 197 205 213 221 237 253 268 283 298 313 328 342 363 384 405 425
50 168 176 183 191 198 205 213 227 241 255 268 281 294 306 318 336 352 368 383
60 162 169 1’75 182 189 I95 202 214 226 237 248 258 268 278 286 299 310 320 329
70 154 160 166 171 177 182 I88 197 207 215 223 230 237 243 249 256 263 268 274
80 I44 149 154 158 163 167 171 178 184 190 195 199 204 207 210 215 219 222 225
90 133 I37 140 i43 146 149 ]52 157 161 164 168 I70 173 175 I77 179 182 184 185
100 120 123 125 128 130 132 133 136 139 141 143 145 146 148 I49 151 152 153 154
110 107 109 111 112 i 14 115 116 118 120 121 123 124 125 126 127 128 129 129 130
120 95.5 96.7 97.9 98.9 100 101 101 103 104 105 106 107 107 108 109 109 110 110 Ill
130 84.6 85.5 86.3 87 87.7 88.3 88.8 89.8 90.6 91.3 92.0 92.5 93.0 93.5 93.9 94.4 94.9 95.3 95.7
140 75.2 75.8 76.4 76.9 77.4 77.8 78.2 78.9 79.5 80.0 80.5 80.9 81,3 81.6 81.9 82.3 82.6 83.0 83.2
150 67.0 67.4 67.9 68.2 68.6 68.9 69.2 69.7 70.2 70.6 70.9 71.2 71.5 71.8 72.0 72.3 72.6 72.9 73.1
160 59.9 60.3 60.6 60.9 61.1 61.4 61.6 62.0 62.4 62.7 62.9 63.2 63.4 63.6 63.8 64.0 64.3 64.5 64.6
170 53.8 54.1 54.3 54.6 54.8 55.0 55.I 55.5 55.7 56.0 56.2 56.4 56,6 56.7 56.9 57.1 57.3 57.4 57.6
180 48.6 48.8 49.0 49.2 49.3 49.5 49.6 49.9 50.1 50.3 50.5 50.6 50.8 50.9 51.0 51.2 51.3 51.5 51.6
190 44.0 44.2 44.3 44.5 44.6 44.7 44.9 45.1 45.3 45.4 45.6 45.7 45.8 45.9 46.0 46.2 46.3 46.4 46.5
200 40.0 40.2 40.3 40.4 40.5 40.7 40.7 40.9 41.1 41.2 41.3 41.4 41.5 41.6 41.7 41.8 41.9 42.0 42.1
210 36.6 36.7 36.8 36.9 37.0 37.1 37.2 37.3 37.4 37.6 37.7 37.8 37.8 37.9 38.0 38.1 38.2 38.3 38.3
220 33.5 33.6 33.7 33.8 33.9 34.0 34.0 34.2 34.3 34.4 34.5 34.5 34.6 34.7 34.7 34.8 34.9 35.0 35.0
230 30.8 30.9 31.0 31.1 31.2 31.2 31.3 31.4 31.5 31.6 31.6 31.7 31.8 31.8 31.9 31.9 32.0 32.1 32.1
240 28.5 28.5 28.6 28.7 28.7 28.8 28.8 28.9 29.0 29.1 29.1 29.2 29.3 29.3 29.4 29.4 29.5 29.5 29.6
250 26.3 26.4 26.5 26.5 26.6 26.6 26.7 26.7 26.8 26.9 26.9 27.0 27.0 27.1 27.1 27.2 27.2 27.3 27.3

Table 9(b) Design Compressive Stress,jC~ (MPa) for Column Buckling Class b
(Clause 7. 1.2.1)
-P
KLJr Yield Stress, -fY(MPa)
J
200 210 220 230 240 250 260 280 300 320 340 360 380 4CQ 420 450 480 510 540
10 182 191 200 209 218 227 236 255 273 291 309 327 345 364 382 409 436 464 491
20 182 190 199 208 217 225 234 251 268 285 302 319 336 353 369 394 419 443 468
30 175 183 192 200 208 216 224 240 256 271 287 302 318 333 348 370 392 414 435
40 168 176 183 191 198 206 213 228 242 256 270 283 297 310 323 342 360 378 395
50 161 167 174 181 188 194 201 214 226 238 250 261 272 283 293 308 322 335 347
60 152 158 164 170 176 181 187 197 207 217 226 235 243 251 259 269 279 287 295
70 142 147 152 157 162 (66 171 179 187 194 201 207 213 218 223 230 236 241 246
80 131 135 139 143 147 150 154 160 165 170 175 179 183 186 190 194 198 201 204
90 120 123 126 129 131 134 136 141 144 148 151 154 156 159 161 163 166 168 170
IC43 108 110 112 114 116 118 120 123 126 128 130 132 134 135 137 139 140 142 143
110 96.5 98.3 100 101 103 104 105 107 109 111 112 114 115 116 117 118 119 121 121
120 86.2 87.5 88.6 89.7 90.7 91.7 92.5 94.1 95.4 96.6 97.7 98.6 100 100 101 102 103 104 104
130 76.9 77.8 78.7 79.5 80.3 81.0 81.6 82.7 83.7 84.6 85.4 86.1 86.8 87.3 87.9 88.6 89.2 89.8 90.3
140 68.7 69.4 70.1 70.7 71.3 71.8 72.3 73.1 73.9 74.6 75.2 75.7 76.2 76.6 77.1 77.6 78.1 78.5 78.9
150 61.6 62.1 62.6 63.1 63.6 64.0 64.3 65.0 65.6 66.1 66.6 67.0 67.4 67.7 68.1 68.5 68,9 69.2 69.5
160 55.4 55.8 56.2 56.6 56.9 57.3 57.5 58.1 58.5 59.0 59.3 59.7 60.0 60.3 60.5 60.9 61.2 61.5 61.7
170 50.0 50.3 50.7 51.0 51.2 51.5 51.7 52.2 52.5 52.9 53.2 53.5 53.7 53.9 54.1 54.4 54.7 54.9 55.1
180 45.3 45.6 45.9 46,1 46.3 46.5 46.7 47.1 47.4 47.7 47.9 48.1 48.3 48.5 48.7 48.9 49.2 49.3 49.5
190 41.2 41.5 41.7 41.9 42.I 42.2 42.4 42.7 42.9 43.2 43.4 43.6 43.7 43.9 44.0 44.2 44,4 44.6 44.7
200 37.6 37.8 38.0 38.2 38.3 38.5 38.6 38.9 39.1 39.3 39.5 39.6 39.8 39.9 40.0 40.2 40.3 40.5 40.6
210 34.5 34.7 34.8 35.0 35.1 35.2 35.3 35.5 35.7 35.9 36.0 36.2 36.3 36.4 36.5 36.6 36.8 36.9 37.0
220 31.7 31.9 32.0 32.1 32.2 32.3 32.4 32.6 32.8 32.9 33.0 33.1 33.2 33.3 33.4 33.6 33.7 33.8 33.9
230 29.2 29.4 29.5 29.6 29.7 29.8 29.9 30.0 30.1 30.3 30.4 30.5 30.6 30.7 30.7 30.8 30.9 31.0 31.1
240 27.1 27.2 27.3 27.3 27.4 27.5 27.6 27.7 27.8 27.9 28.0 28.1 28.2 28.3 28.3 28.4 28.5 28.6 28.7
250 25.1 25.2 25.3 25.3 25.4 25.5 25.6 25.7 25.8 25.9 26.0 26.0 26.1 26.2 26.2 26.3 26.4 26.5 26.5
..
N
o
0
d

&.
N
Table 9(c) Design Compressive Stress,jC~ (MPa) for Column Buckling Class c 6
(Clause 7.1 .2.1) ~
o
..
KL.lr Yield Stress, ~Y(MPa)
J
200 210 220 230 240 250 260 280 300 320 340 3641 380 400 420 450 480 510 540
10 182 191 200 209 218 227 236 255 273 291 309 327 345 364 382 409 436 464 491
20 182 190 199 207 216 224 233 250 266 283 299 316 332 348 364 388 412 435 458
30 172 180 188 196 204 21I 219 234 249 264 278 293 307 321 335 355 376 395 415
40 163 170 177 184 191 198 205 218 231 244 256 268 280 292 304 320 337 352 367
50 153 159 165 172 178 183 189 201 212 222 232 242 252 261 270 282 295 306 317
60 142 148 153 158 163 168 173 182 191 199 207 215 222 228 235 244 252 260 267
70 131 136 140 144 148 152 156 163 170 176 182 187 192 197 202 208 213 218 223
80 120 123 127 130 133 136 139 145 149 154 158 162 165 169 172 176 180 183 186
90 108 111 114 116 119 121 123 127 131 134 137 140 142 144 146 149 152 154 156
100 97.5 100 102 104 105 107 109 112 114 116 119 120 122 124 125 127 129 131 132
110 87.3 89.0 90.5 92.0 93.3 94.6 95.7 97.9 100 102 103 104 106 107 108 110 111 112 113
120 78.2 79.4 80.6 81.7 82.7 83.7 84.6 86.2 87.6 88.9 90.1 91.1 92.1 93.0 93.8 94.9 95.9 96.8 97.6
130 70.0 71.0 71.9 72.8 73.5 74.3 75.0 76.2 77.3 78.3 79.2 80.0 80.7 81.4 82.0 82.9 83.6 84.3 84.9
140 62.9 63.6 64.4 65.0 65.6 66.2 66.7 67.7 68.6 69.3 70.0 70.7 71.2 71.8 72.3 72.9 73.5 74.1 74.6
150 56.6 57.2 57.8 58.3 58.8 59.2 59.7 641.4 61.1 61.7 62.3 62.8 63.3 63.7 64.1 64.6 65.1 65.5 65.9
160 51.1 51.6 52.1 52.5 52.9 53.3 53.6 54.2 54.8 55.3 55.7 56.1 56.5 56.9 57.2 57.6 58.0 58.4 58.7
170 46.4 46.8 47.1 47.5 47.8 48.I 48.4 48.9 49.3 49.8 50.1 50.5 50.8 51.1 51.3 51.7 52.0 52.3 52.6
180 42.2 42.5 42.8 43.1 43.4 43.6 43.9 44.3 44.7 45.0 45.3 45.6 45.8 46.1 46.3 46.6 46.9 47.1 47.3
190 38.5 38.8 39.0 39.3 39.5 39.7 39.9 40.3 40.6 40.9 41.1 41.4 41.6 41.8 42.0 42.2 42.5 42.7 42.9
200 35.3 35.5 35.7 35.9 36.I 36.3 36.5 36.8 37.0 37.3 37.5 37.7 37.9 38.1 38.2 38.4 38.6 38.8 39.0
210 32.4 32.6 32.8 33.0 33.1 33.3 33.4 33.7 33.9 34.1 34.3 34.5 34.7 34.8 34.9 35.1 35.3 35.4 35.6
220 29.9 30.1 30.2 30.4 30.5 30.6 30.8 31.0 31.2 31.4 31.5 31.7 31.8 31.9 32.1 32.2 32.4 32.5 32.6
230 27.6 27.8 27.9 28.0 28.2 28.3 28.4 28.6 28.8 28.9 29.1 29.2 29.3 29.4 29.5 29.7 29.8 29.9 30.0
240 25.6 25.7 25.9 26.0 26.1 26.2 26.3 26.4 26.6 26.7 26.9 27.0 27.1 27.2 27.3 27.4 27.5 27.6 27.7
250 23.8 23.9 24.0 24.1 24.2 24.3 24.4 24.5 24.7 24.8 24.9 25.0 25.1 25.2 25.3 25.4 25.5 25.6 25.7

Table 9(d) Design Compressive Stress,~& (MPa) for Column Buckling Class d
(Clause 7.1.2.1)
KM Yield Stress, ~Y(MPa)
4
200 210 220 230 240 250 260 280 300 320 340 360 380 404) 420 450 480 510 540‘-
10 182 191 200 209 218 227 236 255 273 291 309 327 345 364 382 409 436 464 49I
20 182 190 198 206 215 223 231 247 263 279 294 310 325 340 355 377 399 42I 442
30 168 175 182 189 i97 204 211 224 238 25I 264 277 290 302 314 332 350 367 384
40 154 161 167 173 179 185 191 203 214 2’25 235 246 256 266 275 289 303 316 328
50 141 147 152 157 162 167 172 182 191 199 208 216 224 231 238 249 258 268 277
60 129 133 137 142 146 150 154 161 168 175 182 188 193 199 204 212 219 225 23I
70 }16 120 124 127 130 133 i37 142 148 153 158 162 167 171 174 180 184 189 193
80 105 108 111 113 116 118 121 125 129 i33 137 140 143 146 149 153 156 159 162
90 94.1 96.4 98.6 101 103 105 107 110 113 116 119 121 123 126 128 130 133 135 137
100 84.3 86.2 87.9 89.6 91.1 92.6 94.0 96.7 99. I 101 103 105 107 108 110 112 114 116 117
110 75.6 77.0 78.4 79.’? 81.0 82.1 83.2 85.3 87.1 88.8 90.4 91.8 93.1 94.4 95.5 97.1 98.5 100 10I
120 67.8 69.0 70.1 71.1 72.1 73.0 73.9 75.5 77.0 78.3 79.5 80.6 81.7 82.6 83.5 84.7 85.8 86.9 87.8
130 61.0 62.0 62.8 63.7 64.5 65.2 65.9 67.2 68.3 69.4 70.4 71.2 72.1 72.8 73.5 74.5 75.4 76.2 76.9
140 55.0 55.8 56.5 57.2 57.8 58.4 59.0 60.0 61.0 61.8 62.6 63.3 64.0 64.6 65.2 66.0 66.7 67.3 67,9
150 49.8 50.4 51.0 51.6 52.! .52.6 53.1 53.9 54.7 55.4 56.0 56.6 57.2 57.7 58.1 58.8 59.3 59.9 60.4
160 45.2 45.7 46.2 46.7 47,1 47.5 47.9 48.6 49.3 49.9 50.4 50.9 51.3 51.7 52.1 52.7 53.1 53.6 54.0
170 41.2 41.6 42,1 42.4 42.8 43.1 43.5 44.1 44.6 45.1 45.5 45.9 46.3 46.7 47.0 47.4 47.8 48.2 48,6
180 37.7 38.0 38.4 38.7 39.0 39.3 39.6 40.1 40.5 41.0 41.3 41.7 42.0 42.3 42.6 43.0 43.3 43.6 43.9
190 34.5 34.9 35.2 35.4 35.7 35.9 36.2 36.6 37.0 37.4 37.7 38.0 38.2 38.5 38.7 39.1 39.4 39.6 39.9
200 31.8 32,0 32.3 32.5 32.8 33.0 33.2 33.6 33.9 34.2 34.5 34.7 35.0 35.2 35.4 35.7 35.9 36.2 36.4
210 29.3 29.6 29.8 30.0 30.2 30.4 30.5 30.9 31.2 31.4 31.7 31.9 32.1 32.3 32.5 32.7 32.9 33.1 33.3
2Z0 27.1 27.3 27.5 27.7 27.9 28.0 28.2 28.5 28.7 29.0 29.2 29.4 29.6 29.7 29.9 30.1 30.3 30.5 30.6
230 25.2 25<3 25.5 25.7 25.8 26.0 26.i 26.4 26.6 26.8 27.0 27.k 27,3 27.5 27.6 27.8 27.9 28.1 28.2
240 23.4 23.6 23.7 23.9 24.0 24.i 24.2 24.5 24.7 24.8 25.0 25.2 25.3 25.4 25.5 25.7 25.9 26.0 26.1
250 21.8 22.0 22.! 22.2 22.3 22.s 22.6 22.8 22.9 23.1 23.2 23.4 23.5 23.6 23.7 23.9 24.0 24.1 24.2
..

Table 10 Buckling (3am of Cross-Sections
(Clause 7.1.2.2)
Cross-Section Limits Buckling About Axis Buckling
Class
(1) (2) (3) (4)
Rolled I-Sections h/b, > 1.2:
t, <40 mm z-z
1-.-%
y.y :
r ,, 40<mm<lj<100mm
z-z b
h’
y-y c
Clr
,T’:
, -J
h/bf s 1.2:
z-z b
t( g 100 mm
L_.%_l
y-y c
rl>lOOmm
z-z d
y-v d
Welded l-Section t,
<40 mm z-z b
I--Y
JJ-.Y
~~ “:~
c
r
tw (r f, >40 mm z-z
;
UT- I ‘x
y-y
L._&l
HOI1OW
Section
6YE3D
Hot rolled Any a
Cold formed Any b
welded Box Section
Generally
+Y
D
(except as below)
Any b
r
Thick welds and
“–i–f: ~z “
‘J ,
L
[?/tf<30 z-z c
L-J---d
w,,, <30 Y-Y c
Channel, Angle, T and Solid Sections
.! ~“y~ *+ ‘ny c
l--y
Built-up Member
l--y
m
Any c
zT-- ‘;T
l-y
44

IS 800:2007
Table 11 Effective Length of Prismatic Compression Members
(Clause 7.2.2)
Boundary Conditions Schematic Effective
Representation Length
7
AtOneEnd At the Other End
A
T F
Translation Rotation Translation Rotation
(1) (2) (3) (4) (5) (6)
L]
$
)
t
I

/,
2.OL
Restrained Restrained Free Free
Free
Restrained
Restrained
Restrained
Free
Restrained
Free
Restrained
Free
Restrained
Restrained
Free
I
Y
/
;
‘1
‘
‘.
A
L
,/
Restrained Restrained
{
Restrained Restrained

/
1.OL
1.2L
0.8.L
0.65L
NOTE— L is the unsupportedlengthof the compressionmember(see7.2.1).
45

IS 800:2007
7.3 Design Details (see 9.3.2.2). The ends of compression members faced
7.3.1 Thickness of Plate Elements
Classification of members on the basis of thickness of
constituent plate elements shall satisfy the width-
thickness ratio requirements specified in Table 2.
7.3.2 Effective Sectional Area, A,
Except as modified in 3.7.2 (Class 4), the gross
sectional area shall be taken as the effective sectional
area for all compression members fabricated by
welding, bolting and riveting so long as the section is
semi-compact or better. Holes not fitted with rivets,
bolts or pins shall be deducted from gross area to
calculate effective sectional area.
7.3.3 Eccentricity for Stanchions and Columns
7.3.3.1 For the purpose of determining the stress in a
stanchion or column section, the beam reactions or
similar loads shall be assumed to be applied at an
eccentricity of 100 mm from the face of the section or
at the centre of bearing whichever dimension gives the
greater eccentricity, and with the exception of the
following two cases:
a) In the case of cap connection, the load shall
be assumed to be applied at the face of the
column or stanchion section or at the edge of
packing, if used towards the span of the beam.
b) In the case of a roof truss bearing on a cap,
no eccentricity be taken for simple bearings
without connections capable of developing
any appreciable moment. In case of web
member connection with face, actual
eccentricity is to be considered.
7.3.3.2 In continuous columns, the bending moments
due to eccentricities of loading on the columns at any
floor may be divided equally between the columns
above and below that floor level, provided thaL the
moment of inertia of one column section, divided by
its effective length does not exceed 1.5 times the
correspoi~ding value of the other column. Where this
ratio is exceeded, the bending moment shall be divided
in proportion to the moment of inertia of the column
sections divided by their respective effective lengths.
7.3.4 Splices
for bearing shall invariably be machined to ensure perfect
contact of surfaces in bearing.
7.3.4.2 Where such members are not faced for complete
bearing, the splices shall be designed to transmit all
the forces to which the members are subjected.
7.3.4.3 Wherever possible, splices shall be
proportioned and arranged so that the centroidal axis
of the splice coincides as nearly as possible with the
centroidal axes of the members being jointed, in order
to avoid eccentricity; but where eccentricity is present
in the joint, the resulting stress shall be accounted for.
7.4 Column Bases
7.4.1 General
Column bases should have sufficient stiffness and
strength to transmit axial force, bending moments and
shear forces at the base of the columns to their
foundation without exceeding the load carrying
capacity of the supports. Anchor bolts and shear keys
should be provided wherever necessary, Shear
resistance at the proper contact surface between steel
base and concrete/grout may be calculated using a
friction coefficient of 0.45.
The nominal bearing pressure between the base plate
and the support below may be determined on the basis
of linearly varying distribution of pressure. The
maximum bearing pressure should not exceed the
bearing strength equal to 0.6~C~,wheref,~ is the smaller
of characteristic cube strength of concrete or bedding
material.
7.4,1.1 If the size of the base plate is larger than that
required to limit the bearing pressure on the base
support, an equal projection c of the base plate beyond
the Pace of the column and gusset may be taken as
effective in transferring the column load as given in
Fig. 9, such that bearing pressure on the effective area
does not exceed bearing capacity of concrete base.
7.4.2 Gusseted Bases
For stanchion with gusseted bases, the gusset plates,
angle cleats, stiffeners, fastenings, etc, in combination
with the bearing area of the shaft, shall be sufficient to
take the loads, bending moments and reactions to the
7.3.4.1 Where the ends of compression members are
base plate without ex~eeding specified strength. All
prepared for bearing over the whole area, they shall be
the bearing surfaces shall be machined to ensure perfect
spliced to hold the connected members accurately in
contact.
position, and to resist bending or tension, if present. Such 7.4.2.1 Where the ends of the column shaft and the
splices should maintain the intended member stiffness gusset plates are not faced for complete bearing, the
about each axis. Splices should be located as close to weldings, fastenings connecting them to the base plate
the point of inflection as possible. Otherwise their shall be sufficient to transmit all the forces to which
capacity should be adequate to carry magnified moment the base is subjected.
46

IS 800:2007
7.4.2.2 Column and base plate connections
Where the end of the column is connected directly to
the base plate by means of full penetration butt welds,
the connection shall be deemed to transmit to the base
all the forces and moments to which the column is
subjected.
7.4.3 Slab Bases
Columns with slab bases need not be provided with
gussets, but sufficient fastenings shall be provided to
retain the parts securely in place and to resist all
moments and forces, other than direct compression,
including those arising during transit, unloading and
erection,
7.4.3.1 The minimum thickness, t,, of rectangular slab
bases, supporting columns under axial compression
shall be
t,
= 2.5w(a2–0.3b2 )y~0/fY > t~
where
w = uniform pressure from below on the slab
base under the factored load axial
compression;
a, b = larger and smaller projection, respectively
tf
of the slab base beyond the rectangle
circumscribing the column; and
= flange thickness of compression member.
When only the effective area of the base plate is used
as in 7.4.1.1, C* may be used in the above equation
(see Fig. 9) instead of (a* - 0.3b2).
7.4.3.2 When the slab does not distribute the column
load uniformly, due to eccentricity of the load etc,
special calculation shall be made to show that the base
is adequate to resist the moment due to the non-uniform
pressure from below.
7.4.3.3 Bases for bearing upon concrete or masonry
need not be machined on the underside.
7.4.3,4 In cases where the cap or base is fillet welded
directly to the end of the column without boring and
shouldering, the contact surfaces shall be machined to
give a perfect bearing and the welding shall be
sufficient to transmit the forces as required in 7.4.3.
Where full strength butt welds are provided, machining
of contact surfaces is not required.
7.5 Angle Struts
7.5.1 Single Angle Struts
The compression in single angles may be transferred
either concentrically to its centroid through end gusset
or eccentrically by connecting one of its legs to a gusset
or adjacent member.
7.5.1.1 Concentric loading
When a single angle is concentrically loaded in
compression, the design strength may be evaluated
using 7.1.2.
EFFECTIVE PORTION
j STIFFENER
FIG. 9 EFFECTIVE
AREAOFA BASEPLATE
47

IS 800:2007
7.5.1.2 Loaded through one leg
The flexura! torsional buckling strength of single angle
loaded in compression through one of its legs may be
evaluated using the equivalent slenderness ratio, ACas
given below:
where
k,, kz, k3 = constants depending upon the end
condition, as given in Table 12,
[-)
I
L,,,,= ~&– and k~ =
(b, +b2)/2t
-
J
TCLE
‘%
where
1=
r=
1’1’
bj, bz =
t=
E =
centre-to-centre length of the supporting
member,
radius of gyration about the minor axis,
width of the two legs of the angle,
thickness of the leg, and
yield stress ratio ( 250~Y)05.
Table 12 Constants kl, kz and k~
St No. of Bolts Gusset/Con- k, k, k,
No. at Each End netting
Connection Member
Fixity ‘‘
(1) (2) (3) (4) (5) (6)
i) Fixed
{
0.20 0.35 20
>2
Hinged 0.70 0.60 5
ii) Fixed
{
0.75 0.35 20
1
Hinged 1.25 0.50 60
“ Stiffeners of in-plane rotational restraint provided by the
.gossetkmrmecting
member.
For partial restraint, the LCcan be interpolated between the I.C
results for fixed and hinged cases.
7.5.2 Double Angle Struts
7.5.2.1 For double angle discontinuous struts,
connected back to back, on opposite sides of the gusset
or a section, by not less than two bolts or rivets in line
along the angles at each end, or by the equivalent in
welding, the load may be regarded as applied axially.
The effective length, KL, in the plane of end gusset
shall be taken as between 0.7 and 0.85 times the
distance between intersections, depending on the
degree of the restraint provided. The effective length,
KL, in the plane perpendicular to that of the end gusset,
shall be taken as equal to the distance between centres
of intersections. The calculated average compressive
48
stress shall not exceed the values based on 7.1.2, The
angles shall be connected together over their lengths
so as to satisfy the requirements of 7.8 and 10.2.5.
7.5.2.2 Double angle discontinuous struts connected
back-to-back, to one side of a gusset or section by one
or more bolts or rivets in each angle, or by the
equivalent in welding, shall be designed in accordance
with 7.5.1 and the angles shall be connected together
over their lengths so as to satisfy the requirements
of 7.8 and 10.2.5.
7.5.3 Continuous Members
Double angle continuous struts such as those forming
the flanges, chords or ties of trusses or trussed girders,
or the legs of towers shall be designed as axially loaded
compression members, and the effective length shall
be taken in accordance with 7.2.4.
7.5.4 Combined Stresses
In addition to axial loads, if the struts carry loads which
cause transverse bending, the combined bending and
axial stresses shall be checked in accordance with 9.3.
For determining the permissible axial and bending
stresses, the effective length shall be taken in
accordance with the 7.2 and 8.3.
7.6 Laced Columns
7.6.1 General
7.6.1.1 Members comprising two main components
laced and tied, should where practicable, have a radius
of gyration about the axis perpendicular to the plane
of lacing not less than the radius of gyration about the
axis parallel to the plane of lacing (see Fig. IOA
and 10B).
7.6.1.2 As far as practicable, the lacing system shall
be uniform throughout the length of the column.
7.6.1.3 Except for tie plates as specified in 7.7, double
laced systems (see Fig. 10B) and single laced systems
(see Fig. IOA) on opposite sides of the main
components shall not be combined with cross members
(ties) perpendicular to the longitudinal axis of the strut
(see Fig. 10C), unless all forces resulting from
deformation of the strut members are calculated and
provided for in the design of lacing and its fastenings.
7.6.1.4 Single laced systems, on opposite faces of
the components being laced together shall preferably
be in the same direction so that one is the shadow of
the other, instead of being mutually opposed in
direction.
7.6.1.5 The effective slenderness ratio, (KZA-)., of laced
columns shall be taken as 1.05 times the (KVr)o, the
actual maximum slenderness ratio, in order to account
for shear deformation effects.

IS 800:2007
A 1A
-.. . . ----
+-+
%fB
---- ---
LACING ON
FACE A
LACING ON
FACE B
PREFFERED LACING
ARWNGEMENT
10A .Wgle Laced System
LACING ON
FACE A
LACING ON
FACE B
PREFFERED LACING
ARWNGEMENT
10B Double Laced System
10C Double Laced and Single Laced System Combined with Cross Numbers
FIG. 10 LACED COLUMNS
49

IS 800:2007
7.6.2 Width of Lacing Bars
In bolted/riveted construction, the minimum width of
lacing bars shall be three times the nominal diameter
of the end boltfrivet.
7.6.3 Thickness of Lacing Bars
The thickness of flat lacing bars shall not be less than
one-fortieth of its effective length for single lacings
and one-sixtieth of the effective length for double
lacings.
7.6.3.1 Rolled sections or tubes of equivalent strength
may be permitted instead of flats, for lacings.
7.6.4 Angle of Inclination
Lacing bars, whether in double. or single systems, shall
be inclined at an angle not less than 40° nor more than
7(P to the axis of the built-up member.
7.6.5 Spacing
7.6.5.1 The maximum spacing of lacing bars, whether
connected by bolting, riveting or welding, shall also
be such that the maximum slenderness ratio of the
components of the main member (al/rl ), between
consecutive lacing connections is not greater than 50
or 0.7 times the most unfavorable slenderness ratio
of the member as a whole, whichever is less, where al
is the unsupported length of the individual member
between lacing points, and r, is the minimum radius
of gyration of the individual member being laced
together
7.6.5.2 Where lacing bars are not lapped to form the
connection to the components of the members, they
shall be so connected that there is no appreciable
interruption in the triangulation of the system.
7.6.6 Design of Lacings
7.6.6.1 The lacing shall be proportioned to resist a total
transverse shear, Vt, at any point in the member, equal
to at least 2.5 percent of the axial force in the member
and shall be divided equally among all transverse-
lacing systems in parallel planes.
7.6.6.2 For members carrying calculated bending stress
due to eccentricity of loading, applied end moments
and/or lateral loading, the lacing shall be proportioned
to resist the actual shear due to bending, in addition to
that specified in 7.6.6.1.
7.6.6.3 The slenderness ratio, KIJr, of the lacing bars
shall not exceed 145. In bolted/riveted construction,
the effective length of lacing bars for the determination
of the design strength shall be taken as the length
between the inner end fastener of the bars for single
lacing, and as 0.7 of this length for double lacings
effectively connected at intersections. In welded
construction, the effective lengths shall be taken as 0.7
times the distance between the inner ends of welds
connecting the single lacing bars to the members.
NOTE — The required section for lacing bars as compression/
tension members shall be determined by using the appropriate
design stresses, ~, subject to the requirements given in 7.6.3,
to 7.6.6 and T~in 6.1.
7.6.7 Attachment to Main Members
The bolting, riveting or welding of lacing bars to the
main members shall be sufficient to transmit the force
calculated in the bars. Where welded lacing bars
overlap the main members, the amoupt of lap measured
along either edge of the lacing bar shall be not less
than four times the thickness of the bar or the thickness
of the element of the members to which it is connected,
whichever is less. The welding should be sufficient to
transmit the load in the bar and shall, in any case, be
provided along each side of the bar for the full length
of lap.
7.6.8 End 7te Plates
Laced compression members shall be provided with
tie plates as per 7.7 at the ends of lacing systems and
at intersection with other members/stays and at points
where the lacing systems are interrupted.
7.7 Battened Columns
7.7.1 General
7.7.1.1 Compression members composed of two main
components battened should preferably have the,
individual members of the same cross-section and
symmetrically disposed about their major axis. Where
practicable, the compression members should have a
radius of gyration about the axis perpendicular to the
plane of the batten not less than the radius of gyration
about the axis parallel to the plane of the batten (see
Fig. 11).
7.7.1.2 Battened compression members, not complying
with the requirements specified in this section or those
subjected to eccentricity of loading, applied moments
or lateral forces in the plane of the battens (see Fig. 11),
shall be designed according to the exact theory of
elastic stability or empirically, based on verification
by tests.
NOTE— If the columnsectionis subjectedto eccentricityor
other moments about an axis perpendicular to battens, the
battens and the column section should be speciallydesigned
for such moments and shears.
7.7.1.3 The battens shall be placed opposite to each
other at each end of the member and at points where
the member is stayed in its length and as far as
practicable, be spaced and proportioned uniformly
throughout. The number of battens shall be such that
the member is divided into not less than three bays
50

—
within its actual length from centre-to-centre of end
connections.
00;
001
001
001
u
I
/
I
I
1
I
I
I
I
I
I
I
)0 01 100[
10 01 100
100! !00!
io oi 100’
m
d’-+ %
------1------
-----
-----
-
.{ir.--yip
_—
______
---
-—----
-______
-
I Y
I
FIG. 11 BATTENCOLUMNSECTION
7.7.1.4 The effective slenderness ratio (K!A-). of battened
columns, shall be taken as 1.1 times the (ILVr)o, the
maximum actual slenderness ratio of the column, to
account for shear deformation effects.
7.7.2 Design of Battens
7.7.2.1 Battens
Battens shall be designed to carry the bending moments
and shear forces arising from transverse shear force V[
equal to 2.5 percent of the total axial force on the whole
compression member, at any point in the length of the
member, divided equally between parallel planes of
battens. Battened member carrying calculated bending
moment due to eccentricity of axial loading, calculated
end moments or lateral loads parallel to the plane of
battens, shall be designed to carry actual shear in
addition to the above shear. The main members shall
also be checked for the same shear force and bending
moments as for the battens.
IS 800:2007
Battens shall be of plates, angles, channels, or I-sections
and at their ends shall be riveted, bolted or welded to
the main components so as to resist simultaneously a
shear Vb = VIC/NS along the column axis and a moment
M = V,C12N at each connection,
where
v, =
c=
N=
s=
transverse shear force as defined above;
distance between centre-to-centre of battens,
longitudinally;
number of parallel planes of battens; and
minimum transverse distance between the
centroid of the rivet/bolt group/welding
connecting the batten to the main
member.
7.7.2.2 Tie plates
Tie plates are members provided at the ends of battened
and laced members, and shall be designed by the same
method as battens. In no case shall a tie plate and its
fastenings be incapable of carrying the forces for which
the lacing or batten has been designed.
7.7.2.3 Size
When plates are used for battens, the end battens and
those at points where the member is stayed in its length
shall have an effective depth, longitudinally, not less
than the perpendicular distance between the centroids
of the main members. The intermediate battens shall
have an effective depth of not less than three quarters
of this distance, but in no case shall the effective depth
of any batten be less than twice the width of one
member, in the plane of the battens. The effective depth
of a batten shall be taken as the longitudinal distance
between outermost bolts, rivets or welds at the ends.
The thickness of batten or the tie plates shall be not
less than one-fiftieth of the distance between the
innermost connecting lines of rivets, bolts or welds,
perpendicular to the main member.
7.7.2.4 The requirement of bolt size and thickness of
batten specified above does not apply when angles,
channels or I-sections are used for battens with their legs
or flanges perpendicular to the main member. However,
it should be ensured that the ends of the compression
members are tied to achieve adequate rigidity.
7.7.3 Spacing of Battens
In battened compression members where the individual
members are not specifically checked for shear stress
and bending moments, the spacing of battens, centre-
to-centre of its end fastenings, shall be such that the
slenderness ratio (KZYr) of any component over that
distance shall be neither greater than 50 nor greater
than 0.7 times the slenderness ratio of the member as a
whole about its z-z (axis parallel to the battens).
51

IS 800:2007
7.7.4 Attachment to Main Members
7.7.4.1 Welded connections
Where tie or batten plates overlap the main members,
the amount of lap shall be not less than four times the
thickness of the plate. The length of weld connecting
each edge of the batten plate to the member shall, in
aggregate, be not less than half the depth of the batten
plate. At least one-third of the weld shall be placed at
each end of this edge. The length of weld and depth of
batten plate shall be measured along the longitudinal
axis of the main member.
In addition, the welding shall be returned along the
other two edges of the plates transversely to the axis
of the main member for a length not less than the
minimum lap specified above.
7.S Compression Members Composed of Two
Components Back=to=Back
7.8.1 Compression members composed of two angles,
channels, or tees back-to-back in contact or separated
by a small distance, shall be connected together by
riveting, bolting or welding so that the ratio of most
unfavorable slenderness of each member between the
intermediate connections is not greater than 40 or 0.6
times the most unfavorable ratio of slenderness of
the strut as a whole, whichever is less (see Section 10).
7.8.2 In no case shall the ends of the strut be connected
together with less than two rivets or bolts or their
equivalent in welding, and there shall be not less than
two additional connections in between, spaced
equidistant along the length of the strut. Where the
members are separated back-to-back, the rivets or bolts
through these connections shall pass through solid
washers or packing in between. Where the legs of the
connected angles or the connected tees are 125 mm
wide or more, or where webs of channels are 150 mm
wide or over, not less than two rivets or bolts shall be
used in each connection, one on line of each gauge
mark.
7.8,3 Where these connections are made by welding,
solid packing shall be used to effect the jointing unless
the members are sufficiently close together to permit
direct welding, and the members shall be connected
by welding along both pairs of edges of the main
components.
7.8.4 The rivets, bolts or welds in these connections
shall be sufficient to carry the shear force and moments,
if any, specified for battened struts (see 7.7.3), and in
no case shall the rivets or bolts be less than 16 mm
diameter for members upto and including 10 mm thick;
20 mm diameter for members upto and including
16 mm thick; and 22 mm diameter for members over
16 mm thick.
7.8.4.1 Compression members connected by such
riveting, bolting or welding shall not be subjected to
transverse loading in a plane perpendicular to the
riveted, bolted or welded surfaces.
7.8.5 Where the components are in contact back-to-
back, the spacing of the rivets, bolts or intermittent
welds shall not exceed the maximum spacing for
compression members given in (see Section 10).
SECTION 8
DESIGN OF MEMBERS SUBJECTEDTO
BENDING
8.1 General
Members subjected to predominant bending shall have
adequate design strength to resist bending moment,
shear force, and concentrated forces imposed upon and
their combinations, Further, the members shall satisfy
the deflection limitation presented in Section 5, as
serviceability criteria, Member subjected to other
forces in addition to bending or biaxial bending shall
be designed in accordance with Section 9.
8.1.1 Effective Span of Beams
The effective span of a beam shall be taken as the
distance between the centre of the supports, except
where the point of application of the reaction is taken
as eccentric at the support, when it shall be permissible
to take the effective span as the length between the
assumed lines of the reactions.
8.2 Design Strength in Bending (Flexure)
The design bending strength of beam, adequately
supported against lateral torsional buckling (laterally
supported beam) is governed by the yield stress
(see 8.2.1). When abeam is not adequately supported
against lateral buckling (laterally un-supported beams)
the design bending strength may be governed by lateral
torsional buckling strength (see 8.2.2).
The factored design moment, M at any section, in a
beam due to external actions, shall satisfy
M<M~
where
M~ = design bending strength of the section,
calculated as given in 8.2.1.2.
8.2.1 Laterally Supported Beam
A beam may be assumed to be adequately supported
at the supports, provided the compression flange has
full lateral restraint and nominal torsional restraint at
supports supplied by web cleats, partial depth end
plates, fin plates or continuity with the adjacent span.
Full lateral restraint to compression flange may be
52

