[IJET-V1I3P7] Authors : Prateek Joshi, Mohammad UmairZaki

International Journal of Engineering and Techniques - Volume 1 Issue 3, May - June 2015
ISSN: 2395-1303 http://www.ijetjournal.org Page 29
FEM Analysis of Connecting Rod of different materials using
ANSYS
Prateek Joshi1
, Mohammad UmairZaki2
1(Department of Mechanical Engineering, Noida International University, Greater Noida, India)
2 (Faculty of Mechanical Engineering, Noida International University, Greater Noida, India)
I. INTRODUCTION
Connecting Rods are used practically generally
used in all varieties of automobile engines. Acting
as an intermediate link between the piston and the
crankshaft of an engine of an automobile. It is