IS 800:2007
assumed to exist if the frictional or other positive
restraint of a floor connection to the compression flange
of the member is capable of resisting a lateral force
not less than 2.5 percent of the maximum force in the
compression flange of the member. This may be
considered to be uniformly distributed along the flange,
provided gravity loads constitute the dominant loading
on the member and the floor construction is capable
of resisting this lateral force.
The design bending strength of a section which is not
susceptible to web buckling under shear before yielding
(where dtw < 67&) shall be determined according
to 8.2.1.2.
8.2.1.1 Section with webs susceptible to shear buckling
before yielding
When the flanges are plastic, compact or semi-compact
but the web is susceptible to shear buckling before
yielding (titW <676), the design bending strength shall
be calculated using one of the following methods:
a) The bending moment and axial force acting
on the section maybe assumed to be resisted
by flanges only and the web is designed only
to resist shear (see 8.4).
b) The bending moment and axial force acting
on the section maybe assumed to be resisted
by the whole section. In such a case, the web
shall be designed for combined shear and
normal stresses using simple elastic theory in
case of semi-compact webs and simple plastic
theory in the case of compact and plastic
webs.
8.2.1.2 When the factored design shear force does not
exceed 0.6 V~, where V~is the design shear strength of
the cross-section (see 8.4), the design bending strength,
M~ shall be taken as:
‘d = &,zpfy 1 ?(.0
To avoid irreversible deformation under serviceability
loads, Md shall be less than 1.2 Z. fy /ymo incase of
simply supported and 1.5 Z<Yhy~o in cantilever beams;
where
P, = 1.0 for plastic and compact sections;
1% = Z#ZP for semi-compact sections;
ZP, Z. = plastic and elastic section modulii of the
cross-section, respectively;
f, = yield stress of the material; and
~mO = partial safety factor (see 5.4.1).
8.2.1.3 When the design shear force (factored), V
exceeds 0.6Vd, where V~is the design shear strength of
the cross-section (see 8.4) the design bending strength,
Md shall be taken
where
Mdv =
8.2.1.4
a)
b)
c)
8.2.1.5
M~ = Mdv
design bending strength under high shear as
defined in 9.2.
Holes in the tension zone
The effect of holes in the tension flange, on
the design bending strength need not be
considered if
@nf /Agf) ~ W/f.) (%, 4’mo ) / 0.9
where
Anf /A~~ = ratio of net to gross area of
the flange in tension,
f~fu = ratio of yield and ultimate
stress of the material, and
Yml/YmO = ratio of partial safety
factors against ultimate to
yield stress (see 5.4.1).
When the An~/A~, does not satisfy the above
requirement, the reduced effective flange area,
A#atisfying the above equation maybe taken
as the effective flange area in tension, instead
of A~r
The effect of holes in the tension region of
the web on the design flexural strength need
not be considered, if the limit given in (a)
above is satisfied for the complete tension
zone of the cross-section, comprising the
tension flange and tension region of the
web.
Fastener holes in the compression zone of the
cross-section need not be considered in design
bending strength calculation, except for
oversize and slotted holes or holes without
any fastener.
Shear lag eflects
The shear lag effects in flanges may be disregarded
provided:
a) For outstand elements (supported along one
edge), bOs LO/20; and
b) For internal elements (supported along two
edges), bis LO/ 10.
where
LO = length between points of zero moment
(inflection) in the span,
bO = width of the flange with outstand, and
bi = width of the flange as an internal element.
Where these limits are exceeded, the effective width
of flange for design strength may be calculated using
53

IS 800:2007
specialist literature, or conservatively taken as the value
satisfying the limit given above.
8.2.2 Luterally Unsupported Beams
Resistance to lateral torsional buckling need not be
checked separately (member may be treated as laterally
supported, see 8.2.1) in the following cases:
a) Bending is about the minor axis of the section,
b) Section is hollow (rectangular/ tubular) or
solid bars, and
c) In case of major axis bending, 1~~(as defined
herein) is less than 0.4.
The design bending strength of laterally unsupported
beam as governed by lateral torsional buckling is given
by:
‘d = ~b ‘pfbd
where
& = 1.0 for plastic and compact sections.
= Z@P for semi-compact sections.
ZP,Z. = plastic section modulus and elastic section
modulus with respect to extreme
compression tibre.
fbd = design bending compressive stress,
obtained as given below [see Tables 13(a)
and 13(b)]
fbd = XLTfy &O
XLT= bending stress reduction factor to
account for lateral torisonal buckling,
given by:
o,’ = 0.5[l+~L. (~” ‘0.2) +A~’2]
cxLT,the imperfection parameter is given by:
ctL~ = 0.21 for rolled steel section
~LT = 0.49 fOr welded Steel section
The non-dimensional slenderness ratio, k~T, is given
by
a LT
where
M,, =
~,. b =
V
=f,
L, b
elastic critical moment calculated in
accordance with 8.2.2.1, and
extreme fibre bending compressive stress
corresponding to elastic lateral buckling
moment (see 8.2.2.1 and Table 14).
8.2.2.1 Elastic lateral torsional buckling moment
In case of simply supported, prismatic members with
symmetric cross-section, the elastic lateral buckling
moment, MC, can be determined from:
‘Cr=m=’bzpfcrb
~,,b of non-slender rolled steel sections in the above
equation may be approximately calculated from the
values given in Table 14, which has been prepared using
the following equation:
The following simplified equation may be used in the
case of prismatic members made of standard rolled
I-sections and welded doubly symmetric I-sections,
for calculating the elastic lateral buckling moment,
MC,(see Table 14):
where
1, =
Iw =
IY,,rY=
/+’ .
h~ =
tf =
torsional constant = ~ bi t?/3 for open
section;
warping constant;
moment of inertia and radius of gyration,
respectively about the weaker axis;
effective length for lateral torsional buckling
(see 8.3);
centre-to-centre distance between flanges; and
thickness of the flange.
MC,for different beam sections, considering loading,
support condition, and non-symmetric section, shall
be more accurately calculated using the method given
in Annex E.
8.3 Effective Length for Lateral Torsional Buckling
8.3.1 For simply supported beams and girders of span
length, 1,, where no lateral restraint to the compression
flanges is provided, but where each end of the beam is
restrained against torsion, the effective length LL~of
the lateral buckling to be used in 8.2.2.1 shall be taken
as in Table 15.
54

Table 13(a) Design Bending Compressive Stress Corresponding to Lateral Buckling, fM, a~~ = 0.21
(Clause 8.2.2)
f,
f.r,b
200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
1000o 181.8 190.9 200 209.1 218.2 227.3 236.4 254.5 272.7 290.9 309.1 327.3 345.5 363,6 381.8 409.1 436.4 463.6 490.9
8000 181.8 190.9 200 209.1 218.2 227.3 236.4 254.5 272.7 290.9 309.1 327.3 345,5 363.6 381.8 409.1 436.4 463.6 490.9
6000 181.8 190.9 200 209.1 218.2 227.3 236.4 254.5 272.7 290.9 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490.9
4000 181.8 190.9 200 209.1 218.2 227.3 236.4 254.5 272.7 290.9 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490.9
2000 181.8 190.9 200 209.1 218.2 227.3 236.4 254.5 272.1 290.9 309.1 327.3 345.5 363.6 381.8 409.I 436.4 463.6 490.9
1000 169.1 179.5 186 196.5 202.9 209.1 219.8 229.1 245.5 261.8 275.1 291.3 300.5 323.6 332.2 355.9 370.9 384.8 412.4
900 169.1 179.5 186 194.5 200.7 204.5 215.1 231.6 242.7 258.9 272 291.3 300.5 316.4 328.4 339.5 366.5 380.2 392.7
800 167.3 177.5 184 190.3 196.4 206.8 212.7 224 240 258,9 268.9 284,7 293.6 301.8 324.5 335.5 349.1 370.9 387.8
700 163.6 171.8 182 188.2 192 202.3 208 226.5 237.3 250.2 259.6 278,2 286.7 294.5 305.5 327.3 340.4 352.4 363.3
600 161.8 168 176 181,9 194.2 197.7 203.3 218.9 226.4 244.4 253.5 261.8 276,4 287.3 294 306.8 322.9 333.8 343.6
500 161.8 166.1 172 179.8 185.5 188.6 200.9 208.7 218.2 232.7 244.2 248.7 259.1 269.1 274.9 286.4 296.7 301.4 314.2
450 158.2 164.2 168 173.5 183.3 186.4 191.5 206.2 215.5 224 231.8 242.2 248.7 258.2 263.5 274.1 279.3 292.1 294.5
400 150.9 162.3 166 169.4 174.5 184.1 186.7 196 204.5 215.3 222.5 229.1 238.4 243.6 248.2 257.7 261,8 264.3 274.9
350 147.3 152.7 162 165.2 170.2 172.7 179.6 188.4 193.6 200.7 210.2 212.7 221,1 225.5 229.1 233.2 240 241.1 245.5
300 143.6 147 152 154.7 161.5 163.6 167.8 175.6 182.7 186.2 194.7 196.4 196.9 203.6 206.2 212.7 213.8 217.9 220.9
250 134.5 137.5 142 144.3 148.4 152.3 153.6 160.4 163.6 165.8 170 173.5 179.6 178.2 179.5 184.1 183.3 185.5 191.5
200 121.8 124.1 126 129.6 130.9 134.1 134.7 137.5 141.8 142.5 145.3 147.3 148.5 149.1 152.7 151.4 152.7 153 157.1
150 101.8 103.1 104 104.5 106.9 106.8 108.7 109.5 111.8 113.5 114.4 114.5 117.5 116.4 118.4 118.6 117.8 120.5 122.7
100 74.5 76.4 76 77.4 76.4 77.3 78 78.9 79.1 78.5 80.4 81.8 79.5 80 80.2 81.8 82,9 83.5 83.5
90 67.3 68.7 70 69 69.8 70.5 70.9 71.3 70.9 72.7 74.2 72 72.5 72.7 72.5 73.6 74.2 74.2 73.6
80 61.8 63 62 62.7 63.3 63.6 63.8 63.6 65.5 64 64.9 65.5 65.6 65.5 64.9 65.5 65.5 64.9 68.7
70 54.5 55.4 56 56.5 56.7 56.8 56.7 56 57.3 58.2 58.7 58.9 58.7 58.2 57.3 57.3 56.7 60.3 58.9
60 47.3 47.7 48 48. I 48 50 49.6 48.4 49.1 49.5 49.5 49.1 48.4 50.9 49.6 49.1 52.4 51 49.1
50 40 40.1 40 41.8 41.5 40.9 40.2 40.7 40.9 40.7 43.3 42,5 41.5 43.6 42 40.9 43.6 41.7 44.2
40 32.7 32.5 32 33.5 32.7 34.1 33.1 33.1 32.7 34.9 34 32,7 34.5 32.7 34.4 32.7 34.9 32.5 34.4
30 25.5 24.8 26 25.1 26.2 25 26 25.5 24.5 26.2 24.7 26.2 24.2 25.5 26.7 24.5 26.2 27.8 24.5
20 16.4 17.2 18 16.7 17.5 18.2 16.5 17.8 16.4 17.5 18.5 16.4 17.3 18.2 19.1 16.4 17.5 18.5 19.6
10 9.1 9.5 8 8.4 8.7 9.1 9.5 7.6 8.2 8.7 9.3 9.8 10.4 7.3 7.6 8.2 8.7 9.3 9.8
G
m
o
0
..
N
o
0
-a
I

‘a
m
.
Table 13(b) Design Bending Compressive Stress Corresponding to Lateral Buckling, ~~, a~~ = 0.49 G
(Clause 8.2.2)
00
=
..
1 I &
fcr,b
f, s
4
200 210 220 230 240 250 260 280 300 320 340 360 380 400 420 450 480 510 540
10000 181.8 190.9 200.0 209.1 218.2 227.3 236.4 254.5 272.7 290.9 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490.9
8000 181.8 190.9 200.0 209.1 218.2 227.3 236.4 254.5 272.7
. . 290.9 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490.9
6000 181.8 190,9 200.0 209.1 218.2 227.3 236.4 254.5 272.7 290.9
. . 309.1 327,3 345.5 363,6 381.8 409.1 436.4 463.6 490.9
4000 181.8 190.9 200.0 209.1 218.2 227,3 236.4 254.5 272.7 290.9
. . . 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490.9
2000 181.8 190.9 200.0 209.1 218.2 227.3 236.4 254.5 272.7 290.9
. . .. 309.1 327.3 345.5 363.6 381.8 409.1 436.4 463.6 490,9
1000 160.0 164.2 170.0 179.8 185.5 190.9 196.2 211.3 220.9 235.6 247.3 255.3 266.0 280
. ..—. 290.2 302.7 318.5 329.2 343.6
900 154.5 164,2 170.0 173.5 183.3 188.6 193.8 203.6 218.2 226.9 238.0 252.0 262.5 269.1 282.5 290.5 305.5 319,9 333.8
800 152.7 158.5 168.0 171.5 176.7 181.8 191.5 201.1
. 210.0 224.0 234.9 242.2 252.2 258.2 271.1 282.3 296.7 306 319.1
700 150.9 154.6 160.0 169.4 172.4 177.3 182.0 196 207.3 215.3 222.5 232.4 238.4 247.3 259.6 270 279.3 292.1 304.4
600 145.5 150,8 154.0 161.0 168.0 172.7 177.3 188.4 193.6 203.6 213.3 222.5 228 236.4 244.4 253.6 261.8 273.5 274.9
500 “’ 140.0 145,1 150.0 154.7 159.3 161.4 167.8 175.6 185.5 192 200,9 206,2 214.2 218.2 225.3 229.1 240 245.7 250,4
450 134.5 141.3 144.0 148.5 152.7 156.8 160.7 168 177.3 186.2 191.6 196,4 203.8 210.9 213.8 220.9 231.3 236.5 235.6
4&”’””
“ 129.1 135.5 138.0 142.2 148.4 150 153.6 162.9 169.1 174,5 182.4 183.3 193.5 196.4 202.4 208.6 209.5 217.9 220.9
350 123.6 129.8 132.0 135.9 139.6 143.2 148.9 152.7 158.2 162.9 170 173.5 176.2 181.8 183.3 192.3 196.4 199.4 206.2
300 118.2 122.2 126.0 129.6 130.9 134.1 137.1 142.5 147.3 154.2 157.6 157.1 162.4 167.3 168 175.9 178.9 1808 181.6
250 109.1 112.6 116.0 117.1 120.0 122.7 125.3 129.8 130.9
. . 136.7 139.1 140.7 145.1 149.1 148.9 151.4 152.7 157.6 157.1
200 98.2 101.2 102.0 104.5 104.7 109.1 108.7 112 117.3 119.3 120.5 121.1 124.4 127.3 126 130.9 130.9 129.8 132.5
150 83.6 84.0 86.0 87.8 89.5 88.6 89.8 91.6 95.5 96.0 95.8 98.2 100.2 101.8 103.1 102.3 104.7 106.6 103.1
100 63.6 63.0 64.0 64.8 65.5 65.9 66.2 68.7 68.2 69.8 71.1 68.7 69.1 72.7 72.5 73.6 74.2 74.2 73.6
90 58.2 57.3 60.0 58.5 61.1 61.4 61.5 61.1 62.7 64.0 64.9 65.5 65.6 65.5 64.9
. . . 65.5 65.5 64.9 68.7
80 52.7 53.5 54.0 54.4 54.5 54.5 54.4 56 57.3 58.2 58.7 58.9 58.7 58.2 61.1 61.4 61.1 60.3 58.9
70 47.3 47.7 48.0 48.1 48.0 50.0 49.6 50.9 49.1 49.5 52.5 52.4 51.8 50.9
. 53.5 53.2 52.4 55.6 54.0
60 41.8 42.0 42.0 41.8 43.6 43,2 42.5 43.3 43.6 43.6 43.3 45.8 44.9 47.3 45.8 45.0 48.0 46.4 49.1
50 36.4 36.3 36.0 35.5 37.1 36.4 37.8 38.2 38.2 37.8 37.1 39.3 38.0 40.0 38.2 40.9 39.3 37.1 39.3
40 29.1 30.5 30.0 29.3 30.5 29.5 30.7 30.5 30.0 32.0 30.9 32.7 31.1 32.7
.. . . 30.5 32.7 30.5 32.5 34.4
30 23.6 22.9 22.0 23.0 24.0 22.7 23.6 22.9 24.5 23.3 24.7 22.9 24.2 25.5 22.9 24.5 26.2 23.2 24.5
20 16.4 I5.3 16.0 16.7 I’5.3 15.9 16.5 15.3 16.4 17.5 15.5 16.4 17.3
.. . 18.2 15.3 16.4 17.5 18.5 14.7
10 9.I 7.6 8.0 8.4 8.7 9.1 9.5 7.6 8.2 8.7 9.3 9.8 6.9 7.3 7.6 8.2 8.7 9.3 9.8

Table 14 Critical Stress,JC,, b
JClause 8.2.2.1)
1 I I
ll/tf
16 18 20 25 30 I
o I 21763.1 I 21752.7
+
21740.5 I 21733.8 1 21727.2 ! 21724.2 I
ZcI 60
1
80
— 1=
—
KLlr
8 10 12 14 35
10 22551.2 22255.1 22092.6 21994.1 21929.8 21885.7 217791
20 6220.5 5947.9 5794.5 5700.0 5637.8 5594.7 5563.8 5515.8 5489.7 5473.8 5463.5 5451.4 5444.8 5438.2 5435.1
30 3149.3 2905.9 2764.6 2676.0 2616.7 2575.3 2545.3 2498.5 2472.8 2457.1 2447.0 2434.9 2428.3 2421.7 2418.6
40 2036.1 1821.2 1693.0 I 610.8 1555.1 1515.8 1487.0 I 441.7 1416.5 1401.1 1391.0 1379.0 1372.5 1365.9 1362.8
50 1492.9 1303.2 I 187,3 1111.8 1059.9 1022.7 995.3 951.7 927.1 912.0 902.0 890.2 883.7 877.1 874.2
60 1178.0 1OQ9.5 905.0 835.6 787.4 752.4 726.4 684.6 660.9 646.1 636.4 624.7 618.2 611.7 608.7
70 973.9 823.2 728.5 664.8 620.1 587.4 562.9 522.9 500.0 485.5 476.0 464.4 458.0 451.7 448.7
80 831.3 695.4 609.2 550.7 509.1 478.4 455.3 417.2 395.1 381.2 371.8 360.5 354.1 347.7 344.7
90 725.9 602.6 523.6 469.5 430.9 402.2 380.4 344.2 322.9 309.3 300.2 289.1 282.8 276.5 273,5
100 644.7 532.0 459.3 409,3 373.2 346.4 325.8 291.4 270.9 257.7 248.8 237.9 231.8 225.5 222.5
110 580.4 476.6 409.3 362.9 329.2 303.9 284.5 251.8 232.1 219.3 210.8 200.1 194.0 187.8 184,8
120 527.9 431.9 369.5 326.0 294.5 270.7 252.3 221.2 202.4 190.1 181.6 171.2 165.2 159.I 156.2
130 484.3 395.0 ““--- , ----- , ----- , . . ... , ---- , ---- , ---- 1
3% 9 I 7CK1”T- 76:; 1– 244-- I 7767 I 1971 I 179o i 167.1 158.8 148.6 142.8 136.7 133.9
140 447.6 364.2 309.5 271.5 243.4 222.3 205.8 177.5 160.2 148.7 140.7 130.8 125.0 119.0 116.2
150 416.0 337.8 286.6 250.6 224.2 204.2 188.4 161.5 144.8 133.7 126.0 116.3 110.6 104.7 101.9
160 388.7 315.2 266.8 232.8 207.8 188.8 173.9 148.2 132.0 121.3 113.9 104.3 98.8 93.0 90.1
170 364.9 295.4 249.6 217.5 193.7 175.6 161.4 136.7 121.3 111.0 103.6 94.4 89.0 83.2 80.4
180 343.9 278.0 234.6 204.1 181.5 164.2 150.6 127.1 112.2 102.2 95.2 86.0 80.7 75.0 72.3
190 325.2 262.6 221.3 192.3 170.7 154.2 141.2 118.6 104.3 94.6 87.8 79.0 73.7 68.1 65.3
200 308.3 248.8 209.6 181.7 161.2 145.4 133.0 111.3 97.5 88.1 81.4 72.8 67.8 62.2 59.5
210 293.3 236.5 198.9 172.4 152.7 137.6 125.7 104.8 91.5 82.4 75.9 67.5 62.6 57.1 54.5
220 279.5 225.3 189.3 163.9 145.1 130.6 119.1 99.0 86.2 77.4 71.2 62.9 58.1 52.7 50.1
230 267.1 215.2 180.7 156.3 138.2 124.3 113.3 93.9 81.5 72.9 66.9 58.9 54.1 48.8 46.2
240 255.8 205.8 172.8 149.4 132.0 118.6 108.0 89.3 77.2 69.0 63.1 55.3 50.6 45.4 42.8
250 245.3 197.3 165.6 143.0 126.3 113.4 103.2 85.1 73.5 65.5 59.7 52.1 47.5 42.4 39.8
260 235.7 189.5 159.0 137.3 121.1 108.7 98.8 81.3 70.1 62.3 56.7 49.3 44.:
270 226.8 182.3 152.8 131.9 116.3 104.3 94.7 77.
8 I 39.7 I 37.2 I
91 670 I 594 I 53.9 I 46.8 t 42.2 I 37.3 I 34.8 I
.,. . I -.. . I 1 r 1 I
I
..
I I 1 I 1
1 280 218.6 175.7 147.2 126.9 111.9 100.2 91.1 74.7 64.1 56.8 51.5 44.4 40.0 35.2 32.7
.8 615 I 5A ‘1 49.2 42.2 38.1 33.2 30.8 {
290 I 210.9 I 169.4 I 141.9 I 122.3 107.8 I %.6 I 87.7 I 71.
.--- ...—.
— ---- [ ---- 1 1 1 t !
300 203.8 163.7 137.1 118.1 104.1 93.2 84.5 69.1 59.1 52.1 47.1 40.4 36.2 31.5 29.0
I
..
~
o
-1

IS 800:2007
Insitnply supported beams with intermediate lateral
restraints against lateral torsional buckling, the effective
length for lateral torsional buckling to be used
in 8.2.2.1, ~~ shall be taken as the length of the relevant
segment in between the lateral restraints. The effective
length shall be equal to 1.2 times the length of the
relevant segment in between the lateral restraints.
Restraint against torsional rotation at supports in these
beams may be provided by:
a) web or flange cleats, or
b) bearing stiffeners acting in conjunction with
the bearing of the beam, or
c) lateral end frames or external supports
providing lateral restraint to the compression
flanges at the ends, or
d) their being built into walls.
8.3.2 For beams, which are provided with members
giving effective lateral restraint to the compression
flange at intervals along the span, in addition to the
end torsional restraint required in 8.3.1, the effective
length for Iateral torsional buckIing shall be taken as
the distance, centre-to-centre of the restraint members
in the relevant segment under normal loading condhion
and 1.2 times this distance, where the load is not acting
on the beam at the shear and is acting towards the shear
centre so as to have destabilizing effect during lateral
torsional buckling deformation.
8.3.3 For cantilever beams of projecting length L, the
effective length .L~T
to be used in 8.2.2.1 shall be taken
as in Table 16 for different support conditions.
8.3.4 Where a member is provided intermediate lateral
supports to improve the lateral buckling strength, these
restraints should have sufficient strength and stiffness
to prevent lateral movement of the compression flange
at that point, relative to the end supports. The
intermediate lateral restraints should be either
connected to an appropriate bracing system capable
of transferring the restraint force to the effective lateral
support at the ends of the member, or should be
connected to an independent robust part of the structure
capable of transferring the restraint force. Two or more
parallel member requiring such lateral restraint shall
not be simply connected together assuming mutual
dependence for the lateral restraint.
The intermediate lateral restraints should be connected
to the member as close to the compression flange as
practicable. Such restraints should be closer to the
shear centre of the compression flange than to the shear
centre of the section. However, if torsional restraint
preventing relative rotation between the two flanges is
provided, the intermediate lateral restraint may be
connected at any appropriate level.
For beams which are provided with members giving
effective lateral restraint at intervals along the span,
the effective lateral restraint shall be capable of resisting
a force of 2.5 percent of the maximum force in the
compression flange taken as divided equally between
the points at which the restraint members are provided.
Further, each restraint point should be capable of
resisting 1 percent of the maximum force in the
compression flange.
8.3.4.1 In a series of such beams, with solid webs,
which are connected together by the same system of
restraint members, the sum of the restraining forces
required shall be taken as 2.5 percent of the maximum
flange force in one beam only,
8.3.4.2 In the case of a series of latticed beams, girders
or roof trusses which are connected together by the same
system of restraint members, the sum of the restraining
Table 15 Effective Length for Simply Supported Beams, L~T
(Clause 8.3. 1)
SI Conditions of Restraint at Supports Loading Condition
No. / > ~
TorsionalRestraint WarpingRestraint Destabilizing
(1) (2) (3) (4) (5)
i) Fullyrestrained Bothflangesfullyrestrained 0.70L 0.85 L
ii) Fully restrained Compression flange fully restrained 0.75 L 0.90 L
iii) Fully restrained Both flanges fully restrained 0.80 L 0.95 L
iv) Fully restrained Compressicmflange partially restrained 0.85 L 1.00L
v) Fully restrained Warping not reslrdined in both flanges 1.00L 1.20L
vi) Partially restrained by bottom flange Warping not restrained in both flanges 1.0L+2D 1.2L+2D
support connection
vii) Partially restrained by bottom flange Warping not restrained in both flanges 1.2L+2D 1.4L+2D
bearing support
NOTES
1 Torsionalrestraintpreventsrotationaboutthe longitudinalaxis.
2 Warpingrestraintpreventsrotationof the flangein its plane.
3 D is the overall depth of the beam.
58

IS 800:2007
forces required shall be taken as 2.5 percent of the
maximum force in the compression flange plus 1.25
percent of this force for every member of the series other
than the first, up to a maximum total of 7.5 percent.
8.3.5 Purlins adequately restrained by sheeting need
not be normally checked for the restraining forces
required by rafters, roof trusses or portal frames that
carry predominately roof loads provided there is
bracing of adequate stiffness in the plane of rafters or
roof sheeting which is capable of acting as a stressed
skin diaphragm.
8.3.6 In case of beams with double curvature bending,
adequate direct lateral support to the compression
flange in the hogging moment region maybe provided
as given above for simply supported beam. The effect
of support to the tension (top) flange in the hogging
moment region on lateral restraint to the compression
flange may be considered as per specialist literature.
8.4 Shear
The factored design shear force, V, in a beam due to
external actions shaIl satisfy
v< v,,
where
V~ = design strength
= v“ / ymo
where
7.,0 = partial safetY factor against shear failure
(see 5.4.1).
The nominal shear strength of a cross-section, Vn,may
be governed by plastic shear resistance (see 8.4.1) or
strength of the web as governed by shear buckling
(see 8.4.2).
8.4.1 The nominal plastic shear resistance under pure
shear is given by:
Vn= Vp
where
‘“Y
Av = shear area, and
jYW = yield strength of the web.
8.4.1.1 The shear area may be calculated as given below:
I and channel sections:
Major Axis Bending:
Hot-Rolled
Welded
—htW
—dtW
Minor Axis Bending:
Hot-Rolled or Welded — 2b t~
Rectangular hollow sections of uniform thickness:
Loaded parallel to depth (h) — A h I (b + h)
Loaded parallel to width (b) — A b i (b + h)
Circular hollow tubes of uniform thickness — 2 A I n
Plates and solid bars —A
where
A=
b=
d=
h=
tf =
tw =
cross-section area,
overall breadth of tubular section, breadth
of I-section flanges,
clear depth of the web between flanges,
overall depth of the section,
thickness of the flange, and
thickness of the web.
NOTE— Fastenerholes need not be accounted for in plastic
design shear strength calculation provided that:
If A,ndoes not satisfy the above condition, the effective shear
area may be taken as that satisfying the above limit. Block
shear failure criteria may be verified at the end connections.
Section 9 maybe referred to for design strength under combined
high shear and bending.
8.4.2 Resistance to Shear Buckling
8.4.2.1 Resistance to shear buckling shall be verified
as specified, when
/
d ~ > 67e for a web without stiffeners, and
w
> 67E
r
~ for a web with stiffeners
where
K, = shear buckling coefficient (see 8.4.2.2), and
& = ~250 fy
8.4.2.2 Shear buckling design methods
The nominal shear strength, Vn, of webs with or without
intermediate stiffeners as governed by buckling may
be evaluated using one of the following methods:
a) Simple post-critical method — The simple
post critical method, based on the shear
buckling strength can be used for webs of I-
section girders, with or without intermediate
transverse stiffener, provided that the web has
transverse stiffeners at the supports. The
nominal shem strength is given by:
Vn= Vcr
59

IS 800:2007
where
Vc,=
=
where
11 =
where
Aw =
tCr,e =
where
P=
K, =
=
=
shear force corresponding to web
buckling
Av~~
shear stress corresponding to web
buckling, determined as follows:
1) when ~Ws 0.8
Tb=&w/h
2) when 0.8< AWC 1.2
7,= [1-0.8(AW -0.8)] (~YW/fi)
non-dimensional web slenderness
ratio for shear buckling stress,
given by:
the elastic critical shear stress of the
K, n’ E
‘eb= 12(1 -/.)[dAw~w~
Poisson’s ratio, and
5.35 when transverse stiffeners are
provided only at supports
4.0 + 5.35 /(c/d)2 for cld <1.0
5.35 + 4.0 /(c/d)z for cld 21.0
where c, d are the spacing of
transverse stiffeners and depth of
the web, respectively.
b) Tension field method — The tension field
method, based on the post-shear buckling
strength, may be used for webs with
intermediate transverse stiffeners, in addition
to the transverse stiffeners at supports, provided
the panels adjacent to the panel under tension
field action, or the end posts provide anchorage
for the tension fields and if cld 21.0, where c,
d are the spacing of transverse stiffeners and
depth of the web, respectively.
In the tension field method, the nominal shear
resistance, Vn, is given by:
v“ = Vtf
where
J(, =[4 rb +0.9w,, tW~vsin @]< VP
where
‘cb =
f, =
=
~.
($=
Wtf =
fyw :
d=
c =
‘b =
Sc,s, =
where
M~, =
buckling strength, as obtained from
8.4.2.2(a)
yield strength of the tension field
obtained from
[f yw‘-3T; +y1’]0”5 -l//
1.5 r~ sin 2$
inclination of the tension field
()
=
tan-’~
c
the width of the tension field, given
by:
d cos~ + (c – SC– SJ sin @
yield stress of the web
depth of the web
spacing of stiffeners in the web
shear stress corresponding to
buckling of web 8.4.2.2(a)
anchorage lengths of tension field
along the compression and tension
flange respectively, obtained from:
[ 1-
0.5
2 M,, <c
s=— —
sin@ fyw tw
reduced plastic moment capacity of
the respective flange plate
(disregarding any edge stiffener)
after accounting for the axial force,
Nf in the flange, due to overall
bending and any external axial
force in the cross-section, and is
calculated as:
Mfr=0.25b, t,2
,fyf[]
-{ivI/(b,
~lfyl/ymo)}2]
where
bf, t~ = width and thickness of the relevant
flange respectively
fyf = yield stress of the flange
8.5 Stiffened Web Panels
8.5.1 End Panels Design (see Fig. 12)
The design of end panels in girders in which the interior
panel (panel A) is designed using tension field action
shall be carried in accordance with the provisions given
herein. In this case the end panel should be designed
60

. ..._ .,__ ----
Table 16 Effective Length, L1,Tfor Cantilever of Length, L
(Clause 8.3.3)
rOprestraint conditions
61

IS 800:2007
using only simple post critical method, according
to 8.4.2.2(a).
Additionally, the end panel along with the stiffeners
should be checked as a beam spanning between the
flanges to resist a shear force, R,f and a moment, M,f
due to tension tleld forces as given in 8.5.3. Further,
end stiffener should be capable of resisting the reaction
plus a compressive force due to the moment, equal to
M,j (see Fig. 12).
8.5.2 End Panels Designed Using Tension Field Action
(see Fig. 13 and Fig. 14)
The design of end panels in girders, which are designed
using tension field action shall be carried out in
accordance with the provisions mentioned herein. In
this case, the end panel (Panel B) shall be designed
according to 8.4.2.2(b).
Additionally it should be provided with an end post
consisting of a single or double stiffener (see Fig. 13
and Fig. 14), satisfying the following:
a) Single s~iflener (see Fig. 13) — The top of
the end post should be rigidly connected to
the flange using full streng~h welds.
The end post should be capable of resisting
the reaction plus a moment from the anchor
forces equal to 2/3 M,~ due to tension field
forces, where M,f is obtained from 8.5.3, The
width and thickness of the end post are not
to exceed the width and thickness of the
ilange.
b) Doulde sf@er (see Fig. 14) — The end post
should be checked as abeam spanning between
the flanges of the girder and capable of resisting
a shear force R,~and a moment, Mt~due to the
tension field forces as given in 8.5.3.
8.5.3 Anchor Forces
The resultant longitudinal shear, R,~,and a moment kf,~
from the anchor of tension field forces are evaluated
as given below:
where
(1
1/2
Hq = I.zsvp 1–~
P
d = web depth
If the actual factored shear force, V in the panel
designed using tension field approach is less than the
shear strength, VtFasgiven in 8.4.2.2(b), then the values
v– L,
of H~ may be reduced by the ratio v,~_ v
Cr
where
V,f =
Vcr =
the basic shear strength for the panel
utilizing tension field action as given in
8.4.2.2(b), and
critical shear strength for the panel designed
utilizing tension field action as given
in 8.4.2.2(a).
8.5.4 Panels with Openings — Panels with opening of
dimension greater than 10 percent of the minimum
panel dimension should be designed without using
tension field action as given in 8.4.2.2(b). The adjacent
panels should be designed as an end panel as given in
8.5.1 or 8.5.2, as appropriate.
,
BEARING
STIFFENER — “
PANEL B
~1 ,
“ :< ~
PANEL A d
NOTES
1 Panel A is designed utilizing tension field action as given in 8.4.2.2(b).
2 PanelII is designedwithoututilizingtension field actionas given in tMWa).
3 Bearing stiffener is designed for the compressive force due to bearing plus compressive force
given in 8.5.3.
FIG. 12 END PANELDESIGNEDNOTUSING TENSION FIELD ACTION
fj~
due to the moment M,, as

IS 800:2007
k-
c
1
I
1- j
7
BEARING
STIFFENER AND
END POST / H
PANEL A PANEL A
1! :
7
NOTES
1 Panel A is designed utilizi~g tension field action as given in 8.4.2.2(b).
2 Panel B is designed utilizing tension field action as given in 8.4,2.2(b).
3 Bearing stiffener and end post is designed for combinationof compressiveloads due to bearing and a moment equal to 2/3 M,t m
given in 8.5.3.
FIG. 13 END PANEL DESIGNED USING TENSION FIELD ACTION (SINGLE STIFFENER)
END POST
i
c
, j
T A
BEARING
~
STIFFENER
PANEL A PANEL A d
r
. 1
w///I
NOTES
1 PanelA is designed utilizing tension field action as given in 8.%2.2(b).
2 Bearing stiffener is designed for compressive force due to hewing as given in 8.4.2.2(a).
3 End post is designedfor horizontal shear R,,and moment M,, as given in 8.5.3.
FIG. 14 END PANEL DESIGNED USING TENSION FIELD ACTION (DOUBLH STIFFENER)
8.6 Design of Beams and Plate Girders with Solid
Webs
8.6.1 Minimum Web Thickness
The thickness of the web in a section shall satisfy the
following requirements:
8.6.1.1 Serviceability requirement
a) When transverse stiffeners are not provided,
~ < 200c (web connected to flanges along
rw
both longitudinal edges)
< ~ 90E (web connected to flanges along
[W
one longitudinal edge only),
b) When only transverse stiffeners are provided
(in webs connected to flanges along both
63
longitudinal edges),
1) when3d2c2d
4<200&
.
lW
2) when 0.74 d< c c d
.E < m)&w
rw
3) when c < d
4.s 270Ew
tw
4) when c > 3d, the web shall be considered
as unstiffened,
c) When transverse stiffeners and longitudinal
stiffeners at one level only are provided
(0.2 d from compression flange) according
to 8.7.13 (a)

IS 800:2007
1) when 2.U > c > d
~) when 0.74 d<c <d
zs 250 f%,
(u
3) when c <0.74 d
d) When a second longitudinal stiffener (located
:it neutral axis is provided)
d
— 5:400Ew
lW
dqrthOf the web,
thickness of the web,
spacing of transverse stiffener
(.s[/[~
Fig. 12 :md Fig. 13),
[--
.
yield stress ratio of web= ~“fl .
./:fi
and
yield stress of the web.
8.6.1.2 Compr[’ssion flange buckling requirement
[n order m avoid buckling of the compression flange into
Ihe web, the web thickness shall satisfy the following:
a) When transverse stiffeners are not provided
b) When transverse stiffeners are provided and
1) whenc21.5d
2) when c < 1.5d
where
d =
tw =
c =
E, =
depth of the web,
thickness of the web,
spacing of transverse stiffenel
(see Fig. 12 and Fig. 13),
r
250
yield stress ratio of web= —
f’)1
and
fYr = yield stress of compression
flange.
8.6.2 Sectional Properties
8.6.2.1 The effective sectional area of compression
flanges shall be the gross area with deductions for
excessive width of plates as specified for compression
members ( ree Section 7) and for open holes occurring
in a plane perpendicular to the direction of stress at
the section being considered (see 8.2.1.4).
The effective sectional area of tension flanges shall be
the gross sectional area with deductions for holes as
specified in 8.2.1.4.
The effective sectional area for parts in shear shall be
tAen as specified in 8.4.1.1.
8.6.3 Flanges
8.6.3.1 In riveted or bolted construction, flange angles
shall form as large a part of the area of the flange as
practicable (preferably not less than one-third) and the
number of flange plates shall be kept to a minimum.
1n exposed situations, where flange angles are used, at
least onc plate of the top flange shall extend over the
full length of the girder, unless the top edge of the web
is machined flush with the flange angles. Where two
or more flange plates are used, tacking rivets shall be
provided, if necessary to comply with the requirements
of Section 10,
Each flange plate shall extend beyond its theoretical
cut-off point, and the extension shall contain sufficient
rivets, bolts or welds to develop in the plate, the load
calculated for the bending moment on the girder section
(taken to include the curtailed plate) at the theoretical
cut-off point.
The outstand of flange plates, that is the projection
beyond the outer line of connections to flange angles,
channel or joist flanges or in the case of welded
constructions their projection beyond the face of the
web or tongue plate, shall not exceed the values given
in 3.7.2 (see Table 2).
In the case of box girders, the thickness of any plate,
or the aggregate thickness of two or more plates, when
these plates are tacked together to form the flange, shall
satisfy the requirements given in 3.7.2 (see Tldble 2).
8.6.3.2 Flange splices
Flange splices should preferably, not be located at
points of maximum stress. Where splice plates are
used, their area shall be not less than 5 percent in excess
of the area of the flange element spliced; their centre
of gravity shall coincide, as nearly as possible, with
that of the element spliced. There shall be enough bolts,
rivets or welds on each side of the splice to develop
64

the 10xI in the element spliced plus 5 percent but in no
case should the strength developed be less than 50
percent of’the effective strength of the material spliced.
In welded construction, flange plates shall be joined
by complete penetration butt welds, wherever possible.
These butt welds shall develop the full strength of the
plates.
8.6.3.3 Connection offianges to web
The flanges of plate girders shall be connected to the
web by sufficient rivets, bolts or welds to transmit the
maximum horizontal shear force resulting from the
bending moment gradient in the girder, combined with
any vertical loads which are directly applied to the
flange. If the web is designed using tension field
method as given in 8.4.2.2 (b), the weld should be able
to transfer the tension freld stress, j’ywacting on the
web,
8.6.3.4 Bolted/Riveted construction
For girders in exposed situations and which do not have
flange plates for their entire length, the top edge of the
web plate shall be flush with or above the angles, and
the bottom edge of the web plate shall be flush with or
set back from the angles.
8.6.3.5 Welded construction
The gap between the web plates and flange plates shall
be kept to a minimum and for fillet welds shall not
exceed 1 mm at any point before welding.
8.6.4 Webs
8.6.4.1 Effective sectional area of web of plate girder
The effective cross-sectional area shall be taken as the
full depth of the web plate multiplied by the thickness.
~()’r~ — Where webs are varied in thickness in Lhedepth of
the section by the ase of tongue plates or the like, or where the
pt-opcrrtiun
of the web included in the flange area is 25 percent
or more of the overall depth, the above approximation is not
pcnnissib]c and the maximum shear stress shall be computed
on theory,
8.6.4.2 Splice,v in vvebs
Splices and cutouts for service ducts in the webs should
prefembly not be located at points of maximum shear
force and heavy concentrated loads.
Splices in the webs of the plate girders and rolled
sections shall be designed to resist the shears and
moments at the spliced section (see Annex F).
In riveted or bolted construction, splice plates shall be
provided on each side of the web. In welded
construction, web splices shall preferably be made with
complete penetration butt welds.
8.6.4.3 Where additional plates are required to
IS 800:2007
augment the strength of the web, they shall be placed
on each side of the web and shall be equal in thickness.
The proportion of shear force assumed to be resisted
by these plates shall be limited by the amount of
horizontal shear which they can transmit to the flanges
through their fastenings, and such reinforcing plates
and their fastenings shall be carried up to the points
at which the flange without the additional plates is
adequate.
8.7 Stiffener Design
8.7.1 General
8.7.1.1 When the web of a member acting alone (that
is without stiffeners) proves inadequate, stiffeners for
meeting the following requirements should be
provided:
a)
b)
c)
d)
e)
f)
intermediate tramverse web st~fener — TO
improve the buckling strength of a slender
web due to shear (see 8.7.2).
Load carrying stiflener — To prevent local
buckling of the web due to
concentrated loading (see 8.7.3 and 8.7.5).
Bearing stl~ener — To prevent local crushing
of the web due to concentrated loading
(see 8.7.4 and 8.7.6).
Torsion stiflener — To provide torsional
restraint to beams and girders at supports
(see 8.7.9).
Diagonal stiffener — To provide local
reinforcement to a web under shear and
bearing (see 8.7.7).
Tension str’’encr— To transmit tensile forces
applied to a web through a flange (see 8.7.8).
The some stiffeners may perform more than one
function and their design should comply with the
requirements of all the functions for which designed.
8.7.1.2 O[ltstand of web sti~eners
Unless the outer edge is continuously stiffened, the
outstand f’rom the face of the web should not exceed
2ot,,E.
When the outstand of web is between 14tqEand 20t&
then the stiffener design should be on the basis of a
core section with an outstand of 14t~&,where tq
is the
thickness of the stiffener.
8.7.1.3 St(~~bearing length
The stiff bearing length of any element b,, is that length
which cannot deform appreciably in bending. To
determine b], the dispersion of load through a steel bearing
element should be taken as 45” through solid material,
such as bearing plates, flange plates, etc (see Fig. 15).
65

IS 800:2007
8.7.1.4 Eccentricity where
Where a load or reaction is applied eccentric to the
centreline of the web or where the centroid of the
stiffener does not lie on the centreline of the web, the
resulting eccentricity of loading should be accounted
for in the design of the stiffener.
8.7.1.5 Buckling resistance of stiffeners
The buckling resistance F~d should be based on the
design compressive stress fcd (see 7.1.2.1) of a strut
(curve c), the radius of gyration being taken about the
axis parallel to the web. The effective section is the
full area or core area of the stiffener (see 8.7.1.2)
together with an effective length of web on each side
of the centreline of the stiffeners, limited to 20 times
the web thickness. The design strength used should be
the minimum value obtained for buckling about the
web or the stiffener.
The effective length for intermediate transverse
stiffeners used in calculating the buckling resistance,
F~~, should be taken as 0.7 times the length, L of the
stiffener.
The effective length for load carrying web stiffeners
used in calculating the buckling resistance, FXd,
assumes that the flange through which the load or
reaction is applied is effectively restrained against
lateral movement relative to the other flange, and
should be taken as:
a) KL = 0.7 Lwhen flange is restrained against
rotation in the plane of the stiffener (by other
structural elements).
b) KL = L, when flange is not so restrained:
L= length of the stiffener.
If the load or reaction is applied to the flange by a
compression member, then unless effective lateral
restraint is provided at that point, the stiffener should
be designed as part of the compression member
applying the load, and the connection between the
column and beam flange shall be checked for the effects
of the strut action.
8.7.2 Design of Intermediate Transverse Web Stl~eners
8.7.2.1 General
Intermediate transverse stiffeners may be provided on
one or both sides of the web.
8.7.2.2 Spacing
Spacing of intermediate stiffeners, where provided,
shall comply with 8.6.1 depending on the thickness of
the web.
8.7.2.3 Outstand ofstifjleners
The outstand of the stiffeners should comply
with 8.7.1.2.
8.7.2.4 Minimum stiffeners
Transverse web stiffeners not subject to external loads
or moments should have a second moment of area, Is
about the centreline of the web, if stiffeners are on both
sides of the web and about the face of the web , if
single stiffener on only one side of the web is used
such that:
t.
w
-&-bq—
45° ,
‘ ‘< ;
I L,
X t
‘
f
I
A
FIG. 15 STIFFBEARING LENGTH, b]
66

where
d=
tw =
c =
~ > 1.5d3t;
s
C2
depth of the web;
minimum required web thickness for
spacing using tension field action, as given
in 8.4.2.1; and
actual stiffener spacing.
8.7.2.5 Buckling check on intermediate transverse web
stiffeners
Stiffeners not subjected to external loads or moments
should be checked for a stiffener force:
F, = V- VC,/y.O < F,,
where
F~~ =
v=
Vcr =
design resistance of the intermediate
stiffeners,
factored shear force adjacent to the stiffener,
and
shear buckling resistance of the web panel
designed without using tension field action
as given in 8.4.2.2(a).
Stiffeners subject to external loads and moments should
meet the conditions for load carrying web stiffeners
in 8.7.3. In addition they should satisfy the following
interaction expression:
If F~ c FX, then (F~ – FX) should be taken as zero;
where
F~ =
F~~ =
FX =
FX~ =
M~ =
Mv~ =
stiffener force given above;
design resistance of an intermediate web
stiffener corresponding to buckling about an
axis parallel to the web (see 8.7.1.5);
external load or reaction at the stiffener;
design resistance of a load carrying
stiffener corresponding to buckling about
axis parallel to the web (see 8.7.1.5);
moment on the stiffener due to
eccentrically applied load and transverse
load, if any; and
yield moment capacity of the stiffener
based on its elastic modulus about its
centroidal axis parallel to the web.
IS 800:2007
8.7.2.6 Connection of intermediate sti$eners to web
Intermediate transverse stiffeners not subject to
external loading should be connected to the web so as
to withstand a shear between each component of the
stiffener and the web (in kN/mm) of not less than:
t~/(5b, )
where
tw = web thickness, in mm; and
b, = outstand width of the stiffener, in mm.
For stiffeners subject to external loading, the shear
between the web and the stiffener due to such loading
has to be added to the above value.
Stiffeners not subject to external loads or moments may
terminate clear of the tension flange and in such a
situation the distance cut short from the line of the weld
should not be more than 4tW.
8.7.3 Load Carrying Stiffeners
8.7.3.1 Web check
Load carrying web stiffeners should be provided where
compressive forces applied through a flange by loads
or reactions exceed the buckling strength, FCdW,
of the
unstiffened web, calculated using the following:
The effective length of the web for evaluating the
slenderness ratio is calculated as in 8.7.1.5. The area
of cross-section is taken as (b, + n I) tW:
where
b] = width of stiff bearing on the flange
(see 8.7.1.3), and
n, = dispersion of the load through the web at
45°, to the level of half the depth of the cross-
section.
The buckling strength of this web about axis parallel
to the web is calculated as given in 7.1.2.1, using
curve ‘c’.
8.7.4 Bearing Stiffeners
Bearing stiffeners should be provided for webs where
forces applied through a flange by loads or reactions
exceeding the local capacity of the web at its connection
to the flange, FW, given by:
FW= (b, + n~) twf,~ll’~o
where
bl =
rq =
stiff bearing length (see 8.7.1.3),
length obtained by dispersion through the
67

IS 800:2007
flange to the web junction at a slope of 1 :2.5
to the plane of the flange,
tw = thickness of the web, and
.~W = yield stress of the web.
8.7.5 Design of Load Carrying Stiffeners
8.7.5.1 Buckling check
The external load or reaction, FXon a stiffener should
not exceed the buckling resistance, FX~of the stiffener
as given in 8.7.1.5.
Where the stiffener also acts as an intermediate stiffener
it should be checked for the effect of combined loads
in accordance with 8.7.2.5.
8.7.5.2 Bearing check
Load carrying web stiffeners should also be of sufficient
size that the bearing strength of the stiffener, FP,~,given
below is not less than the load transferred, FX
F,,, = A,fy,/ (0.8y~0 ) 2 F,
where
Fx = external load or reaction,
A~ = area of the stiffener in contact with the
flange, and
~Y~ = yield stress of the stiffener.
8.7.6 Design of Bearing Sti#eners
Bearing stiffeners should be designed for the applied
load or reaction less the local capacity of the web as
given in 8.7.4. Where the web and the stiffener material
are of different strengths the lesser value should be
assumed to calculate the capacity of the web and the
stiffener. Bearing stiffeners should project nearly as
much as the overhang of the flange through which load
is transferred.
8.7.7 Design of Diagonal Stiffeners
Diagonal stiffeners should be designed to carry the
portion of the applied shear and bearing that exceeds
the capacity of the web.
Where the web and the stiffener are of different
strengths, the value for design should be taken as given
in 8.7.6.
8.7.8 Design of Tension Sti#eners
Tension stiffeners should be designed to carry the
portion of the applied load or reaction less the capacity
of the web as given in 8.7.4 for bearing stiffeners.
Where the web and the stiffener are of different
strengths, the value for design should be taken as given
in 8.7.6.
8.7.9 Torsional Stiffeners
Where bearing stiffeners are required to provide
torsional restraint at the supports of the beam, they
should meet the following criteria:
a) Conditions of 8.7.4, and
b) Second moment of area of the stiffener section
about the centreline of the web, 1, should be
such that:
1, 2 o.34a, D3TC’
where
U, =
=
=
D=
TC~ =
KL =
‘Y =
8.7.10 Connection
Bearing Stiffeners
0.006 for L~~ It-ys 50,
0.3/( ~~ /rY) for 50< ~~ /rY= 100,
30/( L~~ /rY )2for L~~ Jry >100,
overall depth of beam at support,
maximum thickness of
compression flange in the span
under consideration,
laterally unsupported effective
length of the compression flange
of the beam, and
radius of gyration of the beam
about the minor axis.
to Web of Load Carrying and
Stiffeners, which resist loads or reactions applied
through a flange, should be connected to the web by
sufficient welds or fasteners to transmit a design force
equal to the lesser of:
a) tension capacity of the stiffene~ and
b) sum of the forces applied at the two ends of
the stiffener when they act in the same
direction or the larger of the forces when they
act in opposite directions.
Stiffeners, which do not extend right across the web,
should be of such length that the shear stress in the
web due to the design force transmitted by the stiffener
does not exceed the shear strength of the web. In
addition, the capacity of the web beyond the end of
the stiffener should be sufficient to resist the applied
force.
8.7.11 Connection to Flanges
8.7.11.1 In tension
Stiffeners required to resist tension should be connected
to the flange transmitting the load by continuous welds
or non-slip fasteners.
8.7.11.2 In compression
Stiffeners required to resist compression should
68

- ...k _
,,
‘----&
either be fitted against the loaded flange or
connected by continuous welds or non-slip fasteners.
The stiffener should be fitted against or connected to
both flanges when:
a) a load is applied directly over a support, or
b) it forms the end stiffener of a stiffened web,
or
c) it acts as a torsion stiffener.
8.7.12 Hollow Sections
Where concentrated loads are applied to hollow
sections consideration should be given to local stresses
and deformations and the section reinforced as
necessary.
8.7.13 Horizontal Stiffeners
Where horizontal stiffeners are used in addition to
vertical stiffeners, they shall be as follows:
a)
b)
c)
d)
One horizontal stiffener shall be placed on the
web at a distance from the compression flange
equal to 1/5 of the distance from the
compression flange angle, plate or tongue
plate to the neutral axis when the thickness
of the web is less than the limits specified
in 8.6.1. The stiffener shall be designed so
that I, is not less than 4ctW>
where 1, and tWare
as defined in 8.7.2.4 and c is the actual
distance between the vertical stiffeners
A second horizontal stiffener (single or
double) shall be placed at the neutral axis of
the girder when the thickness of the web is
less than the limit specified in 8.6.1. This
stiffener shall be designed so that 1, is not less
than dz tWJwhere I, and tware as defined
in 8.7.2.4 and dz is twice the clear distance
from the compression flange angles, plates or
tongue plates to the neutral axis;
Horizontal web stiffeners shall extend
between vertical stiffeners, but need not be
continuous over them; and
Horizontal stiffeners may be in pairs arranged
on each side of the web, or single located on
one side of the web.
8.8 Box Girders
The design and detailing of box girders shall be such
as to give full advantage of its higher load carrying
capacity. Box girder shall be designed in accordance
with specialist literature. The diaphragms and
horizontal stiffeners should conform to 8.7.12
and 8.7.13.
8.8.1 All diaphragms shall
transfer the resultant shears
be connected such as to
to the web and flanges.
IS 800:2007
8.8.2 Where the concentrated or moving load does not
act directly on top of the web, the local effect shall be
considered in the design of flanges and the diaphragms.
8.9 Purlins and Sheeting Rails (Girts)
All purlins shall be designed in accordance with the
requirements for uncased beams as specified in 8.2.1
and 8.2.2, and the limitations of bending stress based
on lateral instability of the compression flange and the
limiting deflection specified under 5.6.1 for the design
of purlins. The maximum bending moment shall not
exceed the values specified in 8.2.1. The calculated
deflections should not exceed those permitted for the
type of roof cladding used as specified in 5.6.1. In
calculating the bending moment, advantage may be
taken of the continuity of the purlin over supports. The
bending about the two axes should be determined
separately and checked according to the biaxial
bending requirements specified in Section 9.
8.10 Bending in a Non-principal Plane
8.10.1 When the flexural deflection of a member is
constrained to a non-principal plane by lateral restraints
preventing lateral deflection, then the force exerted by
the restraints shall be determined, and the principal
axes bending moments acting on the member shall be
calculated from these forces and applied forces, by a
rational analysis. The combined effect of bending
about the principal axes shall satisfy the requirements
of Section 9.
8.10.2 When the deflections of a member loaded in a
non-principal plane are unconstrained; the principal
axes bending moments shall be calculated by a rational
analysis. The combined effect of bending about the
principal axes shall satisfy the requirements of
Section 9.
SECTION 9
MEMBER SUBJECTED TO COMBINED
FORCES
9.1 General
This section governs the design of members subjected
to combined forces, such as shear force and bending,
axial force and bending, or shear force, axial force and
bending.
9.2 Combined Shear and Bending
9.2.1 No reduction in moment capacity of the section is
necessary as long as the cross-section is not subjected
to high shear force (factored value of applied shear force
is less than or equal to 60 percent of the shear strength
of the section as given in 8.4). The moment capacity
may be tiiken as, M~ (see 8.2) without any reduction.
69

IS 800:2007
9.2.2 When the factored value of the applied shear force
is high (exceeds the limit specified in 9.2.1), the
factored moment of the section should be less than the
moment capacity of the section under higher shear
force, lkf~,, calculated as given below:
a) Plastic or Compact Section
M,, = Jf, – P(%–W,) ~1.’2-%f,/Ymo
where
p=
M~ =
v=
Vd =
Mfd =
Ze =
(2v/vd-1)2
plastic design moment of the
whole section disregarding high
shear force effect (see 8.2.1.2)
considering web buckling effects
(see 8.2.1.1),
factored applied shear force as
governed by web yielding or web
buckling,
design shear strength as governed
by web yielding or web buckling
(see 8.4.1 or 8.4.2),
plastic design strength of the area
of the cross-section excluding the
shear area, considering partial
safety factor ymO,and
elastic section modulus of the
whole section.
b) Semi-compact Section
~dv = Z fvi y.,
9.3 Combined Axial Force and Bending Moment
Under combined axial force and bending moment, section
strength as governed by material failure and member
strength as governed by buckling failure shall be checked
in accordance with 9.3.1 and 9.3.2 respectively.
9.3.1 Section Strength
9.3.1.1 Plastic and compact sections
In the design of members subjected to combined axial
force (tension or compression) and bending moment,
the following should be satisfied:
(-4J+(*’h)
Conservatively, the following equation may also be
used under combined axial force and bending moment:
where
MY,M, =
M~~Y,
Mn~Z=
N=
N~ =
M~Y,M~Z =
A~ =
a,, (X2 =
Klo =
factored applied moments about the
minor and major axis of the cross-section,
respectively;
design reduced flexural strength under
combined axial force and the respective
uniaxial moment acting alone (see
9.3.1.2);
factored applied axial force (Tension, T
or Compression, P);
design strength in tension, Tdas obtained
from 6 or in compression due to yielding
given by N, = A~.fYlY~O;
design strength under corresponding
moment acting alone (see 8.2);
gross area of the cross-section;
constants as given in Table 17; and
partial factor of safety in yielding.
9.3.1.2 For plastic and compact sections without bolts
holes, the following approximations may be used for
evaluating Mn~Yand Mn~Z:
a)
b)
c)
d)
e)
Plates
Mn~ = M~(l –n2)
Welded I or H sections
[( )]
2
Mn,Y = M,, 1- ~ 5 MdYwhere n > a
M .~Z= M~Z(1 -n)/(1 –0.5a) SM~Z
where
n = N/N~ anda = (A–2bt~)/A <0.5
For standard I or H sections
for n s 0.2 M.,, = M,,
for n >0.2 MtiY = 1.56 MdY(l -n)(n +0.6)
Mnd, = l.ll MdZ(l–n)SM,Z
For rectangular hollow sections and welded
box sections
When the section is symmetric about both
axes and without bolt holes
Mti, = M~, (1 -n)/(1 -0.5a,) <MdY
Mm,, = M,: (1 – n) /(1 – 0.5aW) < M~Z
where
aW=(A-2bt~)/A <0.5
a, =(A-2htW)/A <0.5
Circular hollow tubes without bolt holes
Mn~ = 1.04M~ (1–n17) <M~
70

....__
. ,_,
___
-
9.3.1.3 Semi-compact section
In the absence of high shear force (see 9.2.1), semi-
compact section design is satisfactory under combined
axial force and bending, if the maximum longitudinal
stress under combined axial force and bending, ~,
satisfies the following criteria:
f. ~fy%o
For cross-section without holes, the above criteria
reduces to,
N ~, ~<lo
~+mfdy
‘Mdz
– “
where
N~, M~Y,M~z are as defined in 9.3.1.1.
Table 17 Constants al and CCz
(Clause 9.3.1.1)
s] Section al CZ2
No.
(1) (2) (3) (4)
i) I and channel 5n>) 2
ii) Circular tubes 2 2
iii) Rectanguku’ 1.661 1.66/
tubes (1–1.13rr2)< 6 (1-1 .13n’)<6
iv) Solid rectangles 1.73+1.8rr] 1.73+1.8n3
NOTE.— n =NINA.
9.3.2 Overall Member Strength
Members subjected to combined axial force and
bending moment shall be checked for overall buckling
failure as given in this section.
9.3.2.1 Bending and axial tension
The reduced effective moment, M.f~,under tension and
bending calculated as given below, should not exceed
the bending strength due to lateral torsional buckling,
M~ (see 8.2.2).
Me,, = [M– VT Zec/A]s M~
where
M,T=
A=
Zec =
factored applied moment and tension,
respectively:
area of cross-section;
elastic section modulus of the section
IS 800:2007
with respect to extreme compression
fibre; and
v = 0.8, if T and M can vary independently,
or otherwise
= 1.0.
9.3.2.2 Bending and axial compression
Members subjected to combined axial compression and
biaxial bending shall satisfy the following interaction
relationships:
C~YMY M
:+KY z <1.()
—+K~~—
liy M,, MdZ
C’~YMY C M
;+ 0.6 KY —+KZ ~<1.()
di M,, M~Z
where
C~Y,Cm, = equivalent uniform moment factor as per
Table 18;
P = applied axial compression under factored
load;
MY,M,= maximum factored applied bending
moments about y and z-axis of the
member, respectively;
P~v P~Z= design strength under axial compression
...
MdY,Ma, =
KY =
K. =
K~~ =
where
nY nZ =
c mLT =
as governed by buckling about minor (y)
and major (z) axis respectively;
design bending strength about y (minor)
or z (major) axis considering laterally
unsupported length of the cross-section
(see Section 8);
1+ (AY– 0.2)nY< 1 + 0.8 nY;
1 + (AZ– 0.2)nZ< 1+ 0.8 n.; and
O.IALTn, 0.1 ny
1- (Cm,, - 0.25) 21- (C.,T- 0.25)
ratio of actual applied axial force to the
design axial strength for buckling about
the y and z axis, respectively, and
equivalent uniform moment factor for
lateral torsional buckling as per Table 18
corresponding to the actual moment
gradient between lateral supports against
torsional deformation in the critical
region under consideration.
71

--J
w
Table 18 Equivalent Uniform Moment Factor
u
?/s
m
(Clause 9.3.2.2)
a
o
..
M
I
o
~
Bending Moment Riigmm
(1)
M
VM
‘L
r- I/A4n
‘L $
Range
cm,, C&, C“LT
Uniform Loading Concentrated Load
(2) (3) (4)
–l~ry~l 0.6 ~ 0.4 yJk O.4
i
o~c@l -l~ysl 0,2 + ().8&2 0.4 0.2 + 0.8as20.4
——.. -—.-— ..—
o<~sl O.l– O.8a,20.4 -0.8 a, 20.4
–1 ~a,~O
-.l~y~o O.1(1-yr) +.8 a,> 0.4 0.2(1–@ -0.8 G 20.4
o<~’:1 -l~y,~l 0.095 – 0.05 uh 0.90 + O.io ah
-.—— _.. —_. —. ._ ———. —— -—
._. —__— ..- .-— —- —
_.—.. —
o~lp~l 0095 + 0.05 al, 0.90 + 0.10 ah
–1 <a$~O
–l<yf~o 0.95 + 0.05 ah (1+2 @ 0.90 + 0.050+ (1+2@
For members with sway bockling mode, the equivalent uniform moment factor C~ = Cm = 0.9.
Cm, C,~. CMLT shall be obtained according to the bending moment diagratn between the relevant braced poinh
A40ment factor Bendiag m“s
: -d
points braced in direction
Cw ~.~
cm Y-Y
“=V===J=%
ftxcm,,
(

- ------
SECTION 10
CONNECTIONS
10.1 General
10.1.1 This section deals with the design and detailing
requirements for joints between members. Connection
elements consist of components such as cleats, gusset
plates, brackets, connecting plates and connectors such
as rivets, bolts, pins, and welds. The connections in a
structure shall be designed so as to be consistent with
the assumptions made in the analysis of the structure
and comply with the requirements specified in this
section. Connections shall be capable of transmitting
the calculated design actions.
10.1.2 Where members are connected to the surface
of a web or the flange of a section, the ability of the
web or the flange to transfer the applied forces locally
should be checked and where necessary, local stiffening
provided.
10.1.3 Ease of fabrication and erection should be
considered in Ihe design of connections. Attention
should be paid to clearances necessary for field
erection, tolerances, tightening of fasteners, welding
procedures, subsequent inspection, surface treatment
md maintenance.
10.1.4 The ductility of steel assists the distribution of
forces generated within a joint. Effects of residual
stresses and stresses due to tightening of fasteners and
normal tolerances of fit-up need not therefore be
considered in connection design, provided ductile
behaviour is ensured.
10.1.5 In general, use of different forms of fasteners
to transfer the same force shall be avoided. However,
when different forms of fmteners are used to carry a
shear load or when welding and fasteners are
combined, then one form of fastener shall be normally
designed to carry the total load. Nevertheless, fully
tensioned friction grip bolts may be designed to share
the ioad with welding, provided the bolts are fully
IS 800:2007
tightened to develop necessary pretension after
welding.
10.1.6 The partial safety factor in the evaluation of
design strength of connections shall be taken as given
in Table 5.
10.2 Location Details of Fasteners
10.2.1 Clearances for Holes for Fasteners
Bolts may be located in standard size, over size, short
slotted or long slotted hole.
a)
b)
c)
Standard clearance hole — Except where
fitted bolts, bolts in low-clearance or oversize
holes are specified, the diameter of standard
clearance holes for fasteners shall be as given
in Table 19.
Over size hole — Holes of size larger than the
standard clearance holes, as given in Table
19 may be used in slip resistant connections
and hold down bolted connections, only
where specified, provided the over size holes
in the outer Ply is covered by a cover plate of
sufficiently large size and thickness and
having a hole not larger than the standard
clearance hole (and hardened washer in slip
resistant connections).
Short and long slots — Slotted holes of size
larger than the standard clearance hole, as
given in Table 19 maybe used in slip resistant
connections and hold down bolted
connections, only where specified, provided
the over size holes in the outer ply is covered
by a cover plate of sufficiently large size and
thickness and having a hole of size not larger
than the standard clearance hole (and
hardened washer in slip resistant connection).
10.2.2 Minimum Spacing
The distance between centre of fasteners shall not be
less than 2.5 times the nominal diameter of the fastener.
Table 19 Clearances for Fastener Holes
(Clause 10.2.1)
SI Nominal Size of Size of the Hole= Nominal Diameter of the Fastener+ Clearances
No. Fastener, d mm
Standard Clearance in Cher Size Clearance in the Length of the Slot
Diameter and Width Clearance in Diameter
of slot < Short Slot Long Slot >
(1) p) (3) (4) (5) (6)
i) 12– 14 1.0 3.0 4.0 2.5d
ii) 16–22 2.0 4.0 6.0 2.5 d
iii) 24 2.0 6.0 8.0 2.5d
iv) Larger than 24 3.0 8.0 10.0 2.5 d
73

IS 800:2007
10.2.3 Muxlmum Spacing not apply to fasteners interconnecting the components
10.2.3.1 The distance between the centres of any two
of back to back tension members. Where the members
adjacent fasteners shall not exceed 32t or 300 mm,
are exposed to corrosive influences, the maximum edge
distance shall not exceed 40 mm plus 4t, where t is the
whichever is less, where tis the thickness of the thinner
plate.
thickness of thinner connected plate.
10.2.3.2 The distance between the centres of two
adjacent fasteners (pitch) in a line lying in the direction
of stress, sh~ll not exceed 16t or 200 mm, whichever
is less, in tension members and 12t or 20() mm,
whichever is less, in compression members; where r is
the thickness of the thinner plate. In the case of
compression members wherein forces are transferred
through butting faces, this distance shall not exceed
4.5 times the diameter of the fasteners for a distance
equal to 1.5 times the width of the member from the
butting faces.
10.2.3.3 The distance between the centres of any two
consecutive fasteners in a line adjacent and parallel to
an edge of an outside plate shall not exceed 100 mm
plus 4t or 200 mm, whichever is less, in compression
and tension members; where t is the thickness of the
thinner outside plate.
10.2.3.4 When fasteners are staggered at equal intervals
and the gauge does not exceed 75 mm, the spacing
specified in 10.2.3.2 and 10.2.3.3 between centres of
fasteners may be increased by 50 percent, subject to
the maximum spacing specified in 10.2.3.1.
10.2.4 Edge and End Distances
10.2.4.1 The edge distance is the distance at right angles
to the direction of stress from the centre of a hole to
the adjacent edge. The end distance is the distance in
the direction of stress from the centre of a hole to the
end of the element.
In slotted holes, the edge and end distances should be
measured from the edge or end of the material to the
centre of its end radius or the centre line of the slot,
whichever is smaller. In oversize holes, the edge and
end distances should be taken as the distance from the
relevant edge/end plus half the diameter of the standard
clearance hole corresponding to the fastener, less the
nominal diameter of the oversize hole.
10.2.4.2 The minimum edge and end distances from
the centre of any hole to the nearest edge of a plate
shall not be less than 1.7 times the hole diameter in
case of sheared or hand-flame cut edges; and 1.5 times
the hole diameter in case of rolled, machine-flame cut,
sawn and planed edges.
10.2.4.3 The maximum edge distance to the nearest
line of fasteners from an edge of any un-stiffened part
should not exceed 12 tE, where c = (250/’)”2 and t is
the thickness of the thinner outer plate. This would
10.2.5 Tacking Fasteners
10.2.5.1 In case of members covered under 10.2.4.3,
when the maximum distance between centres of two
adjacent fasteners as specified in 10.2.4.3 is exceeded,
tacking fasteners not subjected to calculated stress shall
be used.
10.2.5.2 Tacking fasteners shall have spacing in a line
not exceeding 32 times the thickness of the thinner
outside plate or 300 mm, whichever is less. Where the
plates are exposed to the weather, the spacing in line
shall not exceed 16 times the thickness of the thinner
outside plale or 200 mm, whichever is less. In both
cases, the distance between the lines of fasteners shall
not be greater than the respective pitches.
10.2.5.3 All the requirements specified in 10.2.5.2 shall
generally apply to compression members, subject to
the stipulations in Section 7 affecting the design and
construction of compression members.
10.2.5.4 In tension members (see Section 6) composed
of two flats, angles, channels or tees in contact back to
back or separated back to back by a distance not
exceeding the aggregate thickness of the connected parts,
tacking fasteners with solid distance pieces shall be
provided at a spacing in line not exceeding 1000 mm.
10.2.5.5 For compression members covered in
Section 7, tack~ng fasteners in a line shall be spaced at
a distance not exceeding 600 mm.
10.2.6 Countersank Heads
For countersunk heads, one-half of the depth of the
countersinking shall be neglected in calculating the
length of the fastener in bearing in accordance
with 10.3.3. For fasteners in tension having
countersunk heads, the tensile strength shall be reduced
by 33.3 percent. No reduction is required to be made
in shear strength calculations.
10.3 Bewing Type Bolts
10.3.1 Effective Areas of Bolts
10.3.1.1 Since threads can occur in the shear plane,
the area .4Cfor resisting shear should normally be taken
as the net tensile stress area, An of the bolts. For bolts
where the net tensile stress area is not defined, An shall
be taken as the area at the root of the threads.
10.3.1.2 Where it can be shown that the threads do not
occur in the shear plane, A~ may be taken as the cross
section area, A, at the shank.
74

IS 800:2007
10.3.1.3 In the calculation of thread length, allowance
should be made for tolerance and thread run off.
10.3.2 A bolt subjected to a factored shear force ( VJ
shall satisfy the condition
v... = Vdb
where V~~is the design strength of the bolt taken as the
smaller of the value as governed by shear, V~,~
(see 10.3.3) and bearing, V,P~(see 10.3.4).
10.3.3 Shear Capacity of Bolt
The design strength of the bolt, V~,~as governed shear
strength is given by:
vdstr= ‘nsb 1 ~mb
where
Vn,b = nominal shear capacity of a bolt,
calculated as follows:
v],, =@ %)+% ‘%,)
where
~ = uitimate tensile strength of a bolt;
nn = number of shear planes with threads
intercepting the shear plane;
n, = number of shear planes without threads
intercepting the shear plane;
A,b = nominal plain shank area of the bolt; and
Anb = net shear area of the bolt at threads, may
be taken as the area corresponding to
root diameter at the thread.
10.3.3.1 L.ongjoints
When the length of the joint, lj of a splice or end
connection in a compression or tension element
containing more than two bolts (that is the distmce
between the first and last rows of bolts in the joint,
measured in the direction of the load tmnsfer) exceeds
15a!in the direction of load, the nominal shear capacity
(see 10.3.2), V~~shall be reduced by the factor ~lj, given
by:
Plj = 1.075-1, /(200 ~) but 075<Pli<10
= 1.075- o.oo5(lj /d)
where
d = Nominal diameter of the fastener.
NOTE — This provisiondoes not apply when the distribution
of shear over the length ofjoint is uniform, as in the connection
of web of a section to the flanges.
10.3.3.2 Large grip lengths
When the grip length, 1~(equal to the total thickness of
the connected plates) exceeds 5 times the diameter, d
of the bolts, the design shear capacity shall be reduced
by a factor ~1~,given by:
~,, = 8 d /(3 d+ 1,) = 8 /(3+1,/d)
~i, shall not be more than f$j given in 10.3.3.1. The
grip length, 1~shall in no case be greater than 8d.
10.3.3.3 Packing plates
The design shear capacity of bolts carrying shear
through a packing plate in excess of 6 mm shall be
decreased by a factor, ~P~given by:
~,, =(1 -0.0125 tpk)
where
tP~ = thickness of the thicker packing, in mm.
10.3.4 Bearing Capacity of the Bolt
The design bearing strength of a bolt on any plate, V~P~
as governed by bearing is given by:
where
vnpb = nominal bearing strength of a bolt
= 2.5 k~ d tfu
where
e P
—–0.25, $, 1.0;
‘b ‘s ‘mailer ‘f ~’ 3d0 u
e, p = end and pitch distances of the fastener
along bearing direction;
dO = diameter of the hole;
fub,it = Ultimate tensile stress of the bolt and the
ultimate tensile stress of the plate,
respectively;
d = nominal diameter of the bolt; and
[ = summation of the thicknesses of the
connected plates experiencing bearing
stress in the same direction, or if the bolts
are countersunk, the thickness of the
plate minus one half of the depth of
countersinking.
The bearing resistance (in the direction normal to the
slots in slotted holes) of bolts in holes other than
standard clearance holes may be reduced by
multiplying the bearing resistance obtained as above,
V~p~,by the factors given below:
a) Over size and short slotted holes – 0.7, and
b) Long slotted holes – 0.5.
NOTE — The block shear of the edge distance due to
bearing force may be checked as given in 6.4.
75

IS 800:2007
10.3.5 Tension Capacity
Aboltsubjected toafactored tensile force, Th shall
satisfy:
Th < T~h
where
T~b ‘Tnb)’mb
T,,~ = nominal tensile capacity of the bolt,
calculated as:
f).90~u~ A,, < fYb ASb (~mb f %())
where
& = ultimate tensile stress of the bolt,
~,b = yield stress of the bolt,
A. = net tensile stress area as specified in the
appropriate Indian Standard (for bolts
where the tensile stress area is not
defined, A,, shall be taken as the area at
the bottom of the threads), and
A,~ = shank area of the bolt.
10.3.6 Bolt Subjected to Combined Sheat- and Tension
A bolt required to resist both design shear force (V,~)
and design tensile force (TJ at the same time shall
satisfy:
where
V,b =
vdb =
Tb =
T~b .
factored shear force acting on the bolt,
design shear capacity (see 10.3.2),
factored tensile force acting on the bolt, and
design tension capacity (see 10.3.5).
10.4 Friction Grip Type Bolting
10.4.1 In friction grip type bolting, initial pretension
in bolt (usually high strength) develops clamping force
at the interfaces of elements being joined. The frictional
resistance to slip between the plate surfaces subjected
to clamping force opposes slip due to externally applied
shear. Friction grip type bolts and nuts shall conform
to IS 3757. Their installation procedures shall conform
to IS 4000.
10.4.2 Where slip between bolted plates cannot be
tolerated at working loads (slip critical connections),
the requirements of 10.4.3 shall be satisfied. However,
at ultimate loads, the requirements of 10.4.4 shall be
satisfied by all connections.
10.4.3 Slip Resistance
Design for friction type bolting in which slip is required
76
0 be limited, a bolt subjected only to a factored design
jhe~ force, V,~in the interface of connections at which
$Iip cannot be tolerated, shall satisfy the following:
V,f< Vd,f
where
Vd,f = Vn,f/ ymf
Vn,~ = nominal shear capacity of a bolt as
governed by slip for friction type
connection, calculated as follows:
v~,f = t%n. Kh F.
where
Pf = coefficient of friction (slip factor) as
specified in Table 20 @~= 0.55),
ne = number of effective interfaces offering
frictional resistance to s~ip,
K~ = 1.0 for fasteners in clearance hoIes,
= 0.85 for fasteners in oversized and short
slotted holes and for fasteners in long
slotted holes loaded perpendicular to the
slot,
= 0.7 for fasteners in long slotted holes
loaded parallel to the slot,
y~~ = 1.10 (if slip resistance is designed at
service load),
= 1.25 (if slip resistance is designed at
ultimate load),
F. = minimum bolt tension (proof load) at
installation and may be taken as
A.bfO>
A nh = net area of the bolt at threads, and
fO = proof stress (= 0.70~ub).
NOTE — Vn.may be evaluated at a service load or ultimate
load using appropriate partial safety factors, depending upon
whether slip resistance is required at service load or ultimate
load.
10.4.3.1 Long joints
The provision for the long joints in 10.3.3.1 shall apply
to friction grip connections also.
10.4.4 Capacity after slipping
When friction type bolts are designed not to slip only
under service loads, the design capacity at ultimate load
may be calculated as per bearing type connection
(see 10.3.2 and 10.3.3).
NOTE — The block shear resistance of the edge distance due
to bearing force may be checked as given in 6.4.
10.4.5 Tension Resistance
A friction bolt subjected to a factored tension force (Tf )
shall satisfy:

where
Tdf =
Tn~ =
where
Tf< Tdf
Tnf1 k
nominal tensile strength of the friction bolt,
calculated as:
0.9$U~An ~~YbA,b(y~ll %)
f“, =
A. =
ultimate tensile stress of the bolt;
net tensile stress area as specified in
various parts of IS 1367 (for bolts where
the tensile stress area is not defined, A.
shall be taken as the area at the root of
the threads);
A,, = shank area of the bolt; and
y~~ = partial factor of safety.
Table 20 ~pical Average Values for Coefficient
of Friction (pf)
(Clause 10.4.3)
SI Treatment of Surface Coefficient
No. of Friction,
(1) (2) &
O
ii)
iii)
iv)
v)
vi)
vii)
viii)
ix)
x)
xi)
xii)
Surfacesnottreated
Surfacesblastedwithshortor gritwith
anylooserust removed,no pitting
Surfacesblastedwithshotor grit and
hot-dipgalvanized
Surfacesblasted with shot or grit and
spray+netallizedwith zinc (thickness
50-70 jan)
Surfacesblastedwith shotor grit and
paintedwithethylzincsilicatecoat
(thickness30-60 ~)
Sandblastedsurface,atter lightrusting
painted with ethylzinc silicate coat
(thickness60-80 W)
painted with alcalizinc silicate coat
(thickness60-80 ,mn)
Surface blasted with shot or grit and
spray metallized with aluminium
(thickness>50 ,mrr)
Cleanmill scale
Sand blasted surface
Red lead painted surface
0.20
0.50
0.10
0.25
0.30
0.52
0.30
0.30
0.50
0.33
0.48
0.1
IS 800:2007
where
V,f = applied factored shear at design load,
V~f = design shear strength,
T~ = externally applied factored tension at
design load, and
T~~ = design tension strength.
10.4.7 Where prying force, Q as illustrated in Fig. 16
is significant, it shall be calculated as given below and
added to the tension in the bolt.
where
1, =
le =
where
P=
~
=
b, =
f. =
t =
f2=$[Te-fiqf0bet4]
e 271, 1;
distance from the bolt centreline to the toe
of the fillet weld or to half the root radius
for a rolled section,
distance between prying force and bolt
centreline and is the minimum
of either the end distance or the value given
by:
2 for non pre-tensioned bolt and 1 for pre-
tensioned bolt,
1.5,
effective width of flange per pair of bolts,
proof stress in consistent units, and
thickness of the end plate.
t
2Te
II
10.4.6 Combined Shear and Tension
Bolts in a connection for which slip in the serviceability
limit state shall be limited, which are subjected to a
tension force, T and shear force, V, shall satisfy:
B
ITC+Q
FIG. 16 COMBINED PRYING FORCE ANDTENSION
77

IS 800:2007
10.5 Welds and Welding
10.5.1 General
Requirements of welds and welding shall conform to
IS 816 and IS 9595, as appropriate.
10.5.1.1 End returns
Fillet welds terminating at the ends or sides of parts
should be returned continuously around the corners
for a distance of not less than twice the size of the
weld, unless it is impractical to do so. This is
particularly important on the tension end of parts
carrying bending loads.
10.5.1.2 Lap joint
In the case of lap joints, the minimum lap should not
be less than four times the thickness of the thinner part
joined or 40 mm, whichever is more. Single end fillet
should be used only when lapped parts are restrained
from openings. When end of an element is connected
only by parallel longitudinal fillet welds, the length of
the weld along either edge should not be less than the
transverse spacing between longitudinal welds.
10.5.1.3 A single fillet weld should not be subjected to
moment about the longitudinal axis of the weld.
10.5.2 Size of Weld
10.5.2.1 The size of normal fillets shall be taken as the
minimum weld leg size. For deep penetration welds,
where the depth of penetration beyond the root run is
a minimum of 2.4 mm, the size of the fillet should be
taken as the minimum leg size plus 2.4 mm.
10.5.2.2 For fillet welds made by semi-automatic or
automatic processes, where the depth of penetration is
considerably in excess of 2.4 mm, the size shall be
taken considering actual depth of penetration subject
to agreement between the purchaser and the contractor.
10.5.2.3 The size of fillet welds shall not be less than
3 mm. The minimum size of the first run or of a single
run fillet weld shall be as given in Table 21, to avoid
the risk of cracking in the absence of preheating.
10.5.2.4 The size of butt weld shall be specified by the
effective throat thickness.
10.5.3 Effective Throat Thickness
10.5.3.1 The effective throat thickness of a fillet weld
shall not be less than 3 mm and shall generally not exceed
0.7?, or 1.Otunder special circumstances, where t is the
thickness of the thinner plate of elements being welded.
Table 21 Minimum Size of First Rtm or of a
Single Run Fillet Weld
(Clause 10.5.2.3)
SI Thickness of Thicker Part Minimum Size
No. mm mm
/. —_. — —_
Over Up to and
trrcluding
(1) (2) (3) (4)
i) – 10 3
ii) 10 20 5
iii) 20 32 6
iv) 32 50 8 of first run
10 for minimum size of
weld
NOTES
1 When the minimumsizeof the fillet weld given in the table
is greater than the thickness of the thhner part, the minimum
size of the weld should be equal to the thickness of the thinner
part. The thicker part shall be adequately preheated to prevent
cracking ofthe weld.
2 Wherethe thicker part is more than 50 mm thick, special
precautions like pre-heating should be taken.
10.5.3.2 For the purpose of stress calculation in fillet
welds joining faces inclined to each other, the effective
throat thickness shall be taken as K times the fillet size,
where K is a constant, depending upon the angle
between fusion faces, as given in Table 22.
10.5.3.3 The effective throat thickness of a complete
penetration butt weld shall be taken as the thickness of
the thinner part joined, and that of an incomplete
penetration butt weld shall be taken as the minimum
thickness of the weld metal common to the parts joined,
excluding reinforcements.
10.5.4 Effective Length’or Area of Weld
10.5.4.1 The effective length of fiilet weld shall be
taken as only that length which is of the specified size
and required throat thickness, In practice the actual
length of weld is made of the effective length shown
in drawing plus two times the weld size, but not less
than four times the size of the weld.
10.5.4.2 The effective length of butt weld shall be taken
as the length of the continuous ftdl size weld, but not
less than four times the size of the weld.
Table 22 Values of K for Different Angles Between Fusion Faces
(Clause 10.5.3.2)
Angle Between Fusion Faces 60°–900 91”–100” IOI”--1O6” 1070–113° I 14“–120°
Constant, K 0.70 0.65 0.60 0.55 0.50
78

—,,.
10.5.4.3 The effective area of a plug weld shall be
considered as the nominal area of the hole in the plane
of the faying surface. These welds shall not be designed
to carry stresses.
10.5.4.4 If the maximum length /j of the side welds
transferring shear along its length exceeds 150 times
the throat size of the weld, tt, the reduction in weld
strength as per the long joint (see 10.5.7.3) should be
considered. For flange to web connection, where the
welds are loaded for the full length, the above limitation
would not apply.
10.5.5 Intermittent Welds
10.5.5.1 Unless otherwise specified, the intermittent
fillet welding shall have an effective length of not
less than four times the weld size, with a minimum
of 40 mm.
10.5.5.2 The clear spacing between the effective lengths
of intermittent fillet weld shall not exceed 12 and 16
times the thickness of thinner plate joined, for
compression and tension joint respectively, and in no
case be more than 200 mm.
10.5.5.3 Unless otherwise specified, the intermittent
butt weld shall have an effective length of not less than
four times the weld size and the longitudinal space
between the effective length of welds shall not be more
than 16 times the thickness of the thinner part joined.
The intermittent welds shall not be used in positions
subject to dynamic, repetitive and alternating stresses.
10.5.6 Weld Types and Quality
For the purpose of this code, weld shall be fillet, butt,
slot or plug or compound welds. Welding electrodes
shall conform to 1S 814.
10.5.7 Design Stresses in Welds
10.5.7.1 Shop welds
10.5.7.1.1 Fillet welds
Design strength of a fillet weld, ~W~
shall be based on
its throat area and shall be given by:
fwd ‘f.. t YIW
where
f.. = f,/&*
fu = smaller of the ultimate stress of the weld
or of the parent metal, and
y~~ = partial safety factor (see Table 5).
10.5.7.1,2 Butt welds
Butt welds shall be treated as parent metal with a
thickness equal to the throat thickness, and the stresses
shall not exceed those permitted in the parent metal.
79
IS 800:2007
10.5.7.1.3 Slot or plug welds
The design shear stress on slot or plug welds shall be
as per 10.5.7.1.1.
10.5.7.2 Site welds
The design strength in shear and tension for site welds
made during erection of structural members shall be
calculated according to 10.5.7.1 but using a partial
safety factor y~Wof 1.5.
10.5.7.3 Long joints
When the length of the welded joint, lj of a splice or
end connection in a compression or tension element is
greater than 150 t,, the design capacity of weld
(see 10.5.7.1.1), fwd shall be reduced by the factor
0.21.
Plw=l.2---#o.o
[
where
lj =
t, =
length of the joint in the direction of the
force transfer, and
throat size of the weld.
10.5.8 Fillet Weld Applied to the Edge of a Plate or
Section
10.5.8.1 Where a fillet weld is applied to the square
edge of a part, the specified size of the weld should
generally beat least 1.5 mm less than the edge thickness
in order to avoid washing down of the exposed arris
(see Fig. 17A).
10.5.8.2 Where the fillet weld is applied to the rounded
toe of a rolled section, the specified size of the weld
should generally not exceed 3/4 of the thickness of the
section at the toe (see Fig. 17B).
10.5.8.3 Where the size specified for a fillet weld is
such that the parent metal will not project beyond the
weld, no melting of the outer cover or covers shall be
allowed to occur to such an extent as to reduce the
throat thickness (see Fig. 18).
10.5.8.4 When fillet welds are applied to the edges of
a plate, or section in members subject to dynamic
loading, the fillet weld shall be of full size with its leg
length equal to the thickness of the plate or section,
with the limitations specified in 10.5.8.3.
10.5.8.5 End fillet weld, normal to the direction of force
shall be of unequal size with a throat thickness not
less than 0.5t, where t is the thickness of the part, as
shown in Fig. 19. The difference in thickness of the
welds shall be negotiated at a uniform slope.
10.5.9 Stresses Due to Individual Forces
When subjected to either compressive or tensile or

IS 800:2007
1.5 mm
17A 17B
FIG. 17 FILLET WELDS ON SQUARE EDGE OF PLATE OR ROUND TOE OF ROLLED SECTION
18A Desirable 18B Acceptable because of 18C Not Acceptable because of
Full Throat Thickness Reduced Throat Thickness
Fm. 18 FULL SIZE FILLETW ELDAPPLIIZDTO THE EDGE OF A PLATE OR SECTION
shear force alone, the stress in the weld is given by:
faorq=~
where
L=
q =
P=
t, =
lW =
calculated normal stress due to axial force,
in N/mm*;
shear stress, in N/mm*;
force transmitted (axial force Nor the shear
force Q);
effective throat thickness of weld, in mm;
and
effective length of weld, in mm.
10.5.10 Combination of Stresses
10.5.10.1 Fillet welds
10.5.10.1.1 When subjected to a combination of normal
and shear stress, the equivalent stress fe shall satisfy
the following:
where
L=
q =
normal stresses, compression or tension, due
to axial force or bending moment
(see 10.5.9), and
shear stress due to shear force or tension (see
10.5.9).
10.5.10.1.2 Check for the combination of stresses need
not be done fo~
a) side fillet welds joining cover plates and
flange plates, and
b) fillet welds where sum of normal and shear
stresses does not exceed~W~ (see 10.5.7.1.1).
10.5.10.2 Butt welds
10.5.10.2.1 Check for the combination of stresses in
butt welds need not be carried out provided that
a) butt welds are axially loaded, and
b) in single and double bevel welds the sum of
normal and shear stresses does not exceed the
design normal stress, and the shear stress does
not exceed 50 percent of the design shear
stress.
10.5.10.2.2 Combined bearing, bending and shear
Where bearing stress, fb, is combined with bending
(tensile or compressive), fb and shear stresses, q under
the most unfavorable conditions of loading in butt
welds, the equivalent stress, ~, as obtained from the
following formula, shall not exceed the values allowed
for the parent metal:
where
L=
fb =
fb, =
q =
& = Jf; +f; +f, fbr+%’
equivalent stress;
calculated stress due to bending, in N/mmz;
calculated stress due to bearing, in N/mm*;
and
shear stress, in N/mm*.
80

IS 800:2007
CHAMFER
1
h
ri
h:b = 1:2 or Flatter
FORCE
FIG, 19 END FILLETWELD NORMALTODIRECTION
ORFORCE
FORCE
10.5.11 Where a packing is welded between two
members and is less than 6 mm thick, or is too thin to
allo”w provision of adequate welds or to prevent
buckIing, the packing shall be trimmed flush with the
edges of the element subject to the design action and
the size of the welds along the edges shall be increased
over the required size by an amount equal to the
thickness of the packing. Otherwise, the packing shall
extend beyond the edges and shall be fillet welded to
the pieces between which it is fitted.
10.6 Design of Connections
Each element in a connection shall be designed so that
the structure is capable of resisting the design actions.
Connections and adjacent regions of the members shall
be designed by distributing the design action effects
such that the following requirements are satisfied:
a)
b)
c)
Design action effects distributed to various
elements shall be in equilibrium with the
design action effects on the connection,
Required deformations in the elements of the
connections are within their deformations
capacities,
All elements in the connections and the
adjacent areas of members shall be capable
of resisting the design action effects acting
on them, and
81
d) Connection elements shall remain stable
under the design action effects and
deformations.
10.6.1 Connections can be classified as rigid, semi-rigid
and flexible for the purpose of analysis and design as
per the recommendation in Annex F. Connections with
sut%cient rotational stiffness maybe considered as rigid.
Examples of rigid connections include flush end-plate
connection and extended end-plate connections.
Connections with negligible rotational stiffness may be
considered as flexible (pinned). Examples of flexible
connections include single and double web angle
connections and header plate connections. Where a
connection cannot be classified as either rigid or flexible,
it shall be assumed to be semi-rigid. Examples of semi-
rigid connections include top and seat angle connection
and top and seat angle with single/double web angles.
10.6.2 Design shall be on the basis of any rational
method supported by experimental evidence. Residual
stresses due to installation of bolts or welding normaily
need not be considered in statically loaded structures,
Connections in cyclically loaded structures shall be
designed considering fatigue as given in Section 13.
For earthquake load combinations, the connections
shall be designed to withstand the calculated design
action effects and exhibit required ductility as specified
in Section 12.

IS 800:2007
10.6.3 Beam and column splice shall be designed in
accordance with the recommendation given in F-2
and F-3.
10.7 Minimum Design Action on Connection
Connections carrying design action effects, except for
lacing connections, connections of sag rods, purlins
and girts, shall be designed to transmit the greater of
a) the design action in the member; and
b) the minimum design action effects expressed
either as the value or the factor times the
member design capacity for the minimum size
of member required by the strength limit state,
specified as follows:
1) Connections in rigid construction — a
bending moment of at least 0.5 times the
member design moment capacity
2)_ Connections to beam in simple
3)
4)
5)
construction — a shear force of at least
0.15 times the member design shear
capacity or 40 kN, whichever is lesser
Connections at the ends of tensile or
compression member — a force of at least
0.3 times the member design capacity
Splices in members subjected to axial
tension — a force of at least 0.3 times
the member design capacity in tension
Splices in members subjected to axial
compression — for ends prepared for full
contact in accordance with 17.7.1, it shall
be permissible to carry compressive
actions by bearing on contact surf?ces.
When members are prepared for full
contact to bear at splices, there shall be
sufficient fasteners to hold all parts
securely in place. The fasteners shall be
sufficient to transmit a force of at least
0,15 times the member design capacity
in axial compression.
When members are not prepared for full
contact, the splice material and its
fasteners shall be arranged to hold all
parts in line and shall be designed to
transmit a force of at least 0.3 times the
member design capacity in axial
compression.
In addition, splices located between
points of effective lateral support shall
be designed for the design axial force,
P~ plus a Jesign bending moment, not
less than the design bending moment
M,= (P, /,)/1 000
where, /, is the distance between points
of effective lateral support.
82
6) Splices injlexural members — a bending
moment of 0.3 times the member design
capacity in bending. This provision shall
not apply to splices designed to transmit
shear force only.
A splice subjected to a shear force only
shall be designed to transmit the design
shear force together with any bending
moment resulting from the eccentricity
of the force with respect to the centroid
of the group.
7) Splices in members subject to combined
actions — a splice in a member subject
to a combination of design axial tension
or design axial compression and design
bending moment shall satisfy
requirements in (4), (5) and (6) above,
simultaneously.
For earthquake load combinations, the
design action effects specified in this
section may need to be increased to meet
the required behaviour of the steel frame
and shall comply with Section 12.
10.8 Intersections
Members or components meeting at a joint shall be
arranged to transfer the design actions between the
parts, wherever practicable, with their centroidal axes
meeting at a point. Where there is eccentricity at joints,
the members and components shall be designed for
the design bending moments which result due to
eccentricity.
The disposition of fillet welds to balance the design
actions about the centroidal axis or axes for end
connections of single angle, double angle and similar
type members is not required for sta~ally loaded
members but is required for members, connection
components subject to fatigue loading.
Eccentricity between the centroidal axes of angle
members and the gauge lines for their bolted end
connections may be neglected in statically loaded
members, but shall be considered in members and
connection components subject to fatigue loading.
10.9 Choice of Fasteners
Where slip in the serviceability limit state is to be
avoided in a connection, high-strength bolts in a
friction-type joint, fitted bolts or welds shall be used.
Where a joint is subjected to impact or vibration, either
high strength bolts in a friction type joint or ordinary
bolts with locking devices or welds shall be used.
10.10 Connection Components
Connection components (cleats, gusset plates, brackets

and the like) other than connectors, shall have their
capacities assessed using the provisions of Sections 5,
6,7,8 and 9, as applicable.
10.11 Analysis of a Bolt/Weld Group
10.11.1 Bolt/Weld Group Subject to In-plane Loading
10.11.1.1 General method of analysis
The design force in a boltiweld or design force per
unit length in a boltiweld group subject to in-plane
loading shall be determined in accordance with the
following:
a) The connection plates shall be considered to
be rigid and to rotate relative to each other
about a point known as the instantaneous
centre of rotation of the group.
b) In the case of a group subject to a pure couple
only, the instantaneous centre of rotation
coincides with the group centroid. In the case
of in-plane shear force applied at the group
centroid, the instantaneous centre of the
rotation is at infinity and the design force is
uniformly distributed throughout the group.
In all other cases, either the results of
independent analyses for a pure couple alone
and for an in-plane shear force applied at the
group centroid shall be superposed, or a
recognized method of analysis shall be used.
c) The design force in a bolt or design force per
unit length at any point in the group shall be
assumed to act at right angles to the radius
from that point to the instantaneous centre,
and shall be taken as proportional to that
radius.
10.11.2 Bolt/Weld Group Subject to Out-of-Plane
Loading
The design force of a bolt in bolt group or design force
per unit length in the fillet weld group subject to out-
of-plane loading shall be determined in accordance
with the following:
a) Design force in the bolts or per unit length in
the fillet weld group resulting from any shear
force or axial force shall be considered to be
equally shared by all bolts in the group or
uniformly distributed over the length of the
fillet weld group.
b) Design force resulting from a design bending
moment shall be considered to vary linearly
with the distance from the relevant centroidal
axes:
1) In bearing type of bolt group plates in
the compression side of the neutral axis
2)
3)
IS 800:2007
and only bolts in the tension side of the
neutral axis may be considered for
calculating the neutral axis and second
moment of area.
In the friction grip bolt group only the
bolts shall be considered in the
calculation of neutral axis and second
moment of area.
The fillet weld group shall be considered
in isolation from the connected elemen~
for the calculation of centroid and second
moment of the weld length.
10.11.2.2 Alternative analysis
The design force per unit length in a fillet weld/bolt
group may alternatively be determined by considering
the fillet weld group as an extension of the connected
member and distributing the design forces among the
welds of the fillet weld group so as to satisfy
equilibrium between the fillet weld group and the
elements of the connected member.
10.11.3 Bolt/Weld Group Subject to In-plane and
Out-of-Plane Loading
The design force in a bolt or per unit length of the
weld shall be determined by the superposition of
analysis for in-plane and out-of-plane cases discussed
in 10.11.1 and 10.11.2.
10.11.3.2 Alternative analysis
The design force in a bolt or per unit length in the
fillet weld group may alternatively be determined by
considering the fillet weld group as an extension of
the connected member and proportioning the design
force per bolt or unit length in the weld group to satisfy
equilibrium between the bolt/weld group and the
elements of the connected member.
Force calculated in the most stressed bolt or highest
force per unit length of the weld shall satisfy the
strength requirements of 10.3, 10.4 or 10.5, as
appropriate.
10.12 Lug Angles
10.12.1 Lug angles connecting outstanding leg of a
channel-shaped member shall, as far as possible, be
disposed symmetrically with respect to the section of
the member.
10.12.2 In the case of angle members, the lug angles
and their connections to the gusset or other supporting
member shall be capable of developing a strength not
less than 20 percent in excess of the force in the
outstanding leg of the member, and the attachment of
the lug angle to the main angle shall be capable of
83

IS 800:2007
developing a strength not less than 40 percent in excess
of the force in the outstanding leg of the angle.
10.12.3 In the case of channel members and the like,
the lug angles and their connection to the gusset or
other supporting member shall be capable of
developing a strength of not less than 10 percent in
excess of the force not accounted for by the direct
connection of the member, and the attachment of the
lug angles to the member shall be capable of developing
20 percent in excess of that force.
10.12.4 In no case shall fewer than two bolts, rivets or
equivalent welds be used for attaching the lug angle to
the gusset or other supporting member.
10.12.5 The effective connection of the lug angle shall,
as far as possible terminate at the end of the member
connected, and the fastening of the lug angle to the
main member shall preferably start in advance of the
direct connection of the member to the gusset or other
suppc”ting member.
10.12.6 Where lug angles are used to connect an angle
member, the whole area of the member shall be taken
as effective not withstanding the requirements of
Section 6 of this standard.
SECTION 11
WORKING STRESS DESIGN
11.1 General
11.1.1 General design requirements of Section 3 shall
apply in this section.
11.1.2 Methods of structural analysis of Section 4 shall
also apply to this section. The elastic analysis method
shall be used in the working stress design.
11.1.3 The working stress shall be calculated applying
respective partial load factor for service load/working
load.
11.1.4 In load combinations involving wind or seismic
loads, the permissible stresses in steel structural
members may be increased by 33 percent. For anchor
bolts and construction loads this increase shall be
limited to 25 percent. Such an increase in allowable
stresses should not be considered if the wind or seismic
load is the major load in the load combination (such as
acting along with dead load alone).
11.2 Tension Members
11.2.1 Actual Tensile Stress
The actual tensile stress, j on the gross area of cross-
section, A~ of plates, angles and other tension members
shall be less than or equal to the smaller value of
permissible tensile stresses,jat, as given below:
Actual tensile stress, ~ = T,/A~
The permissible stress, ~,[ is smallest of the values as
obtained below:
a) As governed by yielding of gross section
~,= 0.6~
b) As governed by rupture of net section
1) Plates under tension
&t= 0.69 T,n 1A,
2) Angles under tension
&,= 0.69 T,. 1A,
c) As governed by block shear
f,, = 0.69 T,, I A,
where
T, =
As =
Tdn =
Tdb =
actual tension under working
(service) load,
gross area,
design strength in- tension of
respective plate/angle calculated in
accordance with 6.3, and
design block shear strength in
tension of respective plate/angle
calculated in accordance with 6.4.
11.3 Compression Members
11.3.1 Actual Compressive Stress
The actual compressive stress,~ at working (service) load,
P, of a compression member shall be less than or equal to
the permissible compressive stress,fiC as given below:
Actual compressive stress, fc = P, 1A.
The permissible compressive stress, f,c = 0.60 fcd
where
A. =
&d =
effective sectional area as defined in 7.3.2,
and
design compressive stress as defined in
7.1.2.1 (for angles see 7.5.1.2).
11.3.2 Design Details
Design of the compression members shall conform
to 7.3.
11.3.3 Column Bases
The provisions of 7.4 shall be followed for the design
of column bases, except that the thickness of a simple
column base, t$
shall be calculated as:
t,= 3 w (az– 0.3b2 )fb,
where
w = uniform pressure from below on the slab
base due to axial compression;
84

a,b=
f,, =
larger and smaller projection of the slab base
beyond the rectangle circumscribing the
column, respectively; and
permissible bending stress in column base
equal to 0.75fY.
11.3.4 Angle Struts
Provisions of 7.5 shall be used for design of angle
struts, except that the limiting actual stresses shall be
calculated in accordance with 11.3.1.
11.3.5 Laced and Battened Columns
The laced and battened columns shall be designed in
accordance with 7.6 and 7.7, except that the actual
stresses shall be less than the permissible stresses given
in 11.3.1.
11.4 Members Subjected to Bending
11.4.1 Bending Stresses
The actual bending tensile and compressive stresses,
fh,, ~~c at working (service) load moment, M, of a
bending member shall be less than or equaI to the
permissible bending stresses, ~,~t,ja~Crespectively, as
given herein. The actual bending stresses shall be
calculated as:
fk = M. IZ.C and fbt= % /%,
The permissible bending stresses, ~,~. or f,b~ shall be
the smaller of the values obtained from the following:
a) Laterally supported beams and beams
bending about the minor axis:
1) Plastic and compact sections
“&,cor&,, = 0.66&
2) Semi-compact sections
JJ.orjt,, = 0.60~
b) Laterally unsupported beams subjected to
major axis bending:
f&= 0.60 M, J Z,C
f,,, = 0.60 M, I Z.t
c) Plates and solid rectangles bending about
minor axis:
fah =.Lb,= o.75fy
where
z.., Zet=
f, =
M~ =
elastic section modulus for the
cross section with respect to
extreme compression and tension
fibres, respectively;
yield stress of the sect; and
design bending strength of a
laterally unsupported beam bent
about major axis, calculated in
accordance with 8.2.2.
IS 800:2007
11.4.2 Shear Stress in Bending Members
The actual shear stress, ~~ at working load, V, of a
bending member shall be less than or equal to the
permissible shear stress, ‘r,~given below:
Actual shear stress, z~ = V. i A,
The permissible shear stress is given by:
a) When subjected pure sheac
T,, = 0.40 f,
b) When subject to shear buckling (see 8.4.2.1):
T,, = 0.70 Vm/Av
where
Vn = design shear strength as given in 8.4.2.2(a), and
A,, = shear area of the cross-section as given
in 8.4.1.
11.4.3 Plate Girder
Provisions of 8.3,8.4,8.5,8.6 and 8.7 shall apply, for
the design of plate girder, except that the allowable
stresses shall conform to 11.4.1 and 11.4.2.
11.4.4 Box Girder
In design of box girder the provisions of 8.8 shall apply,
except that the allowable bending stresses shall
conform to 11.4.1.
11.5 Combined Stresses
11.5.1 Combined Bending and Shear
Reduction in allowable moment need not be considered
under combined bending and shear.
11.5.2 Combined Bending and Axial Force
Members subjected to combined axial compression and
bending shall be so proportioned to satisfy the
following requirements:
a) Member stability requirement:
f cmyf.y+K A<1O
J-+o.6Ky —
f =Y fix, ‘T Lz- “
f %fky ~ K %zfw < ~.o
++o.6Ky~ ,~-
Jacz
where
Cmy,
Cmz=
k=
fkyfbz =
JatIcy Jatcz
equivalent uniform moment
factor as per Table 18,
applied axial compressive stress
under service load,
applied compressive stresses
due to bending about the major
(Y) and minor (z) axis of the
member, respectively,
85

IS 800:2007
-kpfacz =
fabcy.& =
Ky =
Kz =
KL~ =
where
nY nZ =
c MLT =
L,T =
allowable axial compressive
stress as governed by buckling
about minor (y) and major (z)
axis, respectively,
allowable bending compressive
stresses due to bending about
minor (y) and major (z) axes of
the cross-section (see 11.4),
1 + (kY– 0.2)nY< 1 + 0.8 nY,
1 + (l,Z– 0.2)nz S 1 + 0.8 nZ,
O.lk,~ n,
1- (C~,, - 0.25) 21
0.1 ny
—
(C~L, - 0.25) ‘
ratio of actual applied axial
stress to the allowable axial
stress for buckling about the y
and z axis, respectively;
equivalent uniform moment
factor; and
non-dimensional slenderness
ratio (see 8.2.2).
b) Member strength requirement
At a support he values J&Y and ~,,, shall be
calculated using laterally supported member
and shall satisfy:
c +fk+f~z<lo
f —— —.
0.6 fy fky fk
11.5.3 Combined Bending and Axial Tension
Members subjected to both axial tension and bending
shall be proportioned so that the following condition
is satisfied:
where
&bty&btz = permissible tensile stresses under
bending about minor (y) and major (z)
axis when bending alone is acting, as
given in 11.4.1.
11.5.4 Combined Bearing, Bending and Shear Stresses
Where a bearing stress is combined with tensile or
compressive stress, bending and shear stresses under
the most unfavorable conditions of loading, the
equivalent stress, f, obtained from the following
formula, shall not exceed 0.9fY
f. = Jf:+ f,’+ f: f;+ 3T;
where
‘T
f,
f,
actual shear stress,
actual tensile stress,
yield stress, and
actual bearing stress.
The value of permissible bending stresses fbCyand fkz
to be used in the above formula shall each be ‘lesser of
the values of the maximum allowable stresses f,k and
fab~in bending about appropriate axis.
11.6 Connections
11.6.1 All design provisions of Section 10, except for
the actual and permissible stress calculations, shall
apply.
11.6.2 Actual Stresses in Fasteners
11.6.2.1 Actual stress in bolt in shear, f,b should be
less than or equal to permissible stress of the bolt, f,,b
as given below:
The actual stress in bolt in shear, Lb= V,b/A,b
The permissible stress in bolt in shear, f2.h = 0.60
Vn,b/A,b
where
V,b =
Vn,b=
A,b =
..
actual shear force under working (service)
load,
nominal shear capacity of the bolt as given
in 10.3.3, and
nominal plain shank area of the bolt.
11.6.2.2 Actual stress of bolt in bearing on any plate,
fpb should be less than or equal to the permissible
bearing stress of the boltiplate, f,pb as given below:
Actual stress of bolt in bearing on any plate,
fpb = V,blApb
The permissible bearing stress of the bolt/plate,
fiP~ = 0.60 VnP~JAPb
where
V~Pb
= nominal bearing capacity of a bolt on any
plate as given in 10.3.4, and
A pb = nominal bearing area of the bolt on any plate.
11.6.2.3 Actual tensile stress of the bolt,~b should be
less than or equal to permissible tensile stress of the
boh,f.,b as given below:
Actual tensile stress of the bolt, ~b = T, / A,~
86

IS 800:2007
The permissible tensile stress of the bolt,
where
T< = tension in boltunder working (service) load,
Tnb = design tensile capacity ofaboltas given in
10.3.5, and
A,~ = nominal plain shank area of the bolt.
11.6.2.4 Actual compressive or tensile or shear stress
of a weld,~W should be less than or equal to permissible
stress of the weld, ~~W
as given below:
The permissible stress of the weld,~,W = 0.6~Wn
where
j& = nominal shear capacity of the weld as
calculated in 10.5.7.1.1.
11.6.2.5 If the bolt is subjected to combined shear and
tension, the actual shear and axial stresses calculated
in accordance with 11.6.2.1 and 11.6.2.3 do not exceed
the respective permissible stresses ~a,~andf,[b then the
expression given below should satisfy:
[21+[2]’10
where
.f,b,~b = actual shear and tensile stresses
respectively, and
i.sbt~aib= permissible ‘hear and tensile ‘tresses
respectively.
11.6.3 Stresses in Welds
11.6.3.1 Actual stresses in the throat area of fillet welds
shall be less than or equal to permissible stresses, faw
as given below:
faw = 0.4 f,
11.6.3.2 Actual stresses in the butt welds shall be less
than the permissible stress as governed by the parent
metal welded together.
SECTION 12
DESIGN AND DETAILING FOR
EARTHQUAKE LOADS
12.1 GeneraI
Steel frames shall be so designed and detailed as to
give them adequate strength, stability and ductility to
resist severe earthquakes in all zones classified in
IS 1893 (Part 1) without collapse. Frames, which form
a part of the gravity load resisting system but are not
intended to resist the lateral earthquake loads, need
not satisfy the requirements of this section, provided
they can accommodate the resulting deformation
without premature failure.
12.2 Load and Load Combinations
12.2.1 Earthquake loads shall be calculated as per
IS 1893 (Part 1), except that the reduction factors
recommen-ded in 12.3 may be used.
12.2.2 In the limit state design of frames resisting
earthquake loads, the load combinations shall conform
to Table 4.
12.2.3 In addition the following load combination shall
be considered as required in 12.5.1.1, 12.7.3.1,
12.11.2.2 and 12.11.3.4:
a) 1.2 Dead Load (DL) + 0.5 Live Load (LL) *
2,5 Earthquake Load (EL); and
b) 0.9 Dead Load (DL) & 2.5 Earthquake Load
(EL).
12.3 Response Reduction Factor
For structures designed and detailed as per the
provision of this section, the response reduction factors
specified in Table 23 may be used in conjunction with
the provision in IS 1893 for calculating the design
earthquake forces.
Table 23 Response Reduction Factor (R) for
Building System
sl Lateral Load Resisting System R
No.
(1) (2) (?)
O Braced Frame Systems:
a) OrdtnaryConcentricallyBracedFrames 4
(OCBF)
b) SpecialConcentricallyBracedFrame 4.5
(SCBF)
c) EccentricallyBracedFrame(EBF) 5
ii) Moment Frame System:
a) OrdinaryMomentFrame(OMF) 4
b) SpecialMomentFrame(SMF) 5
12.4 Connections, Joints and Fasteners
12.4.1 All bolts used in frames designed to resist
earthquake loads shall be fully tensioned high strength
friction grip (HSFG) bolts or turned and fitted bolts.
12.4.2 All welds used in frames designed to resist
earthquake loads shall be complete penetration butt welds,
except in column splices, which shall conform to 12.5.2.
12.4.3 Bolted joints shall be designed not to share load
in combination with welds on the same faying surface.
12.5 Columns
12.5.1 Column Strength
When PjP~ is greater than 0.4, the requirements
in 12.5.1.1 and 12.5.1.2 shall be met.
87

IS 800:2007
Where
P, = required compressive strength of the
member, and
Pd = design stress in axial compression as
obtained from 7.1.2.
12.5.1.1 The required axial compressive and axial
tensile strength in the absence of applied moment, shall
be determined from the load combination in 12.2.3.
12.5.1.2 The required strength determined in 12.5.1.1
need not exceed either of the maximum load transferred
to the column considering 1.2 times the nominal
strength of the connecting beam or brace element, or
the resistance of the foundation to uplift.
12.5.2 Column Splice
12.5.2.1 A partial-joint penetration groove weld may
be provided in column splice, such that the design
strength of the joints shall be at least equal to 200 percent
of the required strefigth.
12.5.2.2 The minimum required strength for each
flange splice shall be 1.2 times j#f as showing Fig.
20, where A~ is the area of each flange in the smaller
connected column.
12.6 Storey Drift
The storey drift limits shall conform to IS 1893. The
deformation compatibility of members not designed
to resist seismic lateral load shall also conform to
IS 1893 (Part 1).
Pmjn= 1.2 fYA, Pmh = 1.2 fyA ,
t t
JI 1[
FIG. 20 PARTIALPENETRATION
GROOVEWELD IN
COLUMN SPLICE
12.7 Ordinary Concentrically Braced Frames
(OCBF)
wit,h importance factor greater than unity (1> 1.0) in
seismic zone III.
12.7.1.2 The provision in this section apply for
diagonal and X-bracing only. Specialist literature
may be consulted for V and inverted V-type bracing.
K-bracing shall not be permitted in systems to resist
earthquake.
12.7.2 Bracing Members
12.7.2.1 The slenderness of bracing members shall not
exceed 120.
12.7.2.2 The required compressive strength of bracing
member shall not exceed 0.8 times P~, where P~ is the
design strength in axial compression (see 7.1.2).
12.7.2.3 Along any line of bracing, braces shall be
provided such that for lateral loading in either direction,
the tension braces will have to resist between 30 to 70
percent of the total lateral load,
12.7.2.4 Bracing cross-section can be plastic, compact
or semi-compact, but not slender, as defined in 3.7.2.
12.7.2.5 For all built-up braces, the spacing of tack
fasteners shall be such that the unfavorable
slenderness ratio of individual element, between such
fasteners, shall not exceed 0.4 times the governing
slenderness ratio of the brace itself. Bolted connections
shall be avoided within the middle one-fourth of the
clear brace length (0.25 times the length in the middle).
12.7.2.6 The bracing members shall be designed so that
gross area yielding (see 6.2) and not the net area rupture
(see 6.3) would govern the design tensile strength.
12.7.3 Bracing Connections
12.7.3.1 End connections in bracings shall be designed
to withstand the minimum of the following:
a) A tensile force in the bracing equal to 1.2f#~;
b) Force in the brace due to load combinations
in 12.2.3; and
c) Maximum force that can be transferred to the
brace by the system.
12.7.3.2 The connection should be checked for tension
rupture and block shear under the load determined
in 12.7.3.1.
12.7.1 Ordinary concentrically braced frames (OCBF) 12.7.3.3 The connection shall be designed to withstand
should be shown to withstand inelastic deformation a moment of 1.2 times the full plastic moment of the
corresponding to a joint rotation of at least 0.02 radians braced section about the buckling axis.
without degradation in strength and stiffness below the 12.7.3.4 Gusset plates shall be checked for buckling
full yield value. Ordintuy concentrically braced frames out of their plane.
meeting the requirements of this section shall be
deemed to satisfy the required inelastic deformation. 12.8 Special Concentrically Braced Frames (SCBF)
12.7.1.1 Ordinary concentrically braced frames shall 12.8.1 Special concentrically braced frames (SCBF)
not be used in seismic zones IV and V and for buildings should be shown to withstand inelastic deformation
88

IS 800:2007
corresponding to a joint rotation of at least 0.04 radians 12.8.3.4 Gusset plates shall be checked for buckling
without degradation in strength and stiffness below the out of their plane.
full yield value. Special concentrically braced frames
12.8.4 Column
meeting the requirements of this section shall be
deemed to satisfy the required inelastic deformation. 12.8.4.1 The column sections used in special
12.8.1.1 Special concentrically braced frames (SCBF)
concentrically braced frames (SCBF) shall be plastic
as defined in 3.7.2.
mav be used in anv seismic zone [see IS 1893 (Part 1)1
. .
and for any building (importance-factor value). 12.8.4.2 Splices shall be located within the middle one-
12.8.1.2 The provision in this section apply for diagonal
third of the column clear height. Splices shall be
and X-bracing only. Specialist literature may be
designed for the forces that can be transferred to it. In
consulted for V and inverted V-type bracing. K-bracing
addition, splices in columns shall be designed to
shall not be permitted in system to resist earthquake.
develop at least the nominal shear strength of the
smaller connected member and 50 percent of the
12.8.2 Bracing Members nominal flexural strength of the smaller connected
12.8.2.1 Bracing members shall be made of E250B
section.
steel of IS 2062 only. 12.9 Eccentrically Braced Frames (EBF)
12.8.2.2 The slenderness of bracing members shall not Eccentrically braced frames (EBF) shall be designed
exceed 160 (only hangers). in accordance with specialist literature.
12.8.2.3 The required compressive strength of bracing
12.10 Ordinary Moment Frames (OMF)
member shall not exceed the design strength in axial
compression PA(see 7.1.2) 12.10.1 Ordinary moment frames (OMF) should be
12.8.2.4 Along any line of bracing, braces shall be
shown to withstand inelastic deformation
provided such that for lateral loading in either direction,
corresponding to a joint rotation of 0.02 radians without
the tension braces will resist between 30 to 70 percent
degradation in strength and stiffness below the full yield
value (MP). Ordinary moment frames meeting the
of the load.
requirements of this section shall be deemed to satisfv
12.8.2.5 Braced cross-section shall be plastic as defined
.
the required inelastic deformation.
in 3.7.2.
12.10.1.1 Ordinary moment frames (OMF) shall not
12.8.2.6 In built-up braces, the spacing of tack be used in seismic zones IV and V and for buildings
connections shall be such that the slenderness ratio of with importance factor greater than unity (1 > 1.0) in
individual element between such connections shall not seismic zone III.
exceed 0.4 times the governing slenderness ratio of
the brace itself. Bolted connection shall be avoided
12.10.2 Beam-to-Column Joinls and Connections
within the middle one-fourth of the clear brace length
(0.25 times the length, in the middle).
12.8.2.7 The bracing members shall be designed so that
gross area yielding (see 6.2) and not the net area rupture
(see 6.3) would govern the design tensile strength.
12.8.3 Bracing Connections
12.8.3.1 Bracing end connections shall be designed to
withstand the minimum of the following:
Connections are permitted to be rigid or semi-rigid
moment connections and should satisfy the criteria
in 12.10.2.1 to 12.10.2.5.
12.10.2.1 Rigid moment connections should be
designed to withstand a moment of at least 1.2 times
of either the full plastic moment of the connected beam
or the maximum moment that can be delivered by the
beam to the joint due to the induced weakness at the
ends of the beam, whichever is less.
a) A tensile force in the bracing equal to 1.l~#~; 12.10.2.2 Semi-rigid connections should be designed
and to withstand either a moment of at least 0.5 times the
b) Maximum force that can be transferred to the full plastic moment of the connected beam or the
brace by the system. maximum moment that can be delivered by the system,
12.8.3.2 The connection should be checked for tension whichever is less. The design moment shall be achieved
rupture and block shear under the load determined
within a rotation of 0.01 radians. The information given
in 12.8.3.1. in Annex F may be used for checking.
12.8.3.3 The connection shall be designed to withstand 12.10.2.3 The stiffness and strength of semi-rigid
a moment of ’1.2 times the full plastic moment of the
connections shall be accounted for in the design and
braced section about the critical buckling axis. the overall stability of the frame shall be ensured.
89

IS 800:2007
12.10.2.4 The rigid and semi-rigid connections should
be designed to withstand a shear resulting from the
load combination 1.2DL + 0.5LL plus the shear
corresponding to the design moment defined
in 12.10.2.1 and 12.10.2.2, respectively.
12.10.2.5 In rigid fully welded connections, continuity
plates (tension stiffener, see 8.7) of thickness equal to
or greater than the thickness of the beam flange shall
be provided and welded to the column flanges and web.
12.11 Special Moment Frames (SMF)
12.11.1 Special moment frames (SMF) shall be made
of E250B steel of IS 2062 and should be shown to
withstand inelastic deformation corresponding to a
joint rotation of 0.04 radians without degradation in
strength and stiffness below the full yield value (MP).
Special moment frames meeting the requirements of
this section shall be deemed to satisfy the required
inelastic deformation.
12,11.1,1 Special moment frames (SMF) maybe used
in any seismic zone [see IS 1893 (Part 1)] and for any
buildings (importance-factor values).
12.11.2 Beam-to-Column Joints and Connections
12.11.2.1 All beam-to-column connections shall be
rigid (see Annex F) and designed to withstand a
moment of at least 1.2 times the full plastic moment of
the connected beam. When a reduced beam section is
used, its minimum flexural strength shall be at least
equal to 0.8 times the full plastic moment of the
unreduced section.
12.11.2.2 The connection shall be designed to
withstand a shear resulting from the load combination
1.2DL + 0.5LL plus the shear resulting from the
application of 1.2MP in the same direction, at each end
of the beam (causing double curvature bending). The
shear strength need not exceed the required value
corresponding to the load combination in 12.2.3.
12.11.2.3 In column strong axis connections (beam and
column web in the same plane), the panel zone shall
be checked for shear buckling in accordance with 8.4.2
at the design shear defined in 12.11.2.2. Column web
doubler plates or diagonal stiffeners may be used to
strengthen the web against shear buckling.
12.11.2.4 The individual thickness of the column webs
and doubler plates, shall satisfy the following:
t > (dp+bp)/90
where
A CONTINUITY
PLATE
/
/
I
dp Ti
bP
A
FIG. 21 CONTINUITY
PLATES
12.11,2,5 Continuity plates (tension stiffner) (see 8.7)
shall be provided in all strong axis welded connections
except in end plate connection.
12.11,3 Beam and Column Limitation
12.11.3.1 Beam and column sections shall be either
plastic or compact as defined in 3.7.2. At potential
plastic hinge locations, they shall necessarily be plastic.
12.11.3.2 The section selected for beams and columns
shall satisfy the following relation:
where
~MP = sum of the moment capacity in the
column above and below the beam
centreline; and
~MP, = sum of the moment capacity in the
beams at the intersection of the beam and
column centrelines.
In tall buildings, higher mode effects shall be accounted
for in accordance with specialist literature.
12.11.3.3 Lateral support to the column at both top
and bottom beam flange levels shall be provided so as
to resist at least 2 percent of the beam flange strength,
except for the case described in 12.11.3.4.
12.11.3.4 A plane frame designed as non-sway in the
direction perpendicular to its plane, shall be checked
for buckling, under the load combination specified
in 12.2.3.
t = thickness of column web or doubler plate,
12.12 Column Bases
dP = panel-zone depth between continuity plate,
and 12.12.1 Fixed column bases and their anchor bolts
bP = panel-zone width between column flanges.
should be designed to withstand a moment of 1.2 times
90

the full plastic moment capacity of the column section.
The anchor bolts shall be designed to withstand the
combined action of shear and tension as well as prying
action, if any.
12.12.2 Both fixed and hinged column bases shall be
designed to withstand the full shear under any load
case or 1.2 times the shear capacity of the column
section, whichever is higher.
SECTION 13
FATIGUE
13.1 General
Structure and structural elements subject to loading
that could lead to fatigue failure shall be designed
against fatigue as given in this section, This shall
however not cover the following:
a)
b)
c)
d)
e)
f)
Corrosion fatigue,
Low cycle (high stress) fatigue,
Thermal fatigue,
Stress corrosion cracking,
Effects of high temperature (> 1500 C), and
Effects of low temperature (< brittle transition
temperature).
13.1.1 For the purpose of design against fatigue,
different details (of members and connections) are
classified under different fatigue class. The design
stress range corresponding to various number of cycles,
are given for each fatigue class. The requirements of
this section shall be satisfied with, at each critical
location of the structure subjected to cyclic loading,
considering relevant number of cycles and magnitudes
of stress range expected to be experienced during the
life of the structure.
13.2 Design
13.2.1 Reference Design Condition
The standard S-N curves for each detail category are
given for the following conditions:
a)
b)
c)
d)
e)
Detail is located in a redundant load path,
wherein local failure at that detail alone will
not lead to overall collapse of the structure.
Nominal stress history at the local point in
the detail is estimated/evaluated by a
conventional method without taking into
account the local stress concentration effects
due to the detail.
Load cycles are not highly irregular.
Details are accessible for and subject to
regular inspection.
Structure is exposed to only mildly corrosive
IS 800:2007
environment as in normal atmospheric
condition and suitably protected against
corrosion (pit depth c 1 mm).
f) Structure is not subjected to temperature
exceeding 150 “C.
g) Transverse fillet or butt weld connects plates
of thickness not greater than 25 mm.
h) Holes shall not be made in members and
connections subjected to fatigue.
Fatigue need not be investigated, if condition
in 13.2.2.3, 13.5.1 or 13.6 is satisfied.
The values obtained from the standard S-N curve shall
be modified by a capacity reduction factor p. when
plates greater than 25 mm in thickness are joined
together by transverse fillet or butt welding, given by:
p,= (25/tP)025 <1.0
where
tp = actual thickness in mm of the thicker plate
being joined.
No thickness correction is necessary when full
penetration butt weld reinforcements are machined
flush and proved free of defect through non-destructive
testing.
13.2.2 Design Spectrum
13.2.2.1 Stress evaluation
Design stress shall be determined by elastic analysis
of the structure to obtain stress resultants and the local
stresses may be obtained by a conventional stress
analysis method. The normal and shear stresses shall
be determined considering all design actions on the
members, but excluding stress concentration due to the
geometry of the detail. The stress concentration effect
is accounted for in detail category classification
(see Table 26). The stress concentration, however, not
characteristic of the detail shall be accounted for
separately in the stress calculation.
In the fatigue design of trusses made of members with
open sections, in which the end connections are not
pinned, the stresses due to secondary bending moments
shall be taken into account, unless the slenderness ratio
(KZfr), of the member is greater than 40.
In the determination of stress range at the end
connections between hollow sections, the effect of
connection stiffness and eccentricities may be
disregarded, provided
a) the calculated stress range is multiplied by
appropriate factor given in Table 24(a) in the
case of circular hollow section connections
and Table 24(b) in the case of rectangular
holIow section connections.
91

,,,,,, , I -. ..,..——
IS 800:2007
b) thedesign throat thickness ofiillet weldsin
the joints is greater than the wall thickness of
the connected member.
13.2.2.2 Design stress spectrum
In the case of loading events producing non-uniform
stress range cycle, the stress spectrum may be obtained
by a rational method, such as ‘rain flow counting’ or
an equivalent method.
13.2.2.3 Low fatigue
Fatigue assessment is not required for a member,
connection or detail, if normal and shear design stress
ranges, f satisfy the following conditions:
or if the actual number of stress cycles, N~c, satisfies
()
3
27 I ymfi
N~C < 5X106
Yrnf
where
k,, %, = Partial safety factors for strength and
load, respectively (see 13.2.3), and
f = actual fatigue stress range for the detail.
Table 24 (a) Multiplying Factors for Calculated
Stress Range (Circular Hollow Sections)
(Clause 13.2.2.1)
sl
No.
Type of Connection Chords Verticals Diagonals
(1) (2) (3) (4) (5)
i) Gap
{
Ktype 1.5 1.0 1.3
connections N type 1.5 1.8 I.4
ii) Overlap
{
K type 1.5 1.0 1.2
connections N type 1.5 1.65 1.25
Table 24 (b) Multiplying Factors for Calculated
Stress Range (Rectangular Hollow Sections)
(Clause 13.2.2.1)
SI Types of Joint Chords Verticals Diagonals
No.
(1) (2) (3) (4) (5)
i) Gap
{
K type 1.5 1.0 1.5
connections N type 1.5 2.2 1.6
ii) Overlap
{
K type 1.5 1.0 1.3
connections N type 1.5 2.0 I.4
13.2.3 Partial Safety Factors
13.2.3.1 Partial safety factor for actions and their
etiects (fifl)
Unless and otherwise the uncertainty in the estimation
of the applied actions and their effects demand a higher
value, the partial safety factor for loads in the evaluation
of stress range in fatigue design shall be taken as 1.0.
13.2.3.2 Partial safety factor forfatigue strength (Y~fo
Partial safety factor for strength is influenced by
consequences of fatigue damage and level of inspection
capabilities.
13.2.3.3 Based on consequences of fatigue failure,
component details have been classified as given in
Table 25 and the corresponding partial safety factor
for fatigue strength shall be used:
a) Fail-safe structural component/detail is the
one where local failure of one component due
to fatigue crack does not result in the failure
of the structure due to availability of alternate
load path (redundant system).
b) Non-fail-safe structural component/detail is
the one where local failure of one component
leads rapidly to failure of the structure due to
its non-redundant nature.
Table 25 Partial Safety Factors for Fatigue
Strength (ymn)
(Clause 13.2.3.3)
S1No. Inspection and Access Consequence of Failure
F
Fail-Safe Non-fail-Safe
(1) (2) (3) (4)
i) Periodic inspection, mainte-
nance and accessibility to 1.00 1.25
detailis good
ii) Periodic inspection, mainte-
nance and accessibility to 1.15 1.35
detail is poor
13.3 Detail Category
Tables 26 (a) to (d) indicate the classification of
different details into various categories for the purpose
of assessing fatigue strength. Details not classified in
the table may be treated as the lowest detail category
of a similar detail, unless superior fatigue strength is
proved by testing and/or analysis.
Holes in members and connections subjected to fatigue
loading shall not be made:
a)
b)
using punching in plates having thickness
greater than 12 mm unless the holes are sub-
punched and subsequently reamed to remove
the affected material around the punched hole,
and
using gas cutting unless the holes are reamed
to remove the material in the heat affected
zone.
92

IS 800:2007
13.4 Fatigue Strength
Y
~=j.o 5xI0 IN,C
The fatigue strength of the standard detail for the
norroal or shear fatigue stress range, not corrected for b) Shear stress
effects discussed in 13.2.1, is given below (see also
Fig. 22 and Fig. 23):
r
~~ =7~n55x10elN~c
a) Normal stress range where
when N~cS5 X 106
~, ~t = design normal and shear fatigue s~ess
r
range of the detail, respectively, for
$=.fk 5x1O fN~c life cycle of N~c, and
when 5 x 106 S Nsc S 108
~fn, Zfn= normal and shear fatigue strength
of the detail for 5 x 10” cycles, for
the detail category (see Table 26).
Table 26 (a) Detail Category Classification, Group 1 Non-welded Details
(Clauses 13.2.2.1 and 13.3)
SI Detail Constructional Details
No. Category
Illustration (see Note) Description
(1) (~)
(3) (4)
Rolled and extruded products
-’ 1!, ::::::::%)
(1)
a
iii) Seamless tubes (3)
i)
“8 % Q ‘2) ‘tress
Sharp edges, surface and rolling flaws to be
removed by grinding in the direction of applied
(3)
‘4)4X ‘“’te:=: one-sided cover ‘ate
(4) and (5): Stress range calculated On the
gross section and on the net section
s
connections shall be avoided or the effect of
the eccentricity taken into account in
. .
. . calculating stresses
. .
. >. Material with gas-cut or sheared edges with no
. .
ii) I03 . . draglines
(5)
. .
(6): All hardened material and visible signs
of edge discontinuities to be removed by
machining or grinding in the direction of
applied stress.
(-
Material with machine gas-cut edges with
=
draglines or manual gas-cut material
iii) 92 (7) : Corners and visible signs of edge
discontinuities to be removed by grinding in the
direction of the applied stress.
NOTE— The arrow indicates the location and direction of the stresses acting in the basic material for whichthe stressrange is to be
calculatedon a plane normalto the arrow.
93

IS 800:2007
Table 26 (b) Detail Category Classification, Group 2 Welded, Details — Not in Hollow Sections
(Clauses 13.2.2.1 and 13.3)
{0. Category
Illustration(seeNote) Description
,1) (2) (3) (4)
Welded plate I-section and box girders with
~ QA (8)&(9) :mnmof~ntinuousautomatic
continuous longitudinal welds
longitudinal fillet or butt welds carried out from both
92 (8) sides and all welds not having un-repaired stop-start
i)
Q
positions.
,,, * a’k stoP-s@positions
(10) & (11) : Zones of continuous automatic butt
welds made tlcsm one side only with a continuous
backing bar and all welds not having un-repaired
(lo) (11) (12): Zones of continuous longitudinal fillet or butt
m
welds carried out fkom both sides but containing
stop-start positions. For continuous manual
longitudinal tilIet or butt welds carried out from both
(12) sides, use Detail Category 92.
Q
“.
iii) 66
(13) :Zones of continuous longitudinal welds carried
out ffom one side only, with or without stop-start
(13) positions.
Q
Intermittent longitudinal welds
“.
(14) : Zones of intermittent longitudinal welds
iv) 59 r
(14)
Q
intermittent longitudinal welds
v) (15) : Zones containing cope holes in longitudinally
52 welded T-joints. Cope hole not to be tilled with
weld.
(15)
Transverse butt welds (complete penetration)
a
Weldrun-offtabs to be used, subsequently removed
and ends of welds ground flush in the direction of
stress. Welds to be made from two sides.
—-
(16) : Transverse splices in plates, flats and rolled
vi)
sections having the weld reinforcement ground flush
83 (17)
to p}ate surface. 100 percent NDT inspection, and
(18) weld surface to be ffee of exposed porosity in the
weld metal.
=-
(17) : Plate girders welded as in (16) before
assembly.
(la) (18) : Transverse splices as in (16) with reduced or
tapered transition with taper S1:4
94

..______ ~
IS 800:2007
Table 26 (b) (Continued)
51 Detail Constructional Detaits
io. Category
1) (2) (3) (4)
~
Welds inn-off tabs to be used, subsequently removed
stress. Welds to be made from two sides.
(19)
(19) : Transversesplicesof plates,rolled sections or
66 (20)
iii)
plate girders.
-’k
(20) : Transverse splice of rolled sections or welded
plate girders, without cope hole. With cope hole use
Detail Category 52, asin(15).
(21): Transversesplices in plates m flats bekrgtapcmd
(21)
inwidthor in tldcknesswherethe taperiss 1:4.
.-
Weld run-off tabs to be used, subsequently removed
59
/iii) stress. Welds to be made from two sides.
(22) (22) : Transverse splices as in (21) with taper in
width or thickness >1:4 but <1:2.5.
I-
(23) : Transverse butt-welded splices made on a
backing bar. The end of the fillet weld of the backing
strip shall stop short by more than 10 mm from the
ix) 52 ~ ~fim e~l :::::’:
(24): Transversebutt welds as per (23) with taper on
x)
~4=’Omm
(25) : Transverse butt welds as in (23) where fillet
welds end closer than 10 mm to plate edge.
37
(25)
Cruciform joints with load-carrying welds
52 +
(26) : Full penetration welds with intermediate plate
NDT inspected and free of defects. Maximum
xi) misalignment of plates either side of joint to be
<0.15 times the thickness of intermediate plate.
(26)
‘: : :*
(27) : Partial penetration or fillet welds with stress
range calculated on plate area.
(28) : Partial penetration or fillet welds with stres:
xii) range calculated on throat area of weld.
(27)6 (28)
--”’
Overlapped welded joints
(29) : Fillet welded lap joint, with welds arrc
~iii) 46
overlapping elements having a design capacit)
greater than the main plate. Stress in the main platt
to be calculated on the basis of area shown in th{
(29) illustration.
95

1S 800:2007
Table 26 (b) (Concluded)
No. Category
(1) (2) (3) (4)
Overlapped weld joints
xiv) b
41 (30)
‘w
T
(30) : Fillet welded lap joint, with welds and main
plate both having a design capacity greater than the
>lOmm

overlapping elements.
(31) : Fillet welded lap joint, with main plate and
xv) 33 (31) (30)a (31) overlappingelementsboth having a design capacity
greater than the weld.
66
(32) (33) h,
Q
Welded attachments (non-load carrying welds) —
— 1/3 < r/b ‘7 Longitudina[welds
59 ls50mm —
52 50</ <100 mm l16<r/b<l13 (32) : Longitudinal fillet welds. Class of detail varies
according to the length of the attachment weld as
37 100 mm <1
(32) noted.
—
x~i) (33) : Gussetwelded to the edge of a plate or beam
‘*
flange. Smooth transition radios (r), formed by
machining or flame cutting plus grinding. Class of
33 — r/b<l/6 detail varies according to r)bratio as noted.
M
(33)
m
Welded attachments
xvii) 59 (34) : Shear connectors on base material (failure in
base material).
(34)
—
Transverse welds
59
t<12mm (35) : Transverse fillet welds with the end of the
weld 210 mm from the edge of the plate.
(36) : Vertical stiffeners welded to a beam or plate
(35) girder flange or web by continuous or intermittent
welds. to the case of webs carrying combined
bending and shear design actions, the fatigue
xviii) strength shall be determined using the stress range of
the principal stresses.
52 t~12mm ZI
omm (37) : Diaphragms of box girders welded to the
flange or web by continuous or intermittent welds.
(36)
w
~.=.
;!. j:
(37)
37
rfor tp
a
‘p Cover plates in beams and plate girders
<25 mm
1, (38) : End zonesof singleor multiplewelded cover
xix)
27
ffm tP plates, with or without a weld across the end. For a
>25 mm reinforcing plate wider than the flange, an end weld
(38) is essential.
67 ~i
Welds loaded in shear
(39) : Filletweldstransmittingshear.Stressrangeto
xx) be calculated on weld throat area.
(40) : Stud welded shear connectors (failure in the
(40) (39)
weld) loaded in shear (the shear stress range to be
calculated on the nominal section of the stud).
NOTE — The arrow indicates the location and direction of the stresses acting in the basic material for which the stress range is to be
calculated on a plane normal to the arrow.
96

...-.
______ —-,.
IS 800:2007
Table 26 (c) Detail Category Classification, Group 3 Bolts
(Clauses 13.2.2.1 and 13.3)
sl Constructional Details
No.
Detail Category
Illustration [see Note ) Description
(1) (2) (3) (4)
Bolts in shear (8.8fTBbolting category only)
=u-
(41) : Shear stress range calculated on the
minordiameterareaofthe bolt(J,).
NOTE — If the shear on the joint is
i) 83 insufficientto cause slip of the joint the
shear in the bolt need not reconsidered in
fatigue.
(41)
Bolts and threaded rods in tension (tensile
+ t
stress to be calculated on the tensile stress
area, A,)
Uo
(42) : Additional forces dueto prying effects
shall be taken into account. Fortensionalbolts,
the stress range depends on the connection
geometry.
ii) 27 NOTE — In connectionswith tensioned
bolts,the changein the force in the bolts is
often less than the applied force, but this
effect is dependent on thegeometty of the
i i
connection. It isnotnormally required that
any allowance for fatigue be made in
(42)
calculating the required number of bolts in
such connections.
NOTE— The arrow indicates the location and direction of the stresses acting in the basic material for which the stress mnge is to be
calculated on a plane normal to the arrow.
1000
Stressrangecorresponding
..-
to 2X106cycles
II
20 - at5x106 eyeles
[Detailcategory( fm)]
1
0 105 2
1
34561062
t I 1 I 1
34561072 3456108
NUMBEROF STRESSCYCLES (fJsc)
FIG. 22 S-N CURVE FOR NORMAL STRESS
97

Table 26 (d) Detail Category Classification, Group 4
Welded Details in Hollow Sections
(Clause 13.2.2.1 and 13.3)
sl Detail Category Constructional Details
No.
(1) (2) (3) (4)
103 Continuous automatic longitudinal welds
Q% ‘etachab’ediscontinuities”
(43) : No stop-starts, or as manufactured, proven free to
i)
(43)
66 Transverse butt welds
(t> 8 mm)
ae
(44) : Butt-welded end-to-end connection of circular
52 hollow sections.
ii) (r< 8 mm) NOTE — Height of the weld reinforcementless
(44) than 10percent of weld with smoothtransitionto
the plate surface. Welds made in flat position and
proven free to detachable discontinuities.
52
B
t
(45) :Butt-welded end-to-end connection Ofrectangular
(t> 8 mm) hollow sections
iii)
41
(f< 8 mm) (45)
41 Butt welds to intermediate plate
(t28 mm)
!3:D ~
(46) : Circular hollow sections, end-to-end butt-welded
iv) with an intermediate plate.
(t< Vmm)
(46)
37
=~
(47) Rectangular hollow sections, end-to-end butt
(t> 8 mm) welded with art intermediate plate
v)
30
(t< 8 mm)
(47)
52 %77 s~essdrection~,oomrn
Weldedattachments (non-load-carrying)
(48) : Circular or rectangular hollow section, fillet
welded to another section, Section width parallel to
vi)
J ~EcTlc)NwcmH
<1OOmm
(48)
33
rzj Q
Fillet welds to intermediate plate
(t< 8 mm) (49) : Circularhollowsections,end-to-endfilletwelded
vii) withan intermediateplate.
(t< ?mm) (49)
29
Ixj Q
(50) : Rectangular hollow sections, end-to-end fillet
(/> 8 mm) welded with an intermediate plate.
viii) 27
(t< 8 mm)
(50)
NOTE — The arrow indicates tbe location and direction of the stresses acting in the basic material for which the stress range is to be
calculated on a plane normal tOthe arrow.
98

-_
13.5 Fatigue Assessment
The design fatigue strength for Nsc life cycles ~fd! ‘fd)
may be obtained from the standard fatigue strength
for Nsc cycles by multiplying with comection factor,
p,, for thickness, as mentioned in 13.2.1 and dividing
by partial safety factor given in Table 25.
13.5.1 Exemptions
At any point in a structure if the actual normal and
shear stress range~and ~ are less than the design fatigue
strength range corresponding to 5 x 106 cycles with
appropriate partial safety factor, no further assessment
for fatigue is necessary at that point.
13.5.2 Stress Limitations
13.5.2.1 The maximum (absolute) value of the normal
and shear stresses shall never exceed the elastic limit
(f,, ~,) for the material under cyclic loading.
13.5.2.2 The maximum stress range shall not exceed
1.5$ for normal stresses and 1.5 f,ifi for the shear
stresses under any circumstance.
IS 800:2007
13.5.2.3 Constant stress range
The actual normal and shear stress range f and z at a
point of the structure subjected to NsC cycles in life
shall satisfy.
f ‘ffd = P,.f#%ft
~ S ‘fd = #r ‘f IYmft
where
v, = correction factor (see 13.2.1),
71nf = partial safety factor against fatigue failure,
given in Table 25, and
fi, Tf = normal and shear fatigue strength ranges for
the actual life cycle, Nsc, obtained from 13.4.
13.5.2.4 Variable stress range
Fatigue assessment at any point in a structure, wherein
variable stress ranges jfi or 7$ for ni number of cycles
(i =1 to r ) are encountered, shall satisfy the following:
a) For normal stress (f)
0
IJJ
1-
Q
!JJ
cc 40 ~~Detail cateaotv TI --H_Hk
1 I I I I I I I I II I I I I I I I II I I I I I
I 1
[ I I
I
o 105 2 34561062 34561072 3456108
NUMBER OF STRESS CYCLES (f’f~c)
FIG. 23 S-N CURVE FOR SHEAR STRESS
99

IS 800:2007
b) For shear stresses (t)
,=1
where yf is the summation upper limit of all the
normal stress ranges (J) having magnitude lesser
than (pC~~n/~~~t)
for that detail and the lower limit of
all the normal stress ranges ~j) having magnitude
greater than (PC~#y~J for the detail. In the above
summation all normal stress ranges, f,, and Zihaving
magnitude less than 0.55pC ~fn, and 0.55pC qn may
be disregarded,
13.6 Necessity for Fatigue Assessment
a) Fatigue assessment is not normally required
for building structures except as follows:
1)
2)
3)
4)
b) No
the
1)
2)
3)
Members supporting lifting or rolling
loads,
Member subjected to repeated stress
cycles from vibrating machinery,
Members subjected to wind induced
oscillations of a large number of cycles
in life, and
Members subjected to crowd induced
oscillations of a large number of cycles
in life.
fatigue assessment is necessary if any of
following conditions is satisfied.
The highest normal stress range ~~,~,,
satisfies
L, M.,~ 27PcJYmft
The highest shear stress range ‘r~,~,,
satisfies
‘r < 67/-4/ymft
f,Max
-
The total number of actual stress cycles
NSC,satisfies
[1
3
27pC
N,c S5x10’ —
Ymftffq
where
J%, = equivalent constant amplitude
stress range in MPa given by
I
1/3
~ n,f,’ + ~ njffi’
&q = ‘=’ n’=”
where
‘=~n “
I-I
ffi>fg = stress ranges falling above and
below the f~n, the stress range
corresponding to the detail at
5 x 106 number of life cycles.
SECTlON 14
DESIGN ASSISTED BY TESTING
14.1 Need for Testing
Testing of structures, members or components of
structures is not required when designed in accordance
with this standard. Testing may be accepted as an
alternative to calculations or may become necessary
in special circumstances.
Testing of a structural system, member or component
may be required to assist the design in the following
cases:
a)
b)
c)
d)
e)
When the calculation methods available are not
adequate for the design of a particular structure,
member or component, testing shall be
undertaken in place of design by calculation
or to supplement the design by calculation;
Where rulesor methods for design by
calculation would lead to uneconomical
design, experimental verification may be
undertaken to avoid conservative design;
When the design or construction is not entirely
in accordance with sections of this standard,
experimental verification is recommended;
When confirmation is required on the
consistency of production of material,
components, members or structures originally
designed by calculations or testing; and
When the actual performance of an existing
structure capacity is in question, testing shall
be used to confirm it.
14.1.1 Testing of structural system, member or
component shall be of the following categories:
a) Proof testing — The application of test loads
to a structure, sub-structure, member or
connection to ascertain the structural
characteristics of only that specific unit.
100

. ~~
-------
--—-—— —---%..
b) Prototype testing — Testing of structures, sub-
structures, members or connections is done
to ascertain the structural characteristics of a
class of such structures, sub-structures
members or connection, which are nominally
identical to the units tested.
14.2 Types of Test
14.2.1 Acceptance Test
This is intended as a non-destructive test for confirming
structural performance. It should be recognized that
the loading applied to certain structures might cause
permanent distortions. Such effects do not necessarily
indicate structural failure in acceptance test. However,
the possibility of their occurrence should be agreed to
before testing.
The load for acceptance test, Ftcfi[,.shall be determined
from:
Ft.,,,, = (1.0x self weight)+ (1.15 x remainder
of the permanent load)+ ( 1.25 x variable
load).
The assembly shall satisfy the following criteria:
a) It shall demonstrate substantially linear
behaviour under test loading, and
b) On removal of the test load, the residual
deflection shall not exceed 20 percent of the
maximum-recorded deflection.
If the above criteria are not satisfied the test may be
repeated one more time only, when the assembly shall
satisfy the following criteria:
a)
b)
It shall demonstrate substantially linear
behaviour on the second application of test
loading, and
Corresponding recorded residual deflection
in the second test shall not exceed 10 percent
of the maximum deflection during the test.
14.2.2 Strength Test
Strength test is used to confirm the calculated resistance
of a structure or component. Where a number of items
are to be constructed to a common design, and one or
more prototypes are tested to confirm their strength,
the others may be accepted without any additional test,
provided they are similar in all relevant respects to the
prototype.
Before carrying out the strength test, the specimen
should first be subjected to and satisfy the acceptance
test. Since the resistance of the assembly under test
depends on the material properties, the actual yield
strength of all the steel materials in the assembly shall
be determined from coupon (test piece as defined in
IS 800:2007
IS 1608) tests . The mean value of the yield strength,
~Y~,
taken from such tests shall be determined with due
regard to the importance of each element in the
assembly. The strength test load F~e,~,,(including self
weight) shall be determined from:
Ftest,s = ~mi Fd ~YmyY)
where
~Y = characteristic yield stress of the material as
assumed in the design,
Fd = factored design load for the ultimate limit
state, and
%i = partial safety factor for the type of failure,
as prescribed in this standard.
At this load there shall be no failure by buckling or
rupture of any part of the structure or component tested.
On removal of the test load, the deflection should
decrease by at least 20 percent of the maximum
deflection at F1.,t,,.
14.2.3 Test to Failure (Ultimate Strength Test)
The objective of a test to failure is to determine the
design resistance from the ultimate resistance. In this
situation it is still desirable to carry out the acceptance
and strength tests, before test to failure.
Not less than three tests shall be carried out on
nominally identical specimens. An estimate should be
made of the anticipated ultimate resistance as a basis
for such tests. During a test to failure, the loading shall
first be applied in increments up to the strength test
load. Subsequent load increments shall then be
determined from consideration of the principal load
deflection plot. The test load resistance, Ft.,,.R shall be
determined as that load at which the specimen is unable
to sustain any further increase in load. At this load,
gross permanent distortion is likely to have occurred
and in some cases such large gross deformation may
define the test limit. If the deviation of any individual
test result exceeds 10 percent of the mean value
obtained for all the three tests, at least three more tests
shall be carried out. When the deviation from the mean
does not exceed 10 percent of the mean, the design
resistance may be evaluated as given below:
a) When the failure is ductile, the design
resistance, F~ may be determined from:
Fd = 0.9F,,,,,~in( fY~Y~) /Y~O
where
F,~,,,~in =
f,. =
minimum test result from the tests
to failure,
average yield strength as obtained
from the material tests, and
101

IS 800:2007
~= characteristic yield stress of the
grade of steel.
b) In the case of a sudden (brittle) rupture type
failure, the design resistance may be
determined from:
F~ = 0.9F’,~~,,
~in(~U/j&) / &
where
f“ = characteristic ultimate stress of the
grade of steel used, and
f urn = average ultimate tensile strength of
the material obtained from tests.
c) In the case of a sudden (brittle) buckling type
failure, the design resistance shall be
determined from:
F~ = 0,75Fki, Min(~~!~~)/~mO
d) In ductile buckling type failure in which the
relevant slenderness k can be reliably assessed,
the design resistance may be determined from:
.3(,M”[(tiy %fym)%l
F. = 0.9F
where
x =
x. =
reduction factor for the relevant
buckling curve, and
value of x when the yield strength
isfy”.
14.2.4 Check Tests
Where a component or assembly is designed on the
basis of strength tests or tests to failure and a production
run is carried out of such items, an appropriate number
of samples (not less than two) shall be selected from
each production batch at random for check tests.
14.2.4.1 The samples shall be carefully examined to
ensure that they are similar in all respects to the
prototype tested, particular attention being given to the
following:
a) Dimensions of components and connections;
b) Tolerance and workmanship; and
c) Quality of steel used, checked with reference
to mill test certificates.
14.2.4.2 Where it is not possible to determine either
the variations or the effect of variations from the
prototype, an acceptance test shall be carried out as a
check test.
14.2.4.3 In this check test, the deflections shall be
measured at the same positions as in the acceptance
test of the prototype. The maximum measured
deflection shall not exceed 120 percent of the deflection
recorded during the acceptance test on the prototype
and the residual deflection should not be more than
105 percent of that recorded for the prototype.
14.3 Test Conditions
a)
b)
c)
d)
e)
f)
Loading and measuring devices shall be
calibrated in advance.
The design of the test rig shall be such that:
1)
2)
3)
4)
5)
6)
Loading system adequately simulates the
magnitude and distribution of the
loadlng;
It allows the specimen to perform in a
manner representative of service
conditions;
Lateral and torsional restraint, if any,
should be representative of those in service,
Specimen should be free to deflect under
load according to service condition;
Loading system shall be able to follow
the movements of the specimen without
interruption or abnormal restraints; and
Inadvertent eccentricities at the point of
application of the test loads and at the
supports are avoided,
Test load shall be applied to the unit at a rate
as uniform as practicable.
Deflections should be measured at sufficient
points of high movements to ensure that the
maximum value is determined.
If the magnitude of stresses in a specimen is
to be determined, the strain at the desired
location may be measured and the
corresponding stress calculated.
Prior to any test, preliminary loading (not
exceeding the characteristic values of the
relevant loads) may be applied and then
removed, in order to set the test specimen on
to the test rig.
14.4 Test Loading
14.4.1 Where the self-weight of the specimen is not
representative of the actual permanent load in service,
allowance for the difference shall be made in the
calculation of test loads to be applied.
14.4.2 On the attainment of maximum load for either
acceptance or strength tests, this load shall be
maintained for at least 1 h. Reading of load and
deflection shall be taken at intervals of 15 min and the
loading shall be maintained constant until there is no
significant increase in deflection during a 15 min period
or until at least 1 h has elapsed.
14.4.3 The test load shall be equal to the design load
for the relevant limit state in proof testing.
102

. _ —----%..
14.4.4 The test load in prototype testing shall be equal
to the design load for the relevant limit state as
multiplied by the appropriate factor given in Table 27.
Table 27 Factors to Allow for Variability of
Structural Units
SI No. of Similar For Strength For
No. Units to be Tested Limit State Serviceability
Limit State
(1) (2) (3) (4)
i) 1 1.5 1.2
ii) 2 1.4 1.2
iii) 3 1.3 1.2
iv) 4 1.3 1.1
v) 5 1.3 I.1
vi) 10 I .2 1.1
14.5 Criteria for Acceptance
14.5.1 Acceptance for Strength
The test structure, sub-structure, member or connection
shall be deemed to comply with the requirements for
strength if it is able to sustain the strength test load for
at least 15 min.
It shall then be inspected to determine the nature and
extent of any damage incurred during the tes~ The
effects of the damage shall be considered and if
necessary appropriate repairs to the damaged parts
carried out.
14.5.2 Acceptance for Serviceability
The maximum deformation of the structure or member
under the serviceability limit state test load shall be
within the serviceability limit values appropriate to the
structure.
15.1 General
A durable steel
satisfactorily the
SECTION 15
DURABILITY
structure is one that performs
desired function in the working
environment under the anticipated exposure condition
during its service life, without deterioration of the cross-
sectional area and loss of strength due to corrosion. The
material used, the detailing, fabrication, erection and
surface protection measures should all address the
corrosion protection and durability requirements.
15.2 Requirements for Durability
15.2.1 Shape, Size, Orientation of Members,
Connections and Details
The design, fabrication and erection details of exposed
IS 800:2007
structures should be such that good drainage of water
is ensured. Standing pool of water, moisture
accumulation and rundown of water for extended
duration shall be avoided.
The details of connections should ensure that:
a) AII exposed surfaces are easily accessible for
inspection and maintenance; and
b) All surfaces, not so easily accessible are
completely sealed against ingress of moisture.
15.2.2 Exposure Condition
15.2.2.1 General environment
The general environment, to which a steel structure is
exposed during its working life is classified into five
levels of severity, as given in Table 28.
Table 28 Environmental Exposure Conditions
S1 Environmental
No. Classifications
Exposure Conditions
(1) (2) (3)
i) Mild
ii) Moderate
iii) Severe
iv) Very severe
v) Extreme
Surfaces normally protected against
exposure to weather or aggressive
condition as in interior of buildings,
except when located in coastal areas
Structural steel surfaces:
a) exposed to condensation and rain
b) continuously under water
c) exposed to non-aggressive soiti
groundwater
d) sheltered from saturated salt air in
coastal areas
Structural steel surfaces:
a) exposed to severe frequent rain
b) exposed to alternate wetting and
drying
c) severe condensation
d) completely immersed in sea water
e) exposed to saturated salt air in
coastal area
Structural steel surface exposed to:
a) sea water spray
b) corrosive fumes
c) aggressivesub soil or ground water
Structural steel surfaces exposed to:
O tidal zones and splash zones in the
sea
b) aggressive liquid or solid chemicals
15.2.2.2 Abrasion
Specialist literature may be referred for durability of
surfaces exposed to abrasive action as in machinery,
conveyor belt support system, storage bins for grains
or aggregates.
103

IS 800:2007
15.2.2.3 Exposure to sulphate attack
Appropriate coatings may be used when surfaces of
structural steel are exposed to concentration of
sulphates (SOJ) in soil, ground water, etc.
When exposed to very high sulphate concentrations
of more than 2 percent in soil and 5 percent in water,
some form of lining such as polyethylene,
polychloroprene sheet or surface coating based on
asphalt, chlorinated rubber, epoxy or polymethane
material should be used to completely avoid access of
the solution to the steel surface.
15.2.3 Corrosion Protection Methods
The methods of corrosion protection are governed by
actual environmental conditions as specified in IS 9077
and IS 9172. The main corrosion protection methods
are given below:
a) Controlling the electrode potential,
b) Inhibitors, and
c) Inorganic/metal coatings or organic/paint
systems.
15.2.4 Su~ace Protection
15.2.4.1 In the case of mild exposure, a coat of primer
after removal of any loose mill scale may be adequate.
As the exposure condition becomes more critical, more
elaborate surface preparations and coatings become
necessary. In case of extreme environmental
classification, protection shall be as per specialist
literature. Table 29 gives guidance to protection of
steelwork for different desired lives.
Table 29 (a) Protection Guide for Steel Work Application — Desired Life of Coating
System in Different Environments
SI Atmospheric Condition/ Coating System
No. Environmental Classification
/ Y
1 2 3 4 5 6
(1) (2) (3) (4) (5) (6) (7) (8)
i) Normalinland(ruraland urban
areas),mild
ii) Pollutedinland(high airborne
sulphur dioxide), moderate
iii) Normal coastal (as normal inland
plus high airborne salt levels), severe
iv) Polluted coastal (as polluted inland
plus high airborne salt levels), very
severe or extreme
12years 18years 20 years About
20 years
10years 15years 12years About
18years
10years 12years 20 years About
20 years
8 years 10years 10years About
15 years
About Above
20 years 20 years
15-20years Above
20 years
About Above
20 years 20 years
15-20 years Above
20 years
Table 29 (b) (i) Protection Guide for Steel Work Application — Specification for Different Coating
System (Shop Applied Treatments)
(Clause 15.2.4. 1)
SI Protection Coating System
No.
c
1 2 3 4 5 6
(1) (2) (3) (4) (5) (6) (7) (8)
i) Surface preparation Blast clean
ii) Pre-fabrication Zinc phosphate
primer epoxy, 20 w
iii) Post-fabrication High-build zinc
primer phosphate
modified alkyd,
60pm
iv) Intermediate coat —
Blast clean Blast clean
2 pack zinc-rich
epoxy, 20 pm
2 pack zinc-rich Hot dip
epoxy, 20 pm galvanized,
85pm
High-buildzinc —
phosphate, 25 pm
Blast clean Gkt blast
2 pack zinc-rich —
epoxy, 20p
2 pack zinc-rich Sprayed zinc or
epoxy, 25 pm sprayed
aluminium
2 pack epoxy Sealer
micaceous iron
oxide
2 pack epoxy Sealer
micaceous iron
oxide, 85 Urn
Blast clean
Ethyl zinc
silicate, 20 Urn
Ethyl zinc
silicate, 60 pm
Chlorinated
rubber alkyd,
35pm
v) Top coat — — . —
104

IS 800:2007
Table 29 (b) (ii) Protection Guide for Steel Work Application — Specification for Different Coating
System (Site Applied Treatments)
(Clause 15.2.4.1)
sl Protection Coating System
No.
/ -
1 2 3 4 5 6
(1) (2) (3) (4) (5) (6) (7) (8)
O Surface
preparation
ii) Primer
iii) Intermediate
coat
iv) TOPcoat
As necessary As necessary
Touchin Touchin
Modified
Alkyd
Micaceous
ironoxide,
50 ~m
High-build Modified
Alkyd finish, Alkyd
60~m Micaceous
iron oxide,
50 pm
No site Asnecessary No site As necessary
treatment treatment
— — — Touchin
— Touchtn — High-build
micaceousiron
oxide
Chlorinated
rubber
Micaceous,
— High-build
chlorinated
75 pm
— H@t-build iron
oxide Chlorinated
rubber rubber, 75 ~m
15.2.4.2 Steel surfaces shall be provided with at least
one coat of primer immediately after its surface
preparation such as by sand blasting to remove all mill
scale and rust and to expose the steel.
15.2.4.3 Steel without protective coating shall not be
stored for long duration in out door environment.
15.2.4.4 Surfaces to transfer forces by friction as in
HSFG connections shall not be painted. However it
shall be ensured that moisture is not trapped on such
surfaces after pretensioning of bolts by proper
protective measures.
15.2.4.5 Members to be assembled by welding shall
not be pre-painted at regions adjacent to the location
of such welds. However, after welding, appropriate
protective coatings shall be applied in the region, as
required by the exposure conditions. If the contact
surfaces cannot be properly protected against ingress
of moisture by surface coating, they maybe completely
sealed by appropriate welds.
15.2.4.6 Pre-painted members shall be protected
against abrasion of the coating during transportation,
handling and erection.
15.2.5 Special Steels
Steels with special alloying elements and production
process to obtain better corrosion resistance may be
used as per specialist literature.
SECTION 16
FIRE RESISTANCE
16.1 Requirements
The requirements shall apply to steel building elements
designed to exhibit a required fire-resistance level
(FRL) as per the relevant specifications.
16.1.1 For protected steel members and connections,
the thickness of protection material (hi) shall be greater
than or equal to that required to give a period of
structural adequacy (PSA) greater than or equal to the
required FRL.
16.1.2 For unprotected steel members and connections,
the exposed surface area to mass ratio (k,~) shall be
less than or equal to that required to give a PSA equal
to the required FRL.
16.2 Fire Resistance Level
The required FRL shall be as prescribed in IS 1641,
IS 1642 and IS 1643, as appropriate or in building
specifications or as required by the user or the city
ordinance. The FRL specified in terms of the duration
(in minutes) of standard fire load without collapse
depends upon:
a) the purpose for which structure is used, and
b) the time taken to evacuate in case of fire.
105

IS 800:2007
16.3 Period of Structural Adequacy (PSA)
16.3.1 The calculation of PSA involves:
a)
b)
c)
Calculation of the strength of the element as
a function of temperature of the element and
the determination of limiting temperature;
Calculation of the thermal response of the
element, that is calculation of the variation of
the temperature of the element or the parts of
the element with time, when exposed to fire;
and
Determination of PSA at which the
1.2
CURVE 1: YEILDSTRESS RATIO
1.0 CURVE 2: MODULUSOF
ELASTICITYRATIO
0.8
I
I
0.6
I
0.4 L
I
0.2
I ‘-
I
0 ’215 I T
0 200 400 600 800 1000 1200
temperature of the element or parts of the
element reaches the limiting temperature.
16.3.2 Determination of Period of Structural Adequacy
The period of structural adequacy (PSA) shall be
determined using one of the following methods:
a)
b)
c)
By calculation:
1)
2)
determining the limiting temperature of
the steel (T,) in accordance with 16.5 ;
and
determining the PSA as the time (in rein)
from the start of the test to the time at
which the limiting steel temperature (t)
is attained, in accordance with 16.6 for
protected members and 16.7 for
unprotected members.
By direct application of a single test in
accordance with 16.8; or
By calculation of the temperature of the steel
member by using a rational method of
analysis confirmed by test data or by methods
available in specialist literature.
16.4 Variation of Mechanical Properties of Steel
with Temperature
16.4.1 Variation of Yield Stress with Temperature
The influence of temperature on the yield stress of steel
shall be taken as follows for structures of mild steels
and high strength low alloy steels:
fy(T) 905-T <10
—= —
f, (20) 905 – -
where
fy(T) = yield stress of steel at T°C,
fy(20) = yield stress of steel at 20°C (room
temperature), and
T = temperature of the steel in “C.
This relationship is shown by Curve 1 in Fig. 24.
STEELTEMPERATURE(T) “C
FIG. 24 VARIATION
OFMECHANICAL
PROPERTIES
OF
STEELWITH
TEMPERATURE
For temperature less than 215°C no reduction in the
yield stress need to be considered.
16.4.2 Variation of Modulus of Elasticity with
Temperature
The influence of temperature on the modulus of
elasticity shall be taken as follows for structures of mild
steels and high strength low alloy steels:
E(T)
— = 1.0+
I
T
E(20)
[ ( )1.
T
20001n —
1100
when O“C < T S 600”C
()
690 l-~
1000
=
T-53.5
when 600”C < T S 1 OOO”C
E (7) = modulus of elasticity of steel at T “C,
and
E (20) = modulus of elasticity of steel at 2(YC
(room temperature).
This relationship is shown by curve 2 in Fig. 24.
16.4.3 For special steel with higher temperature
resistance, such as TMCP steels, the manufacturer’s
recommendation shall be used to obtain the variation
of yield strength and modulus of elasticity of steel with
temperature.
16.5 Limiting Steel Temperature
The limiting steel temperature (Tl) in degree Celsius
in the case of ordinary steels, shall be calculated as
follows:
106

.,.,.,..,.,,, ———
T]= 905-690 r~
where
r~ = ratio of the design action on the member
under tire to the design capacity of the
member (R~ = Ru/y~) at room
temperature,
R~,I?u = design strength and ultimate strength of
the member at room temperature
respectively, and
l% = ptiial safety factor for strength.
The design action under fire shall consider
following:
a) Reduced bond likely under tire, and
b) Effects of restraint to expansion of
elements during fire.
the
the
Limiting steel temperature for special steels may be
appropriately calculated using the thermal
characteristics of the material obtained from the
supplier of the steel.
16.6 Temperature Increase with Time in Protected
Members
16.6.1 The time (t) at which the limiting temperature
(Ti) is attained shall be determined by calculation on
the basis of a suitable series of fire tests in accordance
with 16.6.2 or from the results of a single test in
accordance with 16.6.3.
16.6.1.1 For beams and for all members with a four-
sided fire exposure condition, the limiting temperature
(Tl) shall be taken as the average of all of the
temperatures measured at the thermocouple locations
on all sides.
16.6.1.2 For columns with a three-sided fire exposure
condition, the limiting temperature (7’1)shall be taken
as the average of the temperatures measured at the
thermocouple locations on the face farthest from the
wall. Alternatively, the temperatures from members
with a four-sided fire exposure condition and having
the same surface area to mass ratio may be used.
16.6.2 Temperature Based on Test Series
Calculation of the variation of steel temperature with
time shall be by interpolation of the results of a series
of fire tests using the regression analysis equation
specified in 16.6.2.1, subject to the limitations and
conditions of 16.6.2.3.
16.6.2.1 Regression analysis
The relationship between temperature (T) and time (t)
for a series of tests on a group shall be calculated by
least-square regression as follows:
IS 800:2007
t=kO+klhi +k2; +k~T+kahiT+k#+kb~
sm sm sm
where
t = time from the start of the test, in rein;
kOto k~ = regression coefficients from test data
(see 16.6.2.2.);
hi = thickness of fire protection material,
in mm;
T = steel temperature, in degrees celsius
obtained from test as given
in 16.6.1, T > 250” C; and
k,~ = exposed surface area to mass ratio, in
103mm2/kg.
16.6.2.2 In lieu of test results, the values for coefficients
in Table 30 may be used in the equation 16.6.2.1 when
the test satisfies the conditions specified in 16.6.2.3.
Table 30 Regression Coefficients, k
kO k, kz k3 k4 k5 k6
(1) (2) (3) (4) (5) (6) (7)
-25.90 1.698 -13.71 0.0300 0.0005 0.5144 6.633
16.6.2.3 Limitations and conditions on use of
regression analysis
Test data to be utilized in accordance with 16.6.2.1,
shall satisfy the following:
a)
b)
c)
d)
e)
f)
Steel members shall be protected with board,
sprayed blanket or similar insulation materials
having a dry density less than 1000 kg/m3;
All tests shall incorporate the same fire
protection system;
All members shall have the same fire exposure
condition;
Test series shall include at least nine tests;
Test series may include prototypes which have
not been loaded provided that stackability has
been demonstrated; and
All members subject to a three-sided fire
exposure condition shall be within a group in
accordance with 16.9.
The regression equation obtained for one tire protection
system may be applied to another system using the
same fire protection material and the same fire exposure
condition provided that stackability has been
demonstrated for the second system.
A regression equation obtained using prototypes with
a four-sided fire exposure condition maybe applied to
a member with a three-sided fire exposure condition
provided that stackability has been demonstrated for
the three-sided case.
107

1S 800:2007
16.6.3 Temperature Based on Single Test
The variation of steel temperature with time measured
in a standard fire test maybe used without modification
provided:
a)
b)
c)
d)
e)
Fire protection system is the same as the
prototype;
Fire exposure condition is the same as the
prototype;
Fire protection material thickness is equal to
or greater than that of the prototype;
Surface area to mass ratio is equal to or less
than that of the prototype; and
Where the prototype has been submitted to a
standard fire test in an unloaded condition,
stackability has been separately demonstrated.
16.6.4 Parameters of Importance in the Standard Fire
Test
a)
b)
c)
d)
Specimen type, loading, configuration;
Exposed surface area to mass ratio;
Insulation type, thermal properties and
thickness; and
Moisture content of the insulation material.
16.7 Temperature Increase with Time in
Unprotected Members
The time (t)
at which the limiting temperature (Tl) is
attained shall be calculated using the following
equations:
a) Three-sided fire exposure condition
o.433q
t=5.2+0.022 1 T+ -
ksm
b) Four-sided fire exposure condition
t = 4.7
where
t =
T=
k,~ =
+0.0263T+ 3
ksm
time from the start of the test, in rein,
steel temperature, in “C, 500 “C
s T ~ 75t)°C, and
exposed surface area to mass
ratio, 2x103 mm2/kg S k,m S 35
x103 mm2/kg.
For temperatures below 500°C, linear interpolation
shall be used, based on the time at 500”C and an initial
temperature of 20”C at tequals O.
16.8 Determination of PSA from a Single Test
The period of structural adequacy (PSA) determined
from a single test maybe applied without modification
provided:
a) Conditions, specified in 16.6.3 are satisfied,
b) Conditions of support are the same as the
prototype and the restraints are not less
favorable than those of the prototype, and
c) Ratio of the design load for fire to the design
capacity of the member is less than or equal
to that of the prototype.
16.9 Three-Sided Fire Exposure Condition
Members subject to a three-sided fire exposure
condition shall be considered in separate groups unless
the following conditions are satisfied:
a) The characteristics of the members of a group
as given below, shall not vary from one
another by more than
highest in group
1) Concrete density:
lowest in group
<1.25, and
largest in group
2) Effective thickness (h,):
smallest in group
SI.25.
where the effective thickness (h.) is equal to
the cross-sectional area excluding voids per
unit width, as shown in Fig. 25A.
b) IUb voids shall either be:
1) all open; or
2) all blocked as shown in Fig. 25B.
c) Concrete slabs may incorporate permanent
steel deck formwork.
16.10 Special Considerations
16.10.1 Connections
Connections shall be protected with the maximum
thickness of fire protection material required for any
of the members framing into the connection to
achieve their respective fire-resistance levels. This
thickness shall be maintained over all connection
components, including bolt heads, welds and splice
plates.
16.10.2 Web Penetrations
The thickness of tire protection material at and adjacent
to web penetrations shall be the greatest of that
required, when:
a) area above the penetration is considered as a
three-sided fire exposure condition (k,~l)
(see Fig. 26),
b) area below the penetration is considered as a
four-sided fire exposure condition (k,~2)
(see Fig. 26), and
108

IS 800:2007
c) section as a whole is considered as a three- 16.11 Fire Resistance Rating
sided fire exposure condition (k,~)
(see Fig. 26).
The fire resistance rating of various building
components such as walls, columns, beams, and floors
This thickness shall be applied over the full beam depth are given in Table 31 and Table 32. Fire damage
and shall extend on each side of the penetration for a assessment of various structural elements of the
distance at least equal to the beam depth and not less building and adequacy of the structural repairs can be
than 300 mm, done by the fire resistance rating for encased steel
column and beam (Table 31 and Table 32).
t
h-%lkr-E3ki’-J
& - i% .>
25A Effective Thickness
VOID BLOCKED WITH
FIREPROTECTION
~RETE SLAB MATERIAL
}
/’
4
STEELBEAM
FIREPROTECTION
MATERIAL
SIDEVIEW CROSS SECTION
25B Blocking of Rib Voids
FIG. 25 THREESIDEDFIRE EXPOSURE
CONDITION
REQUIREMENTS
w
Side View of Beam with Web Penetration
. . .. ......#...:,.
.. . . . .. . -., .,., . . . . .
kSmf
ii
SECTIONA-A SECTIONB-B
FIG. 26 WEB PENETRATION
109

IS 800:2007
Table 31 Encased Steel Columns, 203 mm x 203 mm
(Protection Applied on Four Sides)
(Clause 16.1 1)
SI Nature of Construction and Materials Minimum Dimensions Excluding Any Fhrish, for a Fire
No. Resistance of
mm
lh 1 fih 2h 3h 4 h’
(1) (2) (3) (4) (5) (6) (7)
O Hollow protection (without an air cavitv over the flan~es):
O
b)
c)
d)
e)
f-)
Metallathingwithtrowelledligh~weight
aggreg~te’gypsum
plaster‘)
Plasterboardwith 1.6mm wire binding at 100mm pitch,
finished with lightweight aggregate gypsum plaster less
than the thickness specified:
I) 9.5 mm plaster board
2) 19mm plaster board
Asbestos insulating boards, thickness of board:
1) Single thickness of board, with 6 mm cover fillets at
transverse joints
2) Two layers, of total thickness
Solid bricks Ofclay, composition or sand lime, reinforced
in every horizontal joint, unplastered
Aerated concrete blocks
Solid blocks of lightweight concrete bellow protection
13 15 20 32 –
10
10
15
13
—
—
20
2.5
19
— —
38
75
50
100
—
50
—
50 50
60
50
60
50
60
50
—
60 75
(with an air cavity over the flanges)
ii) Asbestos insulating board screwed to 25 mm asbestos battens
iii) Solid protections
a) Concrete, not leaner than 1:2:4 mix (unplastered):
1) Concrete not assumed to be load bearing, reinforced 2)
2) Concrete assumed to be load bearing
b) Lightweight concrete, not leaner than 1:2:4 mix (unplast-
ered) concrete not assumed to be load bearing, reinforced 2)
‘)So fixed or designed. as to allow full Penetration for mechanical bond.
19 —
25
50
25
25
50
25
25 50 75
50 ’75 75
25 25 25
‘1Reinforcement ~hallconsist Ofsteel ilnd]ng wire not less than 2.3 mm diameter, or a steel mesh weighing not lesstharrO.sk@2. ln
concrete protection, the spacing of the reinforcement shall not exceed 200 mm in any direction.
SECTION 17
FABRICATION AND ERECTION
1’7.1 General
Tolerances for fabrication of steel structures shall
conform to IS 7215. Tolerances for erection of steel
structures shall conform to IS 12843. For general
guidance on fabrication by welding, reference maybe
made to IS 9595.
17.2 Fabrication Procedures
17.2.1 Straightening
Material shall be straightened or formed to the specified
configuration by methods that will not reduce the
properties of the material below the values used in
design. Local application of pressure at room or at
elevated temperature or other thermal means may be
used for straightening, provided the above is satisfied.
17.2.2 Clearances
The erection clearance for cleated ends of members.
connecting steel to steel should preferably be not
greater than 2,0 mm at each end. The erection clearance
at ends of beams without web cleats should be not more
than 3 mm at each end. Where for practical reasons,
greater clearance is necessary, suitably designed seating
should be provided.
17.2.2.1 In bearing type of connections, the holes may
be made not more than 1.5 mm greater than the
diameter of the bolts in case of bolts of diameter less
than 25 mm and not more than 2 mm in case of bolts
of diameter more than 25 mm, unless otherwise
specified by the engineer. The hole diameter in base
plates shall not exceed the anchor bolt diameter by
more than 6 mm.
17.2.2.2 In friction type of connection clearance may
be maintained, unless specified otherwise in the design
document.
17.2.3 Cutting
Cutting shall be effected by sawing, shearing, cropping,
machining or thermal cutting process. Shearing,
110

..
_,.,_ _.
IS 800:2007
Table 32 Encased Steel Beams, 406 mm x 176 mm
(Protection Applied on Three Sides)
(Clause 16.11 )
S1 Nature of Construction and Materials Minimum Thickness of Protection for a Fire
No. Resistance of
mm
/
A
?
1/2 h Ih lfih 2h 3h 4h
(1) (2) (3) (4) (5) (6) (7) (8)
i) Hollowprotection(withoutan air cavitybeneaththe lowerflanges):
a) Metallathingwithtrowelledlightweightaggregategypsumplaster’) 13 13 15 20 25
b) Plasterboardwith 1.6mm wire binding at 100mm pitch, finished with
lightweight aggregate gypsum plaster less than the thickness specitiedz)
1) 9.5 mm plaster board 10 10 15 — — —
2) 19 mm plaster board 10 10 13 20 —
c) Asbestosinsulatingboards, thickness of board
1) Singlettdcknessof board,with 6 mm coverfilletsattransversejoints — — 19 25 —
2) Twolayers,of total thickness — — — — 38 50
ii) HO11OW
protection(withan air cavitybelowthe lowerflange)
@ Asbestosinsulatingboard screwed to 25 mm asbestos battens 9 12 — —
iii) Solid protections
a) Concrete, not leaner than 1:2:4mix (unpkistered):
1) Concrete not assumed to be load bearing, reinforced 3) 25 25 25 25 50 75
2) Concrete assumed to be load bearing 50 50 50 50 75 75
b) Lightweightconcrete,not leanerthan 1:2:4mix(unplastered)4) 25 25 25 25 40 60
1)so fixedordesigned,asto allowfullpenetrationformechanicalbond.
‘)Wherewirebindingc~not be used,expertadviceshouldbe soughtregarding akemative methods OfSupportto enablethe loweredges
oftheplasterboard to be fixed together and to the lower flange, and for the top edge of the plasterboard to be held in position.
3)Reinforcement shall consist of s~el binding wire not less than 2.3 mm in diameter, or a steel mesh weighing not less than o.5 k~mz. In
concrete protection, the spacing of the reinforcement shall not exceed 200 mm in any direction.
4)Concrete
notassumed to be load bearing, reinforced.
cropping and gas cutting shall be clean, reasonably
square, and free from any distortion. Should the
inspector find it necessary, the edges shall be ground
after cutting. Planning or finishing of sheared or gas-
cut edges of plates or shapes shall not be required,
unless specially noted on drawing or included in
stipulated edge preparation for welding or when
specifically required in the following section.
Re-entrant comers shall be free from notches and shall
have largest practical radii with a minimum radius of
15 mm.
17.2.3.1 Shearing
Shearing of items over 16 mm thick to be galvanized
and subject to tensile force or bending moment shall
not be carried out, unless the item is stress relieved
subsequently.
The use of sheared edges in the tension area shall be
avoided in location subject to plastic hinge rotation at
factored loading.
17.2.3.2 Thermal cutting
Gas cutting of high tensile steel by mechanically
controlled torch may be permitted, provided special
care is taken to leave sufficient metal to be removed
by machining, so that all metal that has been hardened
by flame is removed. Hand flame cutting may be
permitted only subject to the approval of the inspecting
authority.
Except where the material is subsequently joined by
welding, no load shall be transmitted through a gas
cut surface.
Thermally cut free edges, which shall be subject to
calculated static tensile stress shall be free from round
bottom gouges greater than 5 mm deep. Gouges greater
than 5 mm deep and notches shall be removed by
grinding.
17.2.4 Holing
17.2.4.1 Holes through more than one thickness of
material for members, such as compound stanchion and
girder flanges, shall be where possible, drilled after the
members are assembled and tightly clamped or bolted
together. Around hole for a bolt shall either be machine
flame cut, or drilled full size, or sub-punched 3 mm
undersize and reamed to size or punched full size.
Hand flame cutting of a bolt hole shall not be permitted
except as a site rectification measure for holes in
column base plates.
111

IS 800:2007
17.2.4.2 Punching
A punched hole shall be permitted only in ‘material
whose yield stress WY)does not exceed 360 MPa and
where thickness does not exceed (5 600/~Y) mm. In
cyclically loaded details, punching shall be avoided in
plates with thickness greater than 12 mm.
For greater thickness and cyclically loaded details,
holes shall be either drilled from the solid or sub-
punched or sub-drilled and reamed.
The die for all sub-punched holes or the drill for all
sub-drilled holes shall be at least 3 mm smaller than
the required diameter of finished hole.
17.2.4.3 Oversize holes
A special plate washer of minimum thickness 4 mm
shall be used under the nut, if the hole diameter is larger
than the bolt diameter by 3 mm or more.
Oversize hole shall not exceed 1.25d or (d+8) mm in
diameter, were d is the nominal bolt diameter, in mm.
A short slotted hole shall not exceed the appropriate
hole size in width and 1.33d in length. A long slotted
hole shall not exceed the appropriate hole size in width
and 2.5d in length. If the slot length is larger than those
specified, shear transfer in the direction of slot is not
admissible even in friction type of connection.
Slotted holes shall be punched either in one operation
or else formed by punching or drilling two round holes
apart and completed by high quality mechanically
controlled flame cutting and dressing to ensure that
bolt can freely travel the full length of the slot.
17.2.4.4 Fitted bolt holes
Holes for turned and fitted bolts shall be drilled to a
diameter equal to the nominal diameter of the shank
or barrel subject to tolerance specified in IS 919 (Parts
1 and 2). Preferably, parts to be connected with close
tolerance or barrel bolts shall be firmly held together
by tacking bolts or clamps and the holes drilled through
all the thicknesses at one operation and subsequently
reamed to size. All holes not drilled through all
thicknesses atone operation shall be drilled to a smaller
size and reamed out after assembly. Where this is not
practicable, the parts shall be drilled and reamed
separately through hard bushed steel jigs.
17.2.4.5 Holes for rivets or bolts shall not be formed
generally by gas cutting process. However, advanced
gas cutting processes such as plasma cutting may be
used to make holes in statically loaded members only.
In cyclically loaded members subjected to tensile
stresses which are vulnerable under fatigue, gas cutting
shall not be used unless subsequent reaming is done to
remove the material in the heat affected zone around
the hole.
17.3 Assembly
All parts of bolted members shall be pinned or bolted
and rigidly held together during assembly.
The component parts shall be assembled and aligned
in such a manner that they are neither twisted nor
otherwise damaged, and shall’ be so prepared that the
specified camber, if any, is provided.
17.3.1 Holes in Assembly
When holes are drilled in one operation through two
or more separable parts, these parts, when so specified
by the engineer, shall be separated after drilling and
the burrs removed.
Matching holes for rivets and black bolts shall register
with each other so that a gauge of 1.5 mm or 2.0 mm
(as the case may be, depending on whether the diameter
of the rivet or bolt is less than or more than 25 mm)
less in diameter than the diameter of the hole will pass
freely through the assembled members in the direction
at right angle to such members.
Drilling done during assembly to align holes shall not
distort the metal or enlarge the holes.
Holes in adjacent part shall match sufficiently well to
permit easy entry of bolts. If necessary, holes except
oversize or slotted holes maybe enlarged to admit bolts,
by moderate amount of reaming.
17.3.2 Thread Length
When design is based on bobs with unthreaded shanks
in the shear plane, appropriate measures shall be
specified to ensure that, after allowing for tolerance,
neither the threads nor the thread run-out be in the shear
plane.
The length of bolt shall be such that at least one clear
thread shows above the nut and at least one thread plus
the thread run out is clear beneath the nut after
tightening. One washer shall be provided under the
rotated part.
17.3.3 Assembly Subjected to Vibration
When non-preloaded bolts are used in a structure
subject to vibration, the nuts shall be secured by locking
devices or other mechanical means. The nuts of
preloaded bolts may be assumed to be sufficiently
secured by the normal tightening procedure.
17.3.4 Washers
Washers are not normally required on non-preloaded
bolts, unless specified otherwise. Tapered washers shall
be used where the surface is inclined at more than 3“to
a plane perpendicular to the bolt axis.
Hardened washer shall be used for preloaded bolts or
the nut, whichever is to be rotated.
112

All material within the grip of the bolt shall be steel
and no compressible material shall be permitted in the
grip.
17.4 Riveting
17.4.1 Rivets shall be heated uniformly throughout
their length, without burning or excessive scaling, and
shall be of sufficient length to provide a head of
standard dimensions. These shall, when driven,
completely fill the holes and, if countersunk, the
countersinking shall be fully filled by the rivet. lf
required, any protrusion of the countersunk head shall
be dressed off ftush.
17.4.2 Riveted member shall have all parts firmly
drawn and held together before and during riveting,
and special care shall be taken in this respect for all
single-riveted connections. For multiple riveted
connections, a service bolt shall be provided in every
third or fourth hole.
17.4.3 Wherever practicable, machine riveting shall be
carried out by using machines of the steady pressure
type.
17.4.4 All loose, burned or otherwise defective rivets
shall be cut out and replaced before the structure is
loaded, and special care shall be taken to inspect all
single riveted connections.
17.4.5 Special care shall be taken in heating and driving
long rivets.
17.5 Bolting
17.5.1 In all cases where the full bearing area of the
bolt is to be developed, the bolt shall be provided with
a washer of sufficient thickness under the nut to avoid
any threaded portion of the bolt being within the
thickness or the parts bolted together, unless accounted
for in design.
17.5.2 Pre-tensioned bolts shall be subjected to initial
tension (the proof stress) by an appropriate pre-
calibmted method.
17.6 Welding
17.6.1 Welding shall be in accordance with IS 816,
IS 819, IS 1024, IS 1261, IS 1323 and IS 9595, as
appropriate.
17.6.2 For welding of any particular type of joint,
welders shall give evidence acceptable to the purchaser
of having satisfactorily completed appropriate tests as
prescribed in IS 817, IS 1393, IS 7307 (Part 1), IS 7310
(Part 1) andIS7318 (Part 1), as relevant.
17.6.3 Assembly and welding shall be carried out in
such a way to minimize distortion and residuat stress
IS 800:2007
and that the final dimensions are within appropriate
tolerances.
17.7 Machining of Butts, Caps and Bases
17.7.1 Column splices and butt joints of struts and
compression members, depending on contact for stress
transmission, shall be accurately machined and close-
butted over the whole section with a clearance not
exceeding 0.2 mm locally, at any place. Sum of all
such clearance shall not be more than 30 percent of
the contact area for stress transmission. In column caps
and bases, the ends of shafts together with the attached
gussets, angles, channels, etc; after connecting together
should be accurately machined so that clearance
between the contact surfaces shall not exceed 2 mm
locally, subject further to the condition that sum total
of all such clearance shall not exceed 30 percent of the
total contact area for stress transmission. Care should
be taken that these gussets, connecting angles or
channels are fixed with such accuracy that they are
not reduced in thickness by machining by more than
2.0 mm,
17.7.2 Where sufficient gussets and rivets or welds are
provided to transmit the entire loading (see Section 4),
the column ends need not be machined.
17.7.3 Slab Bases and Caps
Slab bases and slab caps, except when cut from material
with true surfaces, shall be accurately machined over
the bearing surfaces and shall be in effective contact
with the end of the stanchion, the bearing face which
is to be grouted to fit tightly at both top and bottom,
unless welds are provided to transmit the entire column
face.
17.7.4 To Facilitate grouting, sufficient gap shall be left
between the base plates and top of pedestal and holes
shall be provided where necessary in stanchion bases
for the escape of air.
17.8 Painting
17.8.1 Painting shall be done in accordance with
IS 1477 (Parts 1 and 2).
17.8.2 All surfaces, which are to be painted, oiled or
otherwise treated, shall be dry and thoroughly cleaned
to remove all loose scale and loose rust.
17.8.3 Shop contzact surfaces need not be painted unless
specified. If so specified, they shall be brought together
while the paint is still wet.
17.8.4 Surfaces not in contact, but inaccessible after
shop assembly, shall receive tbe full specified
protective treatment before assembly. This does not
apply to the interior of sealed hollow sectiorf$.
113

IS 800:2007
17.8.5 Chequered plates shall be painted but the details
of painting shall be specified by the purchaser.
17.8.6 In case of surfaces to be welded, the steel shall
not be painted or metal coated within a suitable distance
of any edge to be welded, if the paint specified or the
metal coating is likely to be harmful to welders or
impair the quality of the welds.
17.8.7 Welds and adjacent parent metal shall not be
painted prior to de-slagging, inspection and approval.
17.8.8 Parts to be encased in concrete shall not be
painted or oiled.
17.8.9 Contact surface in friction type connection shall
not be painted in advance.
17.9 Marking
Each piece of steel work shall be distinctly marked
before dispatch, in accordance with a marking diagram
and shall bear such other marks as will facilitate
erection,
17.10 Shop Erection
17.10.1 The steel work shall be temporarily shop
erected complete or as arranged with the inspection
agency so that accuracy of fit may be checked before
dispatch. The parts shall be shop assembled with
sufficient numbers of parallel drifts to bring and keep
the parts in place.
17.10.2 In the case of parts drilled or punched, through
steel jigs with bushes resulting in all similar parts being
interchangeable, the steelwork maybe shop erected in
such position as arranged with the inspection agency.
17.10.3 In case of shop fabrication using numerically
controlled machine data generated by computer
software (like CAD), the shop erection may be
dispensed with at the discretion of the inspector.
17.11 Packing
All projecting plates or bars and all ends of members
at joints shall be stiffened, all straight bars and plates
shall be bundled, all screwed ends and machined
surfaces shall be suitably packed and all rivets, bolts,
nuts, washers and small and loose parts shall be packed
separately in cases, so as to prevent damage or
distortion during transit.
17.12 Inspection and Testing
17.12.1 The inspecting authority shall have free access
at all reasonable times to those parts of the
manufacturer’s works which are concerned with the
fabrication of the steelwork and shall be afforded all
reasonable facilities for satisfying himself that the
fabrication is being undertaken in accordance with the
provisions of this standard.
17.12.2 Unless specified otherwise, inspection shall
be made at the place of manufacture prior to dispatch
and shall be conducted so as not to interfere
unnecessarily with the operation of the work.
17.12.3 The manufacturer shall guarantee compliance
with the provisions of this standard, if required to do
so by the purchaser.
17.12.4 Should any structure or part of a structure be
found not to comply with any of the provisions of this
standard, it shall be liable to rejection. No structure or
part of the structure, once rejected shall be resubmitted
for test, except in cases where the purchaser or his
authorized representative considers the defect as
rectifiable.
17.12,5 Defects, which may appear during fabrication,
shall be made good with the consent of and according
to the procedure laid down by the inspecting authority.
17.12.6 All gauges and templates necessary to satisfy
the inspection authority shall be supplied by the
manufacturer. The inspecting authority may, at his
discretion, check the test results obtained at the
manufacturer’s works by independent testing at outside
laboratory, and should the material so tested be found
to be unsatisfactory, the cost of such tests shall be borne
by the manufacturer, and if found satisfactory, the cost
shall be borne by the purchaser.
17.13 Site Erection
17.13.1 Plant and Equipment
The suitability and capacity of all plant and equipment
used for erection shall be to the satisfaction of the
engineer.
17.13.2 Storing and Handling
All structural steel should be so stored and handled at
the site that the members are not subjected to excessive
stresses and damage by corrosion due to exposure to
environment.
17.13.3 Setting Out
The positioning and Ievelling of all steelwork, the
plumbing of stanchions and the placing of every part
of the structure with accuracy shall be in accordance
with the approved drawings and to the satisfaction of
the engineer in accordance with the deviation permitted
below.
17.13.3.1 Erection tolerances
Unloaded steel structure, as erected, shall satisfy the
criteria specified in Table 33 within the specified
tolerance limits.
114

Each criterion given in the table shall be considered as
a separate requirement, to be satisfied independent of
any other tolerance criteria. The erection tolerances
specified in Table 33 apply to the following reference
points:
a) For a column, the actual centre point of the
column at each floor level and at the base,
excluding any base-plate or cap-plate. The
level of the base plate on pedestal shall be so
as to avoid contact with soil and corrosive
environment; and
b) For a beam, the actual centre point of the top
surface at each end of the beam, excluding
any end-plate.
Table 33 Normal Tolerances After Erection
L% Criterion Permitted Deviation
No.
(1) (2) (3)
O
ii)
iii)
iv)
v)
Deviation of distance
between adjacent columns
Inclinationof a columnin a
multi-storey building
between adjacent floor
levels
Deviation of location of a
column in a multi-storey
building at any floor level
from a vertical line
through the intended
location of the column
base
Inclination ofa column in
a single storey building,
(not supporting a crane
gantry) r)therthan a portal
frame
Inclination of the column
of a portal frame (not
supporting a crane gantry)
5 mm
0.002h,
where, h, is the storey height
0.0035 z M+”’
where, z hb is the total height
from the base to the floor
level concerned and n is the
number of storeys from the
base to the floor level
concerned
0.003 5h.
where, h. is the height of the
column
Mean:0.002h,
Individual: O.OIOhC
where h, is the height of the
column
The straightness tolerances specified in Table 34 have
been assumed in the derivation of the design stress for
the relevant type of member. Where the curvature
exceeds these values, the effect of additional curvature
on the design calculations shall be reviewed.
A tension member shall not deviate from its correct
position relative to the members to which it is
connected by more than 3 mm along any setting axis.
17.13.4 Safety During Fabrication and Erection
17.13.4.1 All steel materials including fabricated
structures, either at fabrication shop or at erection site,
shall be handled only by a worker skilled in such jobs;
where necessary with load tested lifting devices, having
IS 800:2007
tested wire rope slings of correct size. The devices
should be well maintained and operated by experienced
operators.
Table 34 Straightness Tolerances Incorporated in
Design Rules
(Clause 7.13.3.1)
S1 Criterion Permitted Deviation
No.
(1) (2) (3)
O Straightness of a column (or
other compression member)
between points which will be
laterally restrained on
completion of erection
ii) Straightness of a
compressionflangeof a
beam,relativeto the weak
axis,betweenpoints,which
willbe laterallyrestrainedon
completionof erection.
0.00 IL generally, and
0.002L for members with
hollow cross-sections;
where, L is the length
between points which will
be laterally restrained
0.001L generally, and
0.002L for members with
hollow cross-sections;
where, L is the length
between points which will
be laterally restrained
17.13.4.2 Oxygen and acetylene cylinders and their
hoses shall have distinctive colours. Cylinders should
be stored in upright position in well-ventilated rooms
or in open air, not exposed to flames, naked lights or
extreme heat and should also be in upright position
when they are being used. All gas cutting works shall
be done only by experienced skilled gas cutters,
equipped with gloves, boots, aprons, goggles and good
cutting sets of approved make.
17.13.4.3 While doing any welding work, it should be
ensured that the welding machine is earthed and the
welding cables are free from damage. The welder and
his assistant shall use a face shield or head shield with
a welding lens and clear cover glass and their hands,
legs and bodies shall be well protected by leather
gloves, shoes and aprons. Combustible materials should
be kept away from the sparks and globules of molten
metals generated in any arc welding. In case of welding
in a confined place, it should be provided with an
exhaust system to take care of the harmful gases, fumes
and dusts generated.
17.13.4.4 In addition to precautions against all the
hazards mentioned above, erection workers shall also
be protected in the following manne~
a) All workers shall wear helmets and shall also
be provided with gloves and shoes. In addition
those working at heights shall use safety belts.
b) All structures shall be so braced/guyed during
erection that there is no possibility of collapse
before erection work is completed.
c) Warning signs such as ‘Danger’, ‘Caution’,
115

IS 800:2007
’440 volts’, ‘Do not smoke’, ‘Look ahead’,
etc; should be displayed at appropriate
places,
17.13.4.5 For detailed safety precautions during
erection, reference shall be made to IS 7205.
17.13.5 Field Connections
17.13.5.1 Field riveting
Rivets driven at the site shall be heated and driven with
the same care as those driven in the shop.
17.13.5.2 Field bolting
Field bolting shall be carried out with the same care as
required for shop bolting.
17.13.5.3 Fillet welding
Field assembly and welding shall be executed in
accordance with the requirements for shop fabrications
excepting such as manifestly apply to shop conditions
only. Where the steel has been delivered painted, the
paint shall be removed for a distance of at least 50 mm
on either side of the joint.
17.14 Painting After Erection
17.14.1 Before painting of such steel which is delivered
unpainted is commenced, all surfaces to be painted
shall be dry and thoroughly cleaned from all loose scale
and rust, as required by the surface protection
specification.
17.14.2 The specified protective treatment shall be
~ompleted after erection. All rivet and bolt heads and
the site welds after de-slagging shall be cleaned.
Damaged or deteriorated paint surfaces shall first be
made good with the same type of paint as the shop
coat. Where specified, surfaces which will be in contact
after site assembly, shall receive a coat of paint
(in addition to any shop priming) and shall be brought
together while the paint is still wet. No painting shall
be used on contact surfaces in the friction connection,
unless specified otherwise by the design document.
17.14.3 Where the steel has received a metal coating
in the shop, this coating shall be completed on site so
as to be continuous over any welds and site rivets or
bolts, subject to the approval of the engineer. Painting
on site may complete protection. Bolts, which have
been galvanized or similarly treated, are exempted from
this requirement.
17.14.4 Surface, which will be inaccessible after site
assembly, shall receive the full-specified protective
treatment before assembly.
17.14.5 Site painting should not be done in frosty or
foggy weather, or when humidity is such as to cause
condensation on the surfaces to be painted.
17.15 Bedding Requirement
17.15.1 Bedding shall be carried out with Portland
cement grout or mortar, as described under 17.15.4 or
fine cement concrete in accordance with IS 456.
17.15.2 For multi-storeyed buildings, this operation
shall not be carried out until a sufficient number of
bottom lengths of stanchions have been properly lined,
leveled and plumbed and sufficient floor beams are in
position.
17.15.3 Whatever method is employed, the operation
shall not be carried out until the steelwork has been
finally Ievelled and plumbed, stanchion bases being
supported meanwhile by steel wedges or nuts; and
immediately before grouting, the space under the steel
shall be thoroughly cleaned.
17.15.4 Bedding of structure shall be carried out with
grout or mortar, which shall be of adequate strength
and shall completely fill the space to be grouted and
shall either be placed under pressure or by ramming
against fixed supports. The grouts or mortar used shall
be non’-shrinking variety.
17.16 Steelwork Tenders and Contracts
A few recommendations are given in Annex G for
general information.
116

IS 800:2007
ANNEX A
(Clause 1.1)
LIST OF REFERRED INDIAN STANDARDS
IS No.
456:2000
513:1994
801:1975
808:1989
813:1986
814:2004
816:1969
817
(Part 1): 1992
(Part 2): 1996
819:1957
875
(Part 1): 1987
(Part 2): 1987
(Part 3): 1987
(Part 4): 1987
(Part 5): 1987
919
(Part 1): 1993/
Title
Plain and reinforced concrete —
Code of practice ~ourth revision)
Cold-rolled low carbon steel sheets
and strips (fourth revision)
Code of practice for use of cold-
formed light gauge steel structural
members in general building
construction first revision)
Dimensions for hot-rolled steel
beam, column, channel and angle
sections (third revision)
Scheme of symbols for welding
Covered electrodes for manual metat
arc welding of carbon and carbon
manganese steel — Specification
(sixth revision)
Code of practice for use of metal arc
welding for general construction in
mild steel (first revision)
Training of welders — Code of
practice:
Manual metal arc welding (second
revision)
Oxyfuel welding (second revision)
Code of practice for resistance spot
welding for light assemblies in
mild steel
Code of practice for design loads
(other than earthquake) for
buildings and structures:
Dead loads – unit weights of building
materials and stored materials
(second revision)
Imposed loads (second revision)
Wind loads (second revision)
Snow loads (second revision)
Special loads and load combinations
(second revision)
1S0 systems of limits and fits:
Bases of tolerance, deviations and fits
ISO 286-1:1988 (second revision)
(Part 2) : 1993/ Tables of standard tolerance grades
1S0 286-2:1988 and limit deviations for holes and
shafts (/lrst revision)
962:1989 Code of practice for architectural and
building drawings (second revision)
1024:1999 Code of practice for use of welding
in bridges and structures subject to
dynamic loading (second revision)
IS No.
1030:1998
1079:1994
1148:1982
1149:1982
1261:1959
1278:
1323:
1363
972
982
(Part 1): 2002/
1S0 4016:1999
(Part 2): 2002/
1S04018:1999
(Part 3): 1992/
1S0 4034:1986
1364
(Part 1): 2002/
1s04014:1999
(Part 2): 2002/
1S04017:1999
(Part 3): 2002/
1S04032:1999
(Part 4): 2003/
1s0 4035:1999
(Part 5): 2002/
1S0 4036:1999
1367
(Part 1): 2002/
1S0 8992:1986
(Part 2): 2002/
Title
Carbon steel castings for general
engineering purposes ~fth revision)
Hot rolled carbon steel sheets and
strips — Specification @fib revision)
Specification for hot-rolled rivet bars
(up to 40 mm diameter) for structural
purposes (third revision)
High tensile steel rivet bars for
structural purposes (third revision)
Code of practice for seam welding
in mild steel
Specification for filler rods and wires
for gas welding (second revision)
Code of practice for oxy-acetylene
welding for structural work in mild
steels (second revision)
Hexagon head bolts, screws and nuts
of product grade C:
Hexagon head bolts (size range M5
to M64) ~ourth revision)
Hexagon head screws (size range M5
Hexagon nuts (size range M5 to M64)
(third revision)
Hexagon head bolts, screws and nuts
of product grades A and B:
Hexagon head bolts (size range Ml.6
Hexagon head screws (size range
Ml.6 to M64) (jourth revision)
Hexagon nuts, style 1 (size range
M 1.6 to M64) (fourth revision) -
Hexagon thin nuts (chamfered) (size
range M 1.6 to M64) ($ourth revision)
Hexagon thin nuts — Product grade B
(unchamfered) (size range Ml.6 to
M1O) ~ourth revision)
Technical supply conditions for
threaded steel fasteners:
Generat requirements for bolts, screws
and studs (third revision)
Tolerances for fasteners — Bolts,
1S04759-1 :2000 screws, studs and nuts — Product
grades A, B and C (third revision)
(Part 3): 2002/ Mechanical properties of fasteners
1S0 898-1:1999 made of carbon steel and alloy steel
— bolts, screws and studs ~ourth
revision)
117

IS 800:2007
IS No. Title
(Part 5) : 2002/ Mechanical properties of fasteners
1S0 898-5:1998 made of carbon steel and alloy steei
—set screws and similar threaded
fasteners not under tensile stresses
(third revision)
(Part 6): 1994/ Mechanical properties and test methods
ISO 898-2:1992 for nuts with specified proof loads
(third revision)
(Part 7): 1980 Mechanical properties and test
methods for nuts without specified
proof loads (second revision)
(Part 8) : 2002/ Prevailing torque type steel hexagon
1S0 2320:1997 nuts — Mechanical and performance
properties (third revision)
(Part 9) Surface discontinuities
Sec 1:1993/ Bolts, screws and studs for general
1S0 6157-1:1988 application (third revision)
Sec 2:19931 Bolts, screws and studs for special
1S0 6157-3:1988 applications (third revision)
(Part 10):2002/ Surface discontinuities — Nuts (third
1S0 6157-2:1995 revision)
(Part 11):2002/ Electroplated coatings (tlzzki revision)
1S0 4042:1999
(Part 12):1981 Phosphate coatings on threaded
fasteners (second revision)
(Part 13):1983 Hot dip galvanized coatings on
threaded fasteners (second revision)
(Part 14) Mechanical properties of corrosion-
resistant stainless-steel fasteners,
Sec 1: 2002/ Bolts, screws and studs (third revision)
1S0 3506-1:1997
Sec 2:20021 Nuts (third revision)
1s0 3506-21997
Sec 3:20021 Set screws and similar fasteners not
1S0 3506-3:1997 under tensile stress (third revision)
(Part 16) : 2002/ Designation system for fasteners
1S0 8991:1986 (third revision)
(Part 17) : 1996/ Inspection, sampling and acceptance
ISO 3269:1988 procedure (third revision)
(Part 18) :1996 Packaging (third revision)
(Part 19) : 1997/ Axial load fatigue testing of bolts,
1S0 3800:1993 screws and studs
(Part 20) : 1996/ Torsional test and minimum torques
1S0 898-7:1992 for bolts and screws with nominal
diameters 1 mm to 10 mm
1387:1993 General requirements for the supply
of metallurgical materials (second
revision)
1393:1961 Code of practice for training and
testing of oxy-acetylene welders
1395:1982 Low and medium alloy steel covered
electrodes for manual metal arc
welding (third revision)
IS No.
1477
(Part 1): 1971
(Part 2): 1971
1608: 2005/
ISO 6892:1998
1641:1988
1642:1989
1643:1988
1852:1985
1875:1992
1893
(Part 1): 2002
1929:1982
1990:1973
2002:1992
2062:2006
2155:1982
2708:1993
3039:1988
3613:1974
3640:1982
3757:1985
4000:1992
4326:1993
Title
Code of practice for painting of
ferrous metals in buildings:
Pre-treatment (/irst revision)
Painting (first revision)
Metallic materials —Tensile testing at
ambient temperatures (third revision)
Code of. practice for fire safety of
buildings (general): General
principles of fire grading and
classification (first revision)
Code of practice for fire safety of
buildings (general): Details of
construction (@ revision)
Code of practice for fire safety of
buildings (general): Exposure hazard
(jirst revision)
Rolling and cutting tolerance for hot
rolled steel products ~ourth revision)
Specification for carbon steel billets,
blooms, slabs and bars for forgings
(fi$’h revision)
Criteria for earthquake resistant design
of structures: Part 1 General
provisions and buildings
Specification for hot forged steel
rivets for hot closing (12 to 36 mm
diameter) tjirst revision)
Steel rivet and stay bars for boilers
(/k revision)
Steel plates for pressure vessels for
intermediate and high temperature
service including boilers (second
revision)
Hot rolled low, medium and high
tensile structural steel (sixth revision)
Specification for cold forged solid
steel rivets for hot closing (6 to 16 mm
diameter) (first revision)
1.5 percent manganese steel castings
for general engineering purpose
(third revision)
Structural steel for construction of
hulls of ships (second revision)
Acceptance tests for wire flux
combination for submerged arc
welding (first revision)
Specification for hexagon fit bolts
(jlrsl revision)
Specification for high strength
structural bolts (second revision)
Code of practice for high strength
bolts in steel structures tjirst revision)
Code of practice for earthquake
resistance design and construction of
buildings (second revision)
118

-
IS 800:2007
IS No.
5369:1975
5370:1969
5372:1975
5374:1975
5624:1993
6240:1999
6419:1996
6560 ; 1996
6610:1972
6623:2004
6639:1972
6649:1985
7205:1974
7215:1974
7280:1974
7307
(Part 1): 1974
7310
Title
General requirements for plain
washers and lock washers (first
revision)
Specification for plain washers with
outside diameter =3x inside dkmeter
Taper washers for channels (ISMC)
tjlrst revision)
Taper washers for I-beams (ISMB)
(jlrst revision)
Foundation bolts — Specification
(first revision)
Hot rolled steel plate (upto6 mm)
sheet and strip for the manufacture of
low pressure liquefiable gas cylinders
— Specification (third revision)
Welding rods and bare electrodes for
gas shielded arc welding of structural
steel (first revision)
Molybdenum and chromium-
molybdenum low alloy steel weldlng
rods and bare electrodes for gas
shielded arc welding (jirst revision)
Specification for heavy washers for
steel structures
High strength structural nuts —
Specification (first revision)
Specification for hexagonal bolts for
steel structures
Specification for hardened and
tempered washers for high strength
structural bolts and nuts @rst revision)
Safety code for erection of structural
steelwork
Specification for tolerances for
fabrication of steel structures
Specification for bare wire electrodes
for submerged arc welding of
structural steels
Approwd tests for welding procedures:
Part 1 Fusion welding of steel
Approval tests for welders working
to approved welding procedures
IS No.
(Part 1): 1974
7318 (Part 1):
1974
7557:1982
8000
(Part 1) : 1985/
1S0 1101:1983
(Part 2): 1992/
1S0 2692:1988
(Part 3): 1992/
1S0 1660:1987
(Part 4): 1976
8976:1978
9077:1979
9172:
9295:
979
983
9595:1996
10748:2004
12843:1989
SP6 (1): 1964
Title
Part 1 Fusion welding of steel
Approval test for welders when weld-
ing procedure approval is not
required: Part 1 Fusion welding of
steel
Specification for steel wire (upto
20 mm) for the manufacture of cold
forged rivets (jhst revision)
Geometrical tolerancing on technical
drawings:
Tolerances of form, orientation, loca-
tion and run-out, and appropriate
geometrical definitions (Jirsf
revision)
Maximum material principles (first
revision)
Dimensioning and tolerancing of
profiles (second revision)
Practical examples of indications on
drawings
Guide for preparation and
arrangement of sets of drawings and
parts lists
Code of practice for corrosion
protection of steel reinforcement in
RB and RCC construction
Recommended design practice for
corrosion prevention of steel
structures
Steel tubes for idlers for belt
conveyors @rst revision)
Metal arc welding of carbon and
carbon manganese steels —
Recommendations (jirst revision)
Hot-rolled steel strip for welded
tubes and pipes — Specification
(second revision)
Tolerances for erection of steel
structures
Handbook for Structural Engineers —
Structural Steel Sections
119

IS 800:2007
ANNEX B
[Clause 4.1. 1(c)]
ANALYSIS AND DESIGN METHODS
B-1 ADVANCED STRUCTURAL ANALYSIS AND
DESIGN
B-1.l Analysis
For a frame, comprising members of compact section
with full lateral restraint, an advanced structural
analysis may be carried out, provided the analysis can
be shown to accurately model the actual behaviour of
that class of frames. The analysis shall take into
account the relevant material properties, residual
stresses, geometrical imperfections, reduction in
stiffness due to axial compression, second-order
effects, s.ecti~n strength and ductility, erection
procedures and interaction with the foundations.
Advanced structural analysis for earthquake loads shall
take into account, as appropriate the response history,
torsional response, pounding against adjacent
structures, and strain rate effects.
B-1.2 Design
For the strength limit state, it shall be sufficient to
satisfy the section capacity requirements of Section 8
for the members subjected to bending, of Section 7 for
axial members, of Section 9 for combined forces and
of Section 10 for connections. Effect of moment
magnification given in Section 9, instability given in
Section 7 and lateral buckling given in Section 8 need
not be considered while designing the member, since
advanced analysis methods directly consider these.
An advanced structural analysis for earthquake loads
shall recognize that the design basis earthquake loads
calculated in accordance with IS 1893 is assumed to
correspond to the load at which the first significant
plastic hinge forms in the structure.
B-2 SECOND ORDER ELASTIC ANALYSIS AND
DESIGN
B-2.1 Analysis
In a second-order elastic analysis, the members shall
be assumed to remain elastic, and changes in frame
geometry under the design load and changes in the
effective stiffness of the members due to axial forces
shall be accounted for. In a frame where the elastic
buckling load factor (AC,)of the frame as determined
in accordance with 4.6 is greater than 5, the changes
in the effective stiffness of the members due to axial
forces may be neglected.
B-2.2 Design Bending Moment
The design bending moment under factored load shall
be taken as the maximum bending moment in the length
of the member. It shall be determined either:
a)
b)
c)
directly from the second-order analysis; or
approximately, if the member is divided into
a sufficient number of elements, as the greatest
of the element end bending moments; or
by amplifying the calculated design bending
moment, taken as the maximum bending
moment along the length of a member as
obtained by superposition of the simple beam
bending moments determined by the analysis.
For a member with zero axial force or a member subject
to axial tension, the factored design bending moment
shall be calculated as the moment obtained from second
order analysis without any amplification.
For a member with a design axial compressive force
as determined from the analysis, the factored design
bending moment shall be calculated as follows:
where
5, =
M = &Mm
moment amplification factor for a braced
member determined in accordance with
Section 9.
B-3 FRAME INSTABILITY ANALYSIS
B-3.1 Analysis
Frame instability, as treated here, is related to the design
of multi-storey rigid-jointed frames subject to side
sway. The elastic critical load factor, k~~ may be
determined using the deflection method as given
in B-3.2 or any other recognized method. This is used
to calculate the amplified sway moments for elastic
designs and to check frame stability in plastic designs.
The elastic critical load factor, LC, of a frame is the
ratio by which each of the factored loads would have
to be increased to cause elastic instability.
B-3.2 Deflection Method
An accurate method of analysis (ordinary linear elastic
analysis) should be used to determine the horizontal
deflections of the frame due to horizontal forces applied
at each floor level, which is equal to the notional
horizontal load in 4.3.6. Allowance should be made
120

IS 800:2007
for the degree of rigidity of the base as given in B-3.2
in this deflection calculation.
The base stiffness should be determined by reference
to 4.3.4.
The elastic critical load factor, AC,is calculated as:
AC,= 1
200@s,M,x
where
4s,Max= largest value of the sway inde~y OSgiven
where
h=
8“ =
%=
storey height,
horizontal deflection of the top of the storey
due to the combined gravity and notional
loads, and
horizontal deflection of the bottom of the
storey due to gmvity and notional load.
B-3.3 Partial Sway Bracing
In any storey the stiffening effect of infill wall panels
may be allowed for by introducing a diagonal strut in
that storey of area A, given by:
where
h = storey height;
b = width of the braced bay;
zKC = sum of the stiffness I,L, of the columns
in that storey;
h’ ~SP
kj = s 2; and
80E~ Kc
~SP = surnof spring stiffness horizontal force
per unit horizontal deflection of all the
panels in that storey determined from:
Sp=
0.6h lb
[l+(@l’’pEp
where
‘P =
EP =
thickness of the wall panel, and
modulus of elasticit y of the panel material.
ANNEX C
[Clauses 5.2.2.2(b) and 5.6.2]
DESIGN AGAINST FLOOR VIBRATION
C-1 GENERAL
Floor with longer spans of lighter construction and less
inherent damping are vulnerable to vibrations under
normal human activity. Natural frequency of the floor
system corresponding to the lowest mode of vibration,
damping characteristics, are important characteristics
in floor vibration. Open web steel joists (trusses) or
steel beams on the concrete deck may experience
walking vibration problem. Fatigue, overloading of
floor systems and vibrations due to rhythmic activities
such as aerobic or dance classes are not within the scope
of this Annex.
C-2 ANNOYANCE CRITERIA
In the frt?quency range of 2 to 8 Hz in which people
are most sensitive to vibration, the threshold level
corresponds approximately to 0.5 percent g, where g
is the acceleration due to gravity. Continuous
vibration is generally more annoying then decaying
vibration due to damping. Floor systems with the
natural frequency less than 8 Hz in the case of floors
supporting rhythmic activity and 5 Hz in the case of
floors supporting normal human activity should be
avoided.
C-3 FLOOR FREQUENCY
The fundamental natural frequency can be estimated
by assuming full composite action, even in non-
composite construction. This frequency,$, for a simply
supported one way system is given by
j = 156~*
121

,.,,,,,
1111 II . “-
IS 800:2007
where
E=
IT =
f,=
w=
modulus of elasticity of steel, MPa;
transformed moment of inertia of the one
way system (in terms of equivalent steel)
assuming the concrete flange of width equal
to the spacing of the beam to be effective,
in mm4;
span length, in mm; and
dead load of the one way joist, in N/mm.
If the one way joist system is supported by a flexible
beam running perpendicular with the natural
frequency fz, the floor frequency may be reduced to
~, given by:
11
—=7++
fr2 A f,
C-4 DAMPING
The percentage of critical damping may be assumed
approximately as given below:
S1 System Critical Damping
No. Percent
(1) (2) (3)
i) Fully composite construction 2
ii) Bare steel beam and concrete deck 3-4
iii) Ftoor with finishes, false ceiling, 6
fire proofing, ducts furniture
iv) Partitions not located atong a up to 12
support or not spaced father apart
than 6 m and partitions oriented in
orthogonal dwtions
C-5 ACCELERATION
The peak acceleration ao, from heel impact for floors
of spans greater than 7m and natural frequency f], less
than 10 Hz may be calculated as:
where
w=
b=
t, =
t? =
ANNEX D
(Ckme 7.2.2)
aOlg = 600 f, /W
total weight of floors plus contents over the span
length and equivalent floor width (b), in N;
40t, (20 t,when over hang is only on one
side of the beam);
equivalent thickness of the slab, averaging
concrete in slab and ribs; and
acceleration due to gravity.
DETERMINATION OF EFFECTIVE LENGTH OF COLUMNS
D-1 METHOD FOR DETERMINING EFFECTIVE
LENGTH OF COLUMNS IN FRAMES
In the absence of a more exact analysis, the effective length
of columns in framed structures may be obtained by
multiplying the actual length of the column between the
centres of laterally suppotting members (beams) given
in Fig. 27 and Fig. 28 with the effective length factor K,
calculated by using the equations given below, provided
the connection between beam and column is rigid type:
a) Non-sway Fmmes (BracedFrame) [(see 4.12(a)]
A frame is designated as non-sway frame if
the relative displacement between the two
adjacent floors is restrained by bracings or
shear walls (see 4.1.2). The effective length
factor, K, of column in non-sway frames is
given by (see Fig. 27):
[1+0.145 (#, +@-0.265f11/32]
K= [2- O.364(fl, + ~, )- 0.247~,/3, ]
122
b) Sway Frames (Moment Resisting Frames)
[see 4.1.2(b)]
The effective length factor K, of column in
sway frames is given by (see Fig. 28):
-[ 1
K_
l-o.2(p, +p2)-o.12p,/?2 0’5
1– 0.8(~1 .+ /32)+ 0.6F,pz
where
Kc, Kb = effective flexural stiffness of the
columns and beams meeting at the
joint at the ends of the columns
and rigidly connected at the joints,
and these are calculated by:
K= C(I/L)

., “—--- . _
IS 800:2007
HINGED 1
0.9-
0.8-
0.7-
0.6-
t
0.5-
a- o,4-
0.3 -
0.2 “
0.1 “
0
FIXED 0.0 ‘* I I I I I I 1 I I
o 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
FIXED
P,—————
HINGED
FIG. 27 COLUMNEFFECTIVE
LENGTHFACTOR— NON-SWAYFRAME
PINNED
ai
FIXED
FIXED PINNEC)
P,~
FIG. 28 COLUMNEFFECTIVE
LENGTHFACTOR— SWAY FRAME
123

IS 800:2007
I = moment of inertia of the member about
an axis perpendicular to the plan of the
frame.
L = length of the member equal to centre-
to-centre distance of the intersecting
member.
C = correction factor as shown in Table 35.
Table 35 Correction Factors for Effective
Flexural Stiffness
S1 Far End Condition Correction Factor, C
No.
r’
A .
BracedFrame Unbraeed
Frame
(1) (2) (3) (4)
i) Pinned 1.5(1-ti) 1.5(1-E)
ii) Rigidly connected to column 1.0(1– n) 1.0(1- o.2Fi)
iii) Fixed 2.0(1-0.4E) 0.67(1 - 0.4E)
‘c
where
P. = elastic buckling load, and
P = applied load.
D-2 METHOD FOR DETERMINING EFFECTIVE
LENGTH FOR STEPPED COLUMNS (see 7.2.2)
D-2.1 Single Stepped Columns
Effective length in the plane of stepping (bending about
axis Z-Z) for bottom and top parts for single stepped
column shall be taken as given in Table 36.
NTOTE
— The provisions of D-2.1 are applicable to intermediate
columns as well with stepping on either side, provided
appropriate values Of IIand [j are taken.
D-3 EFFECTIVE LENGTH FOR DOUBLE
STEPPED COLUMNS
Effective lengths in the plane of steppings (bending
about axis Z-Z) for bottom, middle and top parts for a
double stepped column shall be taken as follows
(see also Fig. 29):
P3
L!3
J 1
p2 /3
i-----
r I“av
L2+L3
L2 p, /2
l--
P,
+-
L1 /1 L,
i-- “
‘1
(a) (b)
‘+F
YI
Coefficient K, for effective length of bottom part of
double stepped column shall be taken from the formula:
‘,=m
where
K,, Kz, and K3 are taken from Table41.
tl =
I’,v =
=
1“,, =
=
average value of moment of inertia for the
lower and middle parts
IILl i- IZLZ
LI + L,
average value of moment of inertia for the
middle and top parts
IZLZ i- I~L~
L, + L,
Value of coefficient Kz for middle part of column is
given by formula:
K2=~, and
2
coefficient KS for the top part of the column is given
by:
K3+3
3
where
c2=~
[
II (P2+P3)
L, 12(~+P2+P, )
c3=:m
NOTE — The provisions of D-3 are applicable to intermediate
columns as well with steppings on either side, provided
aPPf’OPriate
values of I,, 12and It are taken.
P3
L
11
p213 r ,3
t
L3
t
L1+L2 L,+L2
1-
/’av
1-
f’,“
(c) (d)
FIG. 29 EFFECTIVE
LENGTHOFDOUBLESTEPPEDCOLUMNS
124

1,
!1,
I
i’
IS 800:2007
Table 36 Effective Length of Single Stepped Columns
(Clause D-2. 1)
SI Degree of End Restraint Sketch Effeetive Length Coefficients
No.
Column Parameters for
All Cases
(1) (2) (3) (4) (5)
i) Effectively held in position
and restrained against
rotation at both ends
33
ii)
Effectively held in position
at both ends and restrained
against rotation at bottom
end only
iii)
iv)
Ii?
rotation at bottom end, and
top end held against
rotation but not held in
position
1
rotation at bottom end, and
top end neither held against
rotation nor held in
position
where
K,zand K,!areto be taken as
per Table 37
‘=
J’w7-
Kz=&3
I
where
K,zand Kll are to be taken as
per Table38
K, to be taken as per Table39
K, to be taken as per Table40
tl
1
12
-1
71
1,
L1
1
Effective length of bottom
part of column in plane 01
stepping = KVLI
Effective length of top part o]
column in plane of stepping=
K~L2
Table 37 Coeftlcients of Effective Lengths K12and K,, for columns with Both Ends Effectively Heid in
Position and Restrained Against Rotation
(Table 36)
Coeftlcients K12and K1lfor LJLI Equal to
12/1[ 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.2 L4 1.6 1.8 2.0
Coefficient KU (PI =0)
0.05 0.74 0.94 1.38 1.60 1.87 2.07 2.23 2.39 2.52 2.67 3.03 3.44 3.85 4.34 4.77
0.1 0.67 0.76 1.00 1.20 1.42 1.61 1.78 1.92 2.04 2.20 2.40 2.60 2.86 3.18 3.41 PZ
0.2 0.64 0.70 0.79 0.93 1.07 1.23 1.41 1.50 1.60 1.72 1.92 2.11 2.28 2.45 2.64
0.3 0.62 0.68 0.74 0.85 0.95 1.06 1.18 1.28 1.39 1.48 1.67 1.82 1.96 2.12 2.20 i L,
0.4 0.60 0.66 0.71 0.77 0.82 0.93 0.99 1.08
3
1.17 1.23 1.39 1.53 1.66 1.79 1.92 ~
0.5 0.59 0.65 0.70 0.77 0.82 0.93 0.99 1.08
1
1.17 1.23 1.39 1.53 1.66 1.79 1.92 /1 ‘1
1.0 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.00 1.10 1.20 1.30 1.40 1.50
Coefficient K,, (P2=O)
II L,
0.05 0.65 0.67 0.71 0.85 1.01 1.17 1.31 1.41 1.50 1.57 1.67 1.74 1.78 1.82 1.86
0.1 0.64 0.65 0.65 0.65 0.78 0.92 1.05 1.15 1.25 1.33 1.45 1.55 1.62 1.68 1.71 -1
0.2 0.62 0.64 0.65 0.65 0.66 0.73 0.83 0.92 1.01 1,09 1.23 1.33 1.41 1.48 1.54
0.3 0.60 0.63 0.64 0.65 0.66 0.67 0.73 0.81 0.89 0.94 1.09 1.20 1.28 1.35 1.41 1
0.4 0.58 0.63 0.63 0.64 0.64 0.66 0.68 0.75 0.82 0.88 1.01 1.10 1.19 1.26 1.32 P, +P2
0.5 0.57 0.61 0.63 0.64 0.64 0.65 0.68 0.72 0.77 0.83 0.94 1.04 1.12 1.19 1.25
1.0 0.55 0.58 0.60 0.61 0.62 0.63 0.65 0.67 0.70 0.73 0.80 0.88 0.93 1.01 1.05
NOTE— Intermediatevaluemaybe obtainedby interpolation.
125

IS800:2007
Table 38 Coefficients of Effective Lengths Klz
and Kll
for Columns with Both Ends Effectively Held in
Position and Restrained Against Rotation at Bottom End Only
(Table 36)
Coefficients KU and KII for LAI Equal to
12/1, 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.2 1.4 1.6 1.8 2.0 P *
Coeftlcient K,, (P, = O)
I
L2
0.05 0.97 1.66 2.10 2.43 2.72 2.92 3.08 3.24 3.48 3.73 4.22 4.85 5.36 6.00 6.58
o.! 0.83 1.21 1.57 1.95 2.14 2.33 2.46 2.60 2.76 2.91 3.28 3.61 4.03 4.43 4.85
0,3 0.78 0.90 1.09 1.27
E
P,
1.44 1.60 1.74 1,86 1.98 2.11 2.35 2.51 2.76 2.99 3.25 12
0.5 0.78 0.86 0.99 1.10 1.22 1.35 1.47 1.57 1.67 1.76 1.96 2.15 2.34 2.50 2.76
1.0 0.78 0.85 0.92 0.99 1.06 1.13 1,20 1.27 1.34 1.41 1.54 1.68 1.82 1.97 2.10 ,
Coefficient KII(PI = O)
1 L,
0.05 0.67 0,67 0.82 1.16 1.35 1.48 1.58 1.65 1,69 1.74 1.81 1.84 1.86 I.88 1.90 J
().! 0.67 0.67 0.73 0.93 1.11 1.25 1.36 1.45 1.52 1.57 I.66 1.72 1.77 1.80 1.82
0,3 0.67 0.67 0.67 0.71 0.80 0.90 0.99 1.08 1,15 1.22 1.33 1.41 1.48 1.54 1.59
0,5 0,67 0.67 0.67 0.69 0.73 0.81 0.87 0.94 1.01 1.07 1.17 1.26 1.33 1.39 1.44 +
i ,0 0.67 0.67 0.67 0.68 0.71 0.74 0.78 0.82 0.87 0.91 0.99 1.07 1.13 1.19 1.24
p, +p2
NOTE — Intermediate value maybe obtained by interpolation.
Table 39 Coefficients of Effective Lengths K1for Columns Effectively Held in Position and Restrained
Against Rotation at Bottom End and Top End Held Against Rotation but not Held in Position
(Table 36)
Coefficients KI for 12/11 Equal to
c] 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.2 1.4 1.6 1.8 2.0
P2
() 2.0 1.8 1,7 1.67 1.6 1,55 1.50 1.4 1.43 1.4 1.37 1.3 1.1 1.10 1.0 t &
05 2.0 1.9 1.8 1.74 1.6 1,65 1.61 1.5 1,55 1.5 — — — — —
F
/2 P,
I.0 2,0 2.0 2.0 2.00 2.0 2.00 — — --- — — — — — —
1.5 2.0 2.2 2.3 2.48-———— -————— —— /1 L,
2.0 2.0 2,62.9————— ———————
1
2.5 2.5 3.1 3.5—————— —-–————
3.0 3.0 3.74,1————— ——————— p, ip2
NOTE -– Intermediate values may be obtained by interpolation.
Table 40 Coefficients of Effective Lengths K1for Columns with Top Ends Free and Bottom End
Effectively Held in Position and Restrained Against Rotation
(Table 36)
Coefficients K, for lJ1, Equal to
P2
c, 0.1 0.2 M 13.6 0.8 1.0 1.2 1.4 1.6 1.8 2.o 2.5 5.o 10 20
i ;2
o 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 2.0 ‘
J
1
‘2
P,
0.5 2.0 2.14 2.24 2.36 2.47 2.57 2.67 2.76 2.85 2.94 3.02 — — — —
1,0 2.0 2.73 3.13 3.44 3.74 4.00 — — — — — — — — —
/1 L,
1,5 3.0 3.774.354.86———— ———————
2.0 4.0 4.905.67 — — — — — — — — — — — — 1
2.5 5.0 6.08 7.00 — — — — — — — — — — — —
i
3.0 6.0 7.25 — — — — — — — –- — — —- — — p, +p2
NOTE — Intermediate values maybe obtained by interpolation.
126

sl
No.
(1)
O
ii)
iii)
iv)
IS 800:2007
Table 41 Values of Kl, Kz and KB
(Clause D-3)
Degree of End
Restraint
(2)
Sketch
(3)
ffectively held in
~sition and restrained
~ainst rotation at both
Ids
ffectively held ir
osition at both end{
ird restrained agains
)tation at bottom enc
rrly
affectively held in
,osition turd restrained
,gairtst rotation al
~ttomend, and top end
eldagainst rotation bul
ot held in position
ffectively held ir
osition and restraine{
gainst rotation a
ottom end, and top em
either held agains
]tation nor agains
anslation.
+
K,
(4)
:, =K,,
{here KI I is
~ken from
‘able37
,
,, =K,,
vhere K, I is
aken from
‘able38
~, - ~,
~here K{ is
ikcn from
‘able 39 with
,,co
Kl=~
1Kz
(5)
:z=K,,
vhere KI I is
aken from
“able37
C2=K,,
vhere KI I k
aken fmm
rable 38
r? = K!
where K, is
aken from
“able 39 with
:,=0
KZ=2
K,
(6)
‘3=K[2
,here K,l is taken
“omTable 37
:3 =K, *
~hereK12is taker
rom Table38
.(3 = KI
where KI k taken
from Table39with
K, = K,
where KI is taker
from Table40 witt
r
L, ~
c,=—
L, +L, [,,
CrAbmn Parameters
<or All Cases
(7)

IS 800:2007
ANNEX E
(Clause 8.2.2.1)
ELASTIC LATERAL TORSIONAL BUCKLING
E-1 ELASTIC CRITICAL MOMENT
E-1.l General
The elastic critical moment is affected by:
a) Moment gradient in the unsupported length,
b) Boundary conditions at the lateral support
points,
c) Non-symmetric and non-prismatic nature of
the member, and
d) Location of transverse load with respect to
shear centre.
The boundary conditions at the lateral supports have
two components:
a) Torsional restraint — Where the cross-section
is prevented from rotation about the shear
centre, and
b) Warping restraint — Where the flanges are
prevented from rotating in their own plane
about an axis perpendicular to the flange.
The elastic critical moment corresponding to Iaterd
torsional buckling of a doubly symmetric prismatic
beam subjected to uniform moment in the unsupported
length and torsionally restraining lateral supports is
given by:
where
IY,I,., 1, = moment of inertia about the minor axis,
warping constant and St. Venants torsion
constant of the cross-section,
respectively;
G = modulus of rigidity; and
LLT = effective length against lateral torsional
buckling (see 8.3).
This equation in simplified form for I-section has been
presented in 8.2.2.1.
While the simplified equation is generally on the safe
side, there are many situations where this may be very
conservative. More accurate calculation of the elastic
critical moment for general case of unsymmetrical
sections, loading away from shear centre and beams
with moment gradient can be obtained from specialist
literature, by using an appropriate computer
programme or equations given below.
E-1.2 Elastic Critical Moment of a Section
Symmetrical About Minor Axis
In case of a beam which is symmetrical only about the
minor axis, and bending about major axis, the elastic
critical moment for lateral torsional buckling is given
by the general equation:
~[(
)
0,5
~+ GI, (LLT )2
X2EIY K 2 I ‘J
——
+ (c2Yg– c3Yj
‘c, = c1 (L,,) Kw 1, Y
rr2EI
)-]
-( )
C2
Yg– c3Yj
1
where
cl, c2~ C3 =
K=
KW =
Yg =
Yj =
y, =
factors depending upon the loading and
end restraint conditions (see Table 42).
effective length factors of the
unsupported length accounting for
boundary conditions at the end lateral
supports. The effective length factor K
varies from 0.5 for complete restraint
against rotation about weak axis to 1.0
for free rotate about weak axis, with 0.7
for the case of one end fixed and other
end free. It is analogous to the effective
length factors for compression members
with end rotational restraint.
warping restraint Factor. Unless special
provisions to restrain warping of the
section at the end lateral supports are
made, KW should be taken as 1.0.
y distance between the point of
application of the load and the shear
centre of the cross-section and is positive
when the load is acting towards the shear
centre from the point of application.
Y, -o.5A(z2 -y2)ydA/Iz
co-ordinate of the shear centre with
respect to centroid, positive when the
shear centre is on the compression side
of the centroid.
co-ordinates of the elemental area with
respect to centroid of the section.
can be calculated by using the following
approximation:
128

IS 800:2007
a) Plain flanges where
Yj = 0.8 (z~f- 1) hY/2.O
(when ~~> 0.5)
yj = 1.0 (z~f - 1) hy/2.O
(when ~~< 0.5)
b) Lipped flanges
Yj =0.8 (2&- 1) (1+ h~/h) hY/2
(when fl~> 0.5) I w=
Yj = (2& - 1) (1+ hL/h) hY/2
(when flf S 0.5)
where
hL =
h =
hY =
It =
=
=
height of the lip,
overall height of the
=
section, and
distance between shear
centre of the two flanges of
the crmis-section. & =
torsion constant, given by:
~biti’ /3 for open section
4A~2f~(blt) for hollow
section
Table 42 Constants cl, Czand c~
(Clause E-1.2)
A. = area enclosed by
the section, and
b, t = breadth and thiCk-
ness of the elements
of the section,
respectively.
The warping constant,
given by:
(l–~f) ~f [YhY2forI-sections
mono-symmetric about
weak axis
O for angle, Tee, narrow
rectangle section and
approximately for hollow
sections
IfC/(IfC+ If,) where lfC,lf(are
the moment of inertia of the
compression and tension
flanges, respectively, about
the minor axis of the entire
section.
Loading and Support Conditions Bending Moment Diagram Value of K Constants
~
(1) (2) (3) (4) (5) (6)
$===+’
VJ=+l
V= +314
V=+I12
-
1,0
0.7
0.5
1.0
0.7
0.5
1.0
0.7
0.5
t ,0
0.7
0.5
I ,0
0,7
0.5
1.0
0.7
0.5
1.0
0.7
0,5
1.0
0.7
0.5
1,0
0.7
0.5
1.000
1.000
I .000
1.141
1.270
1.305
1.323
1.473
1.514
1.563
I.739
1.788
1.879
2.092
2.150
2.281
2.538
2.609
2.704
3.009
3.093
2.927
3.009
3.093
2.752
3.063
3.149
—
—
—
—
—
—
—
—
I.000
1.113
1.144
0.998
1.565
2.283
0.992
1.556
2.271
0.977
1.531
2.235
0.939
1.473
2.150
0.855
1.340
1.957
0.676
1,059
1.546
0.366
0.575
0,837
0.000
0.000
0.000
129

IS 800:2007
Table 42 (Conclude@
Loading and Support Conditions Bending Moment Diagram Valne of K Constants
c 7
(1) (2) (3) (2) :) (%
*
1.0 1.132 0.459 0.525
0.5 0.972 0.304 0.980
1.0
0.5
1.0
0.5
I.0
0.5
1.285 1.562 0.753
0.712 0.652 1.070
1.365 0.553 1.780
1.070 0.432 3.050
1.565 1.257 2.640
0.938 0.715 4.800
IF
1
~F
1.0 1.046 0.430 1.120
i
L/4 L/4~L/4 1/4
Illlllly’
0.5 1.010 0.410 1.390
ANNEX F
(Clause 10.6.1)
CONNECTIONS
F-1 GENJ3RAL
The requirement for the design of splice and beam to
column connection as well as recommendation for their
design shall be as given below.
F-2 BEAM SPLICES
F-2.1 For rolled section beam splices located away
from the point of maximum moment, it may be
assumed that the flange splice carries all the moment
and the web splice carries the shear (see Fig. 30).
However in the case of a deep girder, the total moment
may be divided between the flange and the web in
accordance with the stress distribution. The web
connection should then be designed to resist its share
of moment and shear. Even web splice is designed to
carry only shear force, the moment about the centroid
of the bolt group on either side of the splice should be
designed for moment due to eccentricity.
F-2.2 Flange joints should preferably not be located at
points of maximum stress. Where splice plates are used
(see Fig. 30), their area shall not be less than 5 percent
in excess of the area of the flange element spliced; and
their centre of gravity shall coincide, as nearly as possible
with that of the element spliced. There shall be enough
fasteners on each side of the splice to develop the load
in the element spliced plus 5 percent but in no case
should the strength developed be less than 50 percent
of the effective strength of the material spliced. Wherever
possible in welded construction, flange plates shall be
joined by complete penetration butt welds. These butt
welds shall develop the full strength of the plates.
Whenever the flange width or thickness changes at the
splice location, gradual transition shall be made in the
width/thickness of the larger flange.
F-2.3 When beam splice is located at the point of
inflection of a continuous beam, the flange splicing
requirement given above may be relaxed appropriately.
F-3 COLUMN SPLICE
F-3.1 Where the ends of compression members are
faced for bearing over the whole area, they shall be
spliced to hold the connected parts aligned. The ends
of compression members faced for bearing shall
invariably be machined to ensure perfect contact of
surfaces in bearing (see Fig. 31).
F-3.2 Where such members are not faced for complete
bearing the splices shall be designed to transmit all the
forces to which the member is subjected at the splice
location.
F-3.3 Wherever possible, splices shall be proportioned
and arranged so that centroidal axis of the splice
130

IS 800:2007
, , 1 , , ,
i
r I I I I I I I I
II I
1 I I I } I I 1
1’ I
1
I
v
00
00
00
00
00
I
I L I I
I 1 I I 11,11,
I
I I I II II I 1 1
I I I
INNER SPLICE PLATE
(OPTIONAL)
I
-! -
I
/
I
.1 , - -1
I
Md

{
VM
I ?
I
I
I )
Y “
7
SPLICE PIATE
(OPTIONAL)
VEW!!RED
UNDER DESIGN
30A Conventional Splice (Typical) 306 End Plate Splice
FIG. 30 BEAM SPLICES
coincides as nearly as possible with the centroidal axes
of the members joined, in order to avoid eccentricity;
but where eccentricity is present in the joint, the
resulting stress considering eccentricity shall be
provided for.
F-3.4 If a column flange is subjected to significant
tension or if the faces are not prepared for bearing, or
if full continuity is required without slip, only HSFG
bolts shall be used.
FIG. 31 COLUMNSPLICE(TYPICAL)
F-4 BEAM-TO-COLUMN CONNECTIONS
F-4.1 Simple Connections
Simple connections are assumed to transfer only shear
at some nominal eccentricity and typically used in
frames up to about five stories in height, where strength
rather than stiffness govern the design. In such frames
separate lateral load resisting system is to be provided
in the form of bracings or shear walls. The connections
shown in Fig. 32 (A), (B), (C) and (D) can be assumed
as simple connections in framed analysis and need to
be checked only for the transfer of shear from beam to
column.
F-4.2 Rigid Connections
In high-rise and slender structures, stiffness
requirements may warrant the use of rigid connections.
Rigid connections transfer significant moments to the
columns and are assumed to undergo negligible
deformations at the joint. These are necessary in sway
frames for stability and also contribute in resisting
lateral loads. The connections shown in Fig. 32 (E),
(F), (G) can be assumed as rigid connection in frame
analysis and need to be checked for both shear and
moment transfer from beam to the column. Fully
welded connections can also be considered as rigid
beam to column connections.
F-4.3 Semi-rigid Connections
Semi-rigid connections fall between the two types
mentioned above. The fact is that simple connections
do have some degree of rotational rigidity as in the
semi-rigid connections. Similarly rigid connections do
experience some degree of joint deformation and this
can be utilised to reduce the joint design moments.
The moment-rotation relationship of the connections
have to be determined based on experiments
conducted for the specific design or based on the
relationship derived from tests, presented in specialist
Iiteroture. The simplest method of analysis will be to
idealize the connection as an equivalent rotational
spring with either a bilinear or non-linear moment-
31

IS 800:2007
-Fl-
1 I
I
I
L
(s
I
da 0
1
0
0
r I
_t ~
32A Single Web Angle
f. II
32C Top and Seat Angle with
Double Web Angle
.
I
:
:
::--1 ‘g
--1 L-tp
32E End Plate without Column Stiffeners
--l l-+
32G T-Stub
I I
32B Double Web Angle
D
t7(i
1
L
32D Top and Seat Angle without
Double Web Angie
9
: : ; :2 d
--l I--tp
32F End Plate with Column Stiffeners
t-%
m
00
00
dp
00
II I
32H Header Plate
FIG. 32 SIZE PARAMETER
FOR VARIOUS TYPES OF CONNECTION
132

—
IS 800:2007
rotation characteristics. The classification proposed
by Bjorhovde combined with the Frey-Morris model
can be used with convenience to model semi-rigid
connections, as given in the next section.
F-4.3.1 Connection Classification
Connections are classified according to their ultimate
strength or in terms of their initial elastic stiffness
and Bjorhovde’s classification. It is based on the
non-dimensional moment parameter (m’ = MU/ MP~)
and the non-dimensional rotation (01 = 0, /eP)
parameter, where f)Pis the plastic rotation. The
Bjorhovde’s classification is based on a reference
length of the beam equal to 5 times the depth of the
beam. The limits used for connection classification
are shown in Table 43 and are graphically
represented in Fig. 33.
●
F-4.3.2 Connection Models
Frye-Morris has derived the following polynomial
model for the moment curvature relationship of semi-
rigid connections:
e,= Ckums + C2UGW3+ C3OWP
where
Al = moment at the joint, in kN m;
K = standardization parameter which depend
on the connection type and geometry;
and
Cl, C2,CS = curve fitting constants
Table 44 shows the curve fitting constants
and standardization constants for Frye-
Morris Model [All size parameters in the
table are in mm (see Fig. 32)].
Table 43 Connection Classification Limits
S1No. Nature of the Connection In Terms of Strength In Terms of
Stiffness
(1) (2) (3) (4)
i) Rigid connection ml >0.7 m1~2.50[
ii) Semi-rigid connection 0.7> m’ >0.2 2.5t9’>trr’> 0.5(1’
iii) Flexibleconnection r?r~
<0.2 m’<0.50’
1.0
0.8
0,6
0.4
0.2
0
I ROTATION
-
8/= 618P 2.7
FIG. 33 CLASSIFICATION
OF CONNECTIONS ACCORDINGTOBJORHOVDE
133

IS 800:2007
Table 44 Connection Constants in Frye-Morris Model
(Clause F-4.3.2)
sl Type Connection Type Curve-Fitting Standardization Constants
No. Constants
(1) (2) (3) (4) (5)
i)
ii)
iii)
iv)
v)
vi)
vii)
viii)
A
B
c
D
E
F
G
H
Single web angle connection
Double web angle connection
Top and seat angleconnectionwith doubleweb
angle
Top and seat angle connectionwithout double
webangle
End plateconnectionwithoutcolumnstiffeners
End plateconnectionwithcolumnstiffeners
T-stubconnection
Headerplate connection
C,=l.91 x 104
Cz= 1.30X 10”
CJ=2.70 x 10’7
(2,=1.64 x 103
CZ=l.03 x 10’4
C3=8.18 x 1025
C, =2.24 x 10-’
CZ=I.86 x 104
CJ=3.23 x IOg
CI=I.63 x 103
CZ=7.25 x 10’4
C3=3.31 x 1023
CI=l.78 x 104
CZ=-9.55 x 10’s
C3=5.54 x 1029
CI ‘2.60 x 102
cj=~.37 x 10”
C3=1.31 x IO*2
c1 =4.05 x 102
cl=4.45 x 10’3
cj=–2.03 x 1023
C,=3.87
C,=2.71 x 105
C3=6.06X lo”
~ =~a-2.4tC.l.81g0.1S
~ =&4 ~C-l,81g0.1S
~ =~-!.287ta-l,128tC-0.415
/;13694@
- (3,5@35
~ =~-1.518
-0.5
~,-0.7~<
1.1
~ =~g-2,4tp.04tf
-1.5
~ =~g-
2.4
,P.
0.6
K=d-’”s tC-O’*[,
-07d<’1
where (see Fig. 32) /.= thickness of the web angle, in mm
d = depth of beam If= thickness of flange T-stub connector, in mm
d,= depth of the angle, in mm t.= thicknessof webof the beamin the connection, in mm
db= diameter of the bolt, in mm tP= thickness of end plate, header plate, in mm
dg= center-to-centre of the outermost bolt of the end plate l.= length of the angle, in mm
connection, in mm L= length oftheT-stubconnector,in mm
g = gauge distance of bolt line
I,= thickness of the top angle, in mm
NOTE — For preliminary analysis using a bilinear moment curvature relationship, the stifiess given in Table 45 may be assumed
depending on the type of connection. The values are based on the secant stiffness at a rotation of 0.01 radian and typical dimension of
connecting angle and other components as given in the table.
Table 45 Secant Stiffness
(Table 44)
s] Type of Connection Dimension Secant Stiffeners
No. mm kNm/radian
(1) (2) (3) (4)
i) Single web connection angle da=250, f,= 10, g=35 1150
ii) Double web-angle connection d,= 250, r,= 10, g= 77,5 4450
iii) Top and seat angle connection without double web da=300, t.= 10, /==] 40, db=213 2730
angle connection
iv) Header plate dp= 175, fp= 10, g=75, tw=7.5 2300
F-5 COLUMN BASES of the joint between the base plate and the foundation
F-5.1 Base Plates
shall be determined taking account of the material
properties and dimensions of both the grout and the
Columns shall be provided with base plates capable of concrete foundation.
distributing the compressive forces in the compressed
parts of the column over a bearing area such that the F-5.2 Holding Down Bolts (Anchor Bolts)
bearing pressure on the foundation does not exceed F-5.2.1 Holding down bolts shall be provided if
the design strength of the point. The design strength necessary to resist the effects of the design loads.
134

IS 800:2007
They shall be designed to resist tension due to uplift
forces and tension due to bending moments as
appropriate.
F-5.2.2 When calculating the tension forces due to
bending moments, the lever arm shall not be taken as
more than the distance between the centroid of the
bearing area on the compression side and the centroid
of the bolt group on the tension side, taking the
tolerances on the positions of the holding down bolts
into account.
F-5.2.3 Holding down bolts shall either be anchored
into the foundation by a hook or by a washer plate or
by some other appropriate load distributing member
embedded in the concrete.
F-5.2.4 If no special elements for resisting the shear
force are provided, such as block or bar shear
connectors, it shall be demonstrated that sufficient
resistance to transfer the shear force between the
column and the foundation is provided by one of the
following:
a) Frictional resistance of the joint between the
base plate and the foundation.
b) Shear resistance of the holding down bolts.
c) Shear resistance of the surrounding part of
the foundation.
d) Shear and bearing resistance of the shear key
plates welded to the base plate and embedded
in the pedestal/foundation.
ANNEX G
(Clause 17. 16)
GENERAL RECOMMENDATIONS FOR STEELWORK TENDERS AND CONTRACTS
G-1 GENERAL
G-1.l The recommendations given in this Annex are
in line with those generally adopted for steelwork
construction and are meant for general information.
G-1.2 These recommendations do not form part of the
requirements of the standard and compliance with these
is not necessary for the purpose of complying with this
standard.
G-1.3 The recommendations are unsuitable for
inclusion as a block requirement in a contract, but in
drawing up a contract the points mentioned should be
given consideration.
G-2 EXCHANGE OF INFORMATION
Before the steelwork design is commenced, the
building designer should be satisfied that the planning
of the building, its dimensions and other principal
factors meet the requirements of the building owner
and comply with regulations of all authorities
concerned. Collaboration of building designer and
steelwork designer should begin at the outset of the
project by joint consideration of the planning and of
such questions as the stanchion spacing, materials to
be used for the construction, and depth of basement.
G-3 INFORMATION REQUIRED BY THE
STEELWORK DESIGNER
G-3.1 General
a) Site plans showing in plan and elevation of
135
b)
c)
d)
e)
f)
g)
h)
j)
the proposed location and main dimensions
of the building or structure;
Ground levels, existing and proposed;
Particulars of buildings or other constructions
which may have to remain on the actual site
of the new building or structure during the
erection of the steelwork;
Particulars of adjacent buildings affecting, or
affected by, the new work;
Stipulation regarding the erection sequence
or time schedule;
Conditions affecting the position or continuity
of members;
Limits of length and weight of steel members
in transit and erection;
Drawings of the substructure, proposed or
existing, showing:
1) levels of stanchion foundations, if already
determined;
2) any details affecting the stanchion bases
or anchor bolts;
3) permissible bearing pressure on the
foundation; and
4) provisions for grouting.
NOTE— In the case of new work, the substructure
should be designed in accordance with the relevant
standards dealing with foundations and substructure.
The maximum wind velocity appropriate to
the site (see IS 875); and

IS 800:2007
k)
G-3.2
a)
b)
c)
d)
e)
f)
g)
Environmental factors, such as proximity to
sea coast, and corrosive atmosphere.
Reference to bye-laws and regulations
affecting the steelwork design and
construction.
Further Information Relating to Buildings
Plans of the floors and roof with principal
dimensions, elevations and cross-sections
showing heights between floor levels.
The occupancy of the floors and the positions
of any special loads should be given.
The building drawings, which should be fully
dimensioned, should preferably be to the scale
of 1 to 100 and should show all stairs, fire-
escapes, lifts, etc, suspended ceilings, flues
and ducts for heating and ventilating. Doors
and windows should be shown, as the
openings may be taken into account in the
computations of dead load.
Requirements should be given in respect of
any maximum depth of beams or minimum
head room.
Large-scale details should be given of any
special features affecting the steelwork.
The inclusive weight per mz of walls, floors,
roofs, suspended ceilings, stairs and
partitions, or particulars of their construction
and finish for the computation of dead load.
The plans should indicate the floors, which
are to be designed to carry partitions. Where
the layout of partitions is not known, or a
given layout is liable to alteration, these facts
should be specially noted so that allowance
may be made for partitions in any position
(see IS 875).
The superimposed loads on the floors
appropriate to the occupancy, as given in
IS 875 or as otherwise required.
Details of special loads from cranes, runways,
tips, lifts, bunkers, tanks, plant and equipment.
The grade of fire resistance appropriate to the
occupancy as may be required.
G-4 INFORMATION REQUIRED BY TENDERER
(IF NOT ALSO DESIGNER )
G-4.1 General
a) All information listed under G-3.1;
b) Climatic conditions at site-seasonat variations
of temperature, humidity, wind velocity and
direction;
c) Nature of soil. Results of the investigation of
sub-soil at site of building or structure;
d)
e)
f-)
g)
h)
j)
k)
m)
n)
P)
Accessibility of site and details of power
supply;
Whether the steelwork contractor will be
required to survey the site and set out or check
the building or structure lines, foundations and
levels;
Setting-out plan of foundations, stanchions
and levels of bases;
Cross-sections and elevations of the steel
structure, as necessary, with large-scale details
of special features;
Whether the connections are to be bolted,
riveted or welded. Particular attention should
be drawn to connections of a special nature,
such as turned bolts, high strength friction grip
bolts, long rivets and overhead welds;
Quality of steel, and pro~isions for
identification;
Requirements in respect of protective
paintings at works and on site, galvanizing or
cement wash;
Approximate dates for commencement and
completion of erection;
Details of any tests which have to be made
during the course of erection or upon
completion; and
Schedule of quantities. Where the tenderer is
required to take off quantities, a list should
be given of the principal items to be included
in the schedule.
G-4.2 Additional Information Relating to Buildings
a)
b)
c)
d)
e)
f)
Schedule of stanchions giving sizes, lengths
and typical details of brackets, joints, etc;
Plan of g,rillages showing sizes, lengths and
levels of grillage beams and particulars of any
stiffeners required;
Plans of floor beams showing sizes, lengths
and levels eccentricities and end moments.
The beam reactions and details of the type of
connection required should be shown on the
plans;
Plan of roof steelwork. For a flat roof, the plan
should give particulars similar to those of a
floor plan. Where the roof is pitched, details
should be given of trusses, portals, purlins,
bracing, etc;
The steelwork drawings should preferably be
to a scale of 1 to 100 and should give
identification marks against all members; and
Particulars of holes required for services,
pipes, machinery fixings, etc. Such holes
should preferably be drilled at works.
136

G-4.3 Information Relating to Execution of Building
Work
a)
b)
c)
d)
e)
f)
g)
h)
j)
k)
Supply of Materials;
Weight of Steelwork for Payment;
Wastage of Steel;
Insurance, Freight and Transport from Shop
to Site;
Site Facilities for Erection;
Tools and Plants;
Mode and Terms of Payment;
Schedules;
Forced Majeure (Sections and provisions for
liquidation and damages for delay in
completion); and
Escalation Sections.
G*5 DETAILING
In addition to the number of copies of the approved
drawings or details required under the contract,
dimensioned shop drawings or details should be
submitted in duplicate to the engineer who should
retain one copy and return the other to the steel supplier
or fabricators with his comments, if any.
G-6 TIME SCHEDULE
As the dates on which subsequent trades can
commence, depend on the progress of erection of the
steel framing, the time schedule for the latter should
be carefully drawn up and agreed to by the parties
concerned at a joint meeting.
G-7 PROCEDURE ON SITE
The steelwork contractor should be responsible for the
positioning and Ievelling of all steelwork. Any checking
or approval of the setting out by the general contractor
or the engineer should not relieve the steelwork
contractor of his responsibilities in this respect.
G-8 INSPECTION
References may be made to IS 7215 for general
guidance.
IS 800:2007
G-8.1 Access to Contractor’s Works
The contractor should offer facilities for the inspection
of the work at all stages.
G-8.2 Inspection of Fabrication
Unless otherwise, agreed, the inspection should be
carried out at the place of fabrication. The contractor
should be responsible for the accuracy of the work
and for any error, which may be subsequently
discovered.
G-8.3 Inspection on Site
To facilitate inspection, the contractor should during
all working hours, have a foreman or properly
accredited charge hand available on the site, together
with a complete set of contract drawings and any
further drawings and instructions which may have been
issued from time to time,
G-9 MAINTENANCE
G-9.1 General
Where steelwork is to be encased in solid concrete,
brickwork or masonry, the question of maintenance
should not arise, but where steelwork is to be housed
in hollow fire protection or is to be unprotected,
particularly where the steelwork is exposed to a
corroding agent, the question of painting or protective
treatment of the steelwork should be given careful
consideration at the construction stage, having regard
to the special circumstances of the case.
G-9.2 Connections
Where connections are exposed to a corroding agent,
they should be periodically inspected, and any corroded
part should be thoroughly cleaned and painted.
G-9.2.1 Where bolted connections are not solidly
encased and are subject to vibratory effects of
machinery or plant, they should be periodically
inspected and all bolts tightened.
137

s
ANNEX H
m
=
(Informative) ..
!S
PLASTIC PROPERTIES OF BEAMS o
4
Table 46 Plastic Properties of Beams (see also IS 808)
Designation Weight per Seetional Depth of Seetion Width of Thickness of Thickness of Radii ofGyration Section Plastic Shape Factor
Metre Area Flange Flange Web A Modulus Modulns
(D) ( b,) (t,) (tw) < (r.) (r,)’ (Zez) (%J (z,z/z=)
kg/m cmz mm mm mm mm cm cm cm’ cm’
(1) (2) (3) (4) (5) (6) (7) (8) (9) (lo) (11) (12)
LSWB 600
ISWB 600
ISMB 600
ISWB 550
ISLB 600
ISMB 550
ISWB 500
. ISLB 550
u
00 ISMB 500
ISHB 450
ISHB 450
ISLB 500
ISWB 450
ISHB 400
ISHB 400
ISMB 450
ISLB 450
ISWB 400
ISHB 350
ISHB 350
ISMB 400
ISLB 400
ISWB 350
lSHB 300
ISHB 300
ISMC 400
LSMB350
lSLB 350
lSLC 400
ISWB 300
lSHB 250
ISLB 325
*145.1
*133.7
*122.6
*112.5
*99.5
103.7
*95.2
*86.3
86.9
92.5
87.2
*75.O
79.4
82.2
77.4
●
72.4
*65.3
66.7
72.4
67.4
*61.5
*56.9
56.9
63.0
58.8
*49.4
52.4
49.5
*45.7
48.1
54.7
*43.1
184.86
170.38
156.21
143.34
126.07
132.11
121.22
109.97
110.74
117.89
111.14
95.50
10I. I5
104.66
98.66
92.27
83.14
85.01
92.21
85.91
78.40
72.43
72.50
80.25
74.85
62.93.
66.70
63.01
58.25
61.33
69.71
54.90
600
600
600
550
600
550
500
550
500
450
450
500
450
400
400
450
450
400
350
350
400
400
350
300
300
400
350
350
400
300
250
325
.-
250
250
210
250
210
190
250
190
180
250
250
180
200
250
250
150
170
200
250
250
140
165
200
250
250
100
140
165
100
200
250
165
23.6
21.3
20.8
17.6
15.5
19.3
14.7
15.0
17.2
13.7
13.7
14.1
15.4
12.7
12.7
17.4
13.4
13.0
11.6
11.6
16.0
12.5
11.4
10.6
10.6
15.3
14.2
)1.4
14.0
10.0
9.7
9.8
11.8
11.2
12
10.5
10.5
11.2
9.9
9.9
10.2
11.3
9.8
9.2
9.2
10.6
9.1
9.4
8.6
8.6
10.1
8.3
8.9
8
8.0
9.4
7.6
8.6
8.1
7.4
8.0
7.4
8.8
7.0
25.01
24.97
24.24
22.86
23.9a
22.16
20.77
21.99
20.21
18.50
18.78
20.10
18.63
16.61
16.87
18.15
18.20
16.60
14.65
14.93
16.05
16.33
14.63
12.70
12.95
15.48
14.32
14.45
I5.50
12.66
10.70
13.41
5.35
5.25
4.12
5.11
3.79
3.73
4.96
3.48
3.52
5.08
5.18
3.34
4.11
5.16
5.26
3.01
3.20
4.04
5.22
5.34
2.84
3.15
4.03
5.29
5.41
2.83
2.84
3.17
2.81
4.02
5.37
3.05
3854.2
3540.0
3060.4
2723.9
2428.9
2359.8
2091.6
1933.2
1 8Q8.7
1793.3
1742.7
1543.2
1558.1
1444.2
1404.2
1350.7
1223.8
1171.3
1131.6
1094.8
I 020.0
965.3
887.0
863.3
836.3
754.1
779.0
751.9
699.5
654.8
638.7
607.7
4341.63
3986.66
3510.63
3066.29
2798.56
2711.98
2351.35
2228.16
2074.67
2030.95
I 955.03
1773.67
1760.59
1626.36
1556.33
1533.36
1401.35
1290.19
1268.69
1213.53
1176.18
1099.45
995.49
962.18
921.68
891.03
889.57
851.11
825.02
731.21
708.43
687.76
1.1265
1.1262
1.1471
1.1257
1.1522
1.1492
1.1242
1.1526
1.147 I
1.1325
1.1218
1.1493
1.1300
1.1261
1.1155
1.1500
1.1451
1.1271
1.1212
1.1085
1.1498
1.1390
1.1223
1.1145
1.1021
1.1816
1.1421
1.1320
1.1794
1.1167
1.1092
1.1317

Table 46 (Continued)
Designistion Weight per Sectional Depth of Section Width of Thickness of Thickness of Radii of Gyration Section Plastic Shape Factor
Metre Area Flange Flange Web A Modulus Modulus
(D) ( b,) (t,) (tw) f (rZ) (r,)’ (Zez) (.%) (zpz/ Zez)
kg/m cm2 mm mm mm mm cm cm cm] cm3
(1) (2) (3) (4) (5) (6) (7) (8) (9) (lo) (11) (12)
ISHB 250
lSMC 350
lSMB 300
[SLC 350
ISLB 300
ISHB 225
ISWB 250
ISHB 225
LSMC300
ISMB 250
ISLC 300
lSLB 275
ISHB 200
lSHB 200
ISWB 225
% ISMC 250
ISMB 225
ISLB 250
ISLC 250
lSWB 200
ISMC 225
ISLC 225
ISLB 225
ISMB 200
ISHB 150
ISHB 150
ISHB 150
lSMC 200
ISLC 200
lSWB 175
lSLB 200
ISMB 175
ISMC 175
ISLC 175
lSLB 175
ISJB 225
ISJC 200
ISWB 150
51.0
*42. 1
*44.2
*38.8
*37.7
46.8
40.9
43.1
*35.8
37.3
*33.1
*33.O
40.0
37.3
33.9
*30.4
31.2
*27.9
28.0
28.8
*25.9
*24.O
*23.5
25.4
34.6
30.6
27.1
*22. 1
*20.6
22.1
*19.8
*19.3
●19.1
*17.6
*16.7
●12.8
13.9
17.0
64.96
53.66
56.26
49.47
48.08
59.66
52.05
54.94
45.64
47.55
42.11
42.02
50.94
47.54
43.24
38.67
39.72
35.53
35.65
36.71
33.01
30.53
29.92
32.33
44.08
38.98
34.48
28.21
26.22
28.11
25.27
24.62
24.38
22.40
21.30
16.28
17.8
21.67
~50
350
300
350
300
225
250
225
300
250
300
275
200
200
225
250
225
250
250
200
225
225
225
200
150
150
150
200
200
175
200
175
175
175
175
225
200
150
250
100
140
100
150
225
200
225
90
125
100
140
200
200
150
80
110
125
100
140
80
90
100
100
150
150
150
75
75
125
100
90
75
75
90
80
70
100
9.7
13.5
12.4
12.5
9.4
9.1
9.0
9.1
13.6
12.5
11.6
8.8
9.0
9.0
9.9
14.1
11.8
8.2
10.7
9.0
12.4
10.2
8.6
10.8
9.0
9.0
9.0
11.4
10.8
7.4
7.3
8.6
10.2
9.5
6.9
5.0
7.1
7.0
6.9
8.1
7.5
7.4
6.7
8.6
6.7
6.5
7.6
6.9
6.7
6.4
7.8
6.1
6.4
7,1
6.5
6.1
6.1
6.1
6.4
5.8
5.8
5.7
11.8
8.4
5.4
6.1
5.5
5.8
5.4
5.5
5.7
5.1
5.1
3.7
4.1
5.4
10.91
13.66
12.37
13.72
12.35
9.58
10.69
9.80
11.81
10.39
1I.98
11.31
8.55
8.71
9.52
9.94
9.31
10.23
10.17
8.46
9.03
9.14
9.15
8.32
6.09
6.29
6.50
8.03
8.11
7.33
8.19
7.19
7.08
7.16
7.17
8.97
8.08
6.22
5.49
2.83
2.84
2.82
2.80
4.84
4.06
4.96
2.61
2.65
2.87
2.61
4.42
4.51
3.22
2.38
2.34
2.33
2.89
2.99
2.38
2.62
1.94
2.15
3.35
3.44
3.54
2.23
2.37
2.59
2.13
1.86
2.23
2.38
1.93
1.58
2.18
2.09
618.9
571.9
573.6
532.1
488.9
487.0
475.4
469.3
424.2
410.5
403.2
392.4
372.2
360.8
348.5
305.3
305.9
297.4
295.0
262.5
239.5
226.5
222.4
223.5
218.1
205.3
194.1
181.9
172.6
172.5
169.7
145.4
139.8
131.3
125.3
116.3
116.1
111.9
678.73
672.19
651.74
622.95
554.32
542.22
527.57
515.82
496.77
465.71
466.73
443.09
414.23
397.23
389.93
356.72
348.27
338.69
338.11
293.99
277’.93
260.13
254.72
253.86
251.64
232.52
215.64
211.25
198.77
194.20
184.34
166.08
161.65
150.36
143.30
134.15
133.12
126.86
1.0967
1.1754
1.1362
i.1707
1.1338
1.1134
1.1097
1.0987
1.1711
1.1345
1.1576
1.1305
1.1129
1.1010
1.1189
1.1684
1.1385
1.1388
1.1462
1.1200
1.1605
1.1485
1.1453
1.1358
1.1538
1.1326
1.1110
1.1614
1.1516
1.1258
1.1370
1.1422
1.1563
1.1452
1.1437
1.1535
1.1465
1.1337

Table 46 (Concluded) 3
Oe
Designation Weight per Sectional
o
Depth of Section Width of Thickness of Thickness of Radii of Gyration Section Plastic o
Metre
Shape Factor ..
Area Flange Flange Web A Modulus Modulus N
(D) ( b,) (?,) (tw) f (r,)
o
(r,)’ (Zez) (%) (zpz/za) o
+
kg/m ~m2 mm mm mm mm cm cm cm’ cm]
(1) (2) (3) (4) (5) (6) (7) (8) (9) (10) (11) (12)
ISMC 150 16.4 20.88 150 75 9.0 5.4 6.11 2.21 103.9
ISMB 150 14.9 19.00 150 80 7.6 4.8 6.18 1.66 96.9
ISLC 150 14.4 18.36 150 75 7.8 4.8 6.16 2.37 93.0
ISLB 150 14.2 18.08 150 80 6.8 4.8 6.17 1.75 91.8
ISJC 175 ●11.2 14.24 175 60 6.9 3.6 7.11 1.88 82.3
ISJB 200 *9.9 12.64 200 60 5.0 3.4 7.86 1.17 78.1
ISMB 125 13.0 16.60 125 75 7.6 4.4 5.20 1.62 71.8
ISMC 125 12.7 16.19 125 65 8.1 5.0 5.07 1.92 66.6
ISLB 125 11.9 15.12 125 75 6.5 4.4 5.19 1.69 65.1
ISJC 150 9.9 12.65 150 55 6.9 3.6 6.9 1.73 62.8
ISLC 125 10.7 13.67 125 65 6.6 4.4 5.11 2.05 57.1
ISJB 175 *8.1 10.28 175 50 4.6 3.0 6.83 0.97 54.8
ISMB 100 8.9 11.4 100 50 7.0 4,2 4.00 1.05 36.6
ISJB 150 *7.1 9.01 150 50 4.6 3.0 5.98 1.01 42.9
z ISJC 125 7.9 10.07 125
0
50 6.6 3.0 5.18 1.60 43.2
ISMC 100 9.2 11.70 100 50 7.5 4.7 4.00 1.49 37.3
ISLB 100 8.0 10.21 100 50 6.4 4.0 4.06 1.12 33.6
ISLC 100 7.9 10.02 I00 50 6.4 4.0 4.06 1.57 32.9
ISJC 100 *5.8 7.41 100 45 5.1 3.0 4.09 1.42 24.8
ISMC 75 6.8 8.67 75 40 7.3 4.4 2.96 1.21 20.8
ISLB 75 6.1 7.71 75 50 5.0 3.7 3.07 1.14 19.4
ISLC 75 *5.7 7.26 75 40 6.0 3.7 3.02 1.26 17.6
NOTE — Sections having ‘weight per meter’markedwithan asterik(*)may be chosen as the section is lighter having high ZPas compared to sections below it.
119.82
110.48
106.17
104.50
94.22
90.89
81.85
77.15
73.93
72.04
65.45
64.22
41.68
49.57
49.08
43.83
38.89
38.09
28.38
24.17
22.35
20.61
1.1533
1.1401
1.1416
1.1384
1.1449
1.1639
1.1399
1.1585
1.1356
1.1472
1.1462
1.1799
1.1389
1.1556
1.1362
1.1750
1.1573
1.1576
1.1442
1.1904
1.1522
1.1710

IS 800:2007
ANNEX J
(Fioreword)
COMMITTEE COMPOSITION
Structural Engineering and Structural Sections Sectional Committee, CED 7
Organization
Indian Institute of Technology, Chennai
In personal capacity (P-244 Scheme Vi M, CIT Road,
t10. Kankurgachi, Kolkata 700054)
Bengal Engineering & Science University, Howrah
Bhillai Institute of Technology, Durg
C. R. Narayana Rae, Chennai
Central Electricity Authority, New Delhi
Cemwd Public Works Department, New Delhi
Centre for High Technology, New Delhi
Central Water Commission, New Delhi
Consulting Engineering Services India (Pvt) Ltd, New Delhi
Construma Consultancy Pvt Limited, Mumbai
Development Commissioner for Iron & Steel Control, Kolkata
Direct&ate General of Supplies & Disposals, New Delhi
Engineer-in-Chief’s Branch, New Delhi
Engineers India Limited, New Delhi
GAIL India Ltd, New Delhi
Gammon India Limited, Mumbai
Hindalco Industries Limited, Mirzapur
Hindustan Steel Works Construction Limited, Kolkata
Indian Institute of Technology, Chennai
Indian Oil Corporation, Noida
Institute of Steel Development & Growth (INSDAG), Kolkata
Institution of Engineers (India), Kolkata
Jindal V[jayaNagar Steel Limited, Bellary
Larsen & ToubroLimited, Chennai
M. N. Dastur & Company Pvt Limited, Kolkata
Metallurgical& Engg Consultants Limited, Ranchi
Ministry of Road Transport & Highways (Rep. IRC), New Delhi
141
Representative(s)
DR V. KALYANARAMAN
(Chairman)
SHRI A. BASU (Former Cfsairmarr)
DR SAIBALKUMARGHOSH
DR SUBRATA
CHACKRABORTY
(Alternate)
DR MOHANG[JFTA
DR C. N. SRINIVASAN
SHRIC. R. ARVIND(Alternafe)
SHRI KARNAILSINGH
SHRI S. K. ROY CHOWDHURY
(Alternate)
CHIEFENGINEER
SUPERINTENDING
ENGINEER
(Ahernate)
SHIU S. K. BAHAL
DIRECTOR,GATES DESIGN
SHRIA. K. BAJAI (Alternate)
SHRI S. GHOSH
SHRI S. K. HAZRA CHOWDHURY
(Ahernare)
DR HARSHAVARDHAN
SUBBARAO
SHRI B. D. GHOSH
SHRI R. N. GUIN (Alfernafe)
SHRI R. K. AGARWAL
SHRI S. K. AGARWAL(Alfernare)
SHKi J. B. SHABMA
SHRIYGGESHKUMAR SINGHAL(Alternate)
SHRIV. Y. SALPEKAR
SHRIARVINDKUMAR (Alrernate)
SHRI S. SHYAMSUNOER
SHRIV. M. DHARAP
SHRI M. V. JATKAR(Ahernate)
DR. J, MUKHOPADYAY
SHRIAIAY KUMARAGARWAL(Alternate)
SUPERINTENDING
ENGINEER
DEPUTYCHIEFENGINEER
(Alternate)
DR SATISHKUMAR
SHRI T. BANDYOPAOHYAY
SHRIP. V. RAIARAM(A[ternate)
DR T. K. BANDYOPADHYAY
SHRI P. B. VUAY
DIRECTOR
SHRI T. VENKATESH
RAO
SHRIMATI
M. F. FEBIN(Alternate)
SHRI SATYAKISEN
SHRI PRATIPBHATTACHARYA
(Alternate)
GENERALMANAGER
SHRIK. K. DE (Alternate)
SECRETARY
IRC
DIRECTOR
lRC (Alterna~e)

IS 800:2007
Represerrtacive(s)
Organization
Mumbai Port Trust, Mumbai
National Thermal Power Corporation, Noida
Northern Railway, New Delhi
Oil and Natural Gas Commission, Dehradun
Oil Industry Safety Directorate, New Delhi
Research, Designs & Standards Organization, Lucknow
Rites Ltd, Gurgaon
Steel Authority of India Limited, Ranchi
Steel Authority of India Limited, Bokaro
Steel Authority of India Limited, Bhilai
Steel Re-Rolling Mills Association of India, Kolkata
STUP Consultants Pvt Ltd, Kolkata
Structural Engineering Research Centre, Chennai
Vkakhapatnam Steel Project, Vkakhapatnam
BIS Directorate General
SUPERINTENDING
ENGINEER
EXECUTIVE
ENGINEER
(Alternate)
DR S. N. MANDAL
SHRI R. K. GUPTA(Alferrrafe)
REPRESENTATIVE
REPRESENTATIVE
SHRI S. K. NANDr
EXECUTIVE
DIRECTOR
DIRECTOR(Alternate)
SHRI SRINIVASAN
SHRI T. K. GHOSAL
SHRI R. M. CHATTOPADHYAY
(Ahernafe)
SHRI S. K. BANERJEE
SHRI SHYAMANAND TERIAR(Alrernate)
SHRI BHARATLAL
SHRI RANJANHALDAR(Alternate)
SHRI R, P. BHATIA
SHRIANIL KUMARJAVERI(Alterrrafe)
SHRI A. GHOSHAL
DR N. BANDOPADHYAY
(Alternate)
DR N. LAKSHMANAN
DR S. SEETHARAMAN (Alternate)
SHRI U. V. SWAMY
Smu S. GHOSH(Alternate)
SHRIA. K. Sma, scientist ‘F’ &Head (CED)
[Representing Director General (Ex-@7icio Member)]
SHRI S. K. Jm,scientist ‘F’& Head (Former) (CED)
[Representing Director General (Ex-ojjicio Member)]
Member Secretaries
SHRI J. ROY CHOWDHURY
Scientist ‘E’ (CED), BIS
SHRI S. CHATURVEDI
Scientist ‘E’ (CED), BIS
(Former Member Secretary)
SHRI AMAN DEEP GARG
Scientist ‘B’ (CED), BIS
(Former Member Secretary)
Use of Structural Steel in General Building Construction Subcommittee, CED 7:2
Ministry of Railways, New Delhi SHRI A. K. HARIT (Converser)
Bengal Engineering & Science University, Howrah PROFESSOR & HEAD
Bharat Heavy Electrical Limited, Trichy SHRI R. MATHtANNAL
SHRI R. JEYAKUMAR
(Alternate)
Braithwait & Company Limited, Hoogly DEPUTY MANAGER
ASSISTANT MANAGER (Akerrrure)
C. R. Narayana Rae, Chennai DR C. N. SRINIVASAN
SHRI C. R. ARVIND(Alferrrafe)
Central Electricity Authority, New Delhi StwuA. K. JAIN
SHRI PRAVEEN
VASISTH(Aherrrate)
142

Orgcarizafion
Engineer-in-Chief’s Branch, New Delhi
Engineers India Limited. New Delhi
Indian Institute of Technology, New Delhi
Indian Institute of Technology, Kanpur
Iustitute of Steel Development and Growth (INSDAG), Kolkata
Jadavpur University, Kolkata
Larsen & Toubro Limited, Chennai
M. N. Dastur Company Pvt Limited, Kolkata
Metallurgical & Engineering Consultants Limited, Ranchi
National Thermal Power Corporation, Noida
Prrblic Works Department, Mumbai
Research, Designs and Standards Organization, Lucknow
Richardson & Cruddas Limited, Nagpur
Steel Authority of India Ltd. Bokaro
Structural Engineering Research Centre, Chennai
Tata Iron & Steel Company Limited, Jamshedpur
Representative(s)
SHR! YOGESHKUMAR SINGHAL
SHRIARWND KUMAR
SHRI S. B. JAIN (Alrernare)
HEAD
DR DURGESHC. RAI
DR C. V. R. MURTHY(Alternate)
DR T. K. BAN~YOPA~HYAY
PROF K. K. GHOSH
DR. K. NATARAJAN
SHRI S. R. KULKARNI
SHRI SATYAKISEN (Alternate)
SHRJA. K. CHAKROBORTY
SHRIR. PRAMANIK (Alternate)
SHRI R. K. GUPTA
SHRI BHARATROHRA (Alternate)
SHRI K. S. JANGDE
DIRECTOR
SHIU S. K. DATT~
Sttm S. K. BANERIEE
SHRI SHYAMANAND T~RIAR (Alternate)
DR D. S. RAMCHANDRAMURTHY
SHRIG. S. PALANI(Alternafe)
SHRI S. N. GHATAK
SHRI K. S. RANGANATHAN
(Ahernafe)
Ad-hoc Group for Preparation of Final Draft for Revision of IS 800
Indian Institute of Technology, Chennai DR V. KALYANARAMAN
Institute of Steel Development & Growth (INSDAG), Kolkata DR T. K. BANDYOPADHYAY
143

Bureau of Indian Standards
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harmonious development of the activities of standardization, marking and quality certification of goods
and attending to connected matters in the country.
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without the prior permission in writing of BIS. This does not preclude the free use, in the course of
implementing the standard, of necessary details, such as symbols and sizes, type or grade designations.
Enquiries relating to copyright be addressed to the Director (Publications), BIS.
Review of Indian Standards
Amendments are issued to standards as the need arises on the basis of comments. Standards are also reviewed
periodically; a standard along with amendments is reaffirmed when such review indicates that no changes are
needed; if the review indicates that changes are needed, it is taken up for revision. Users of Indian Standards
should ascertain that they are in possession of the latest amendments or edition by referring to the latest issue of
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This Indian Standard has been developed from Doc : No. CED7(7182).
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Amend No. Date of Issue Text Affected
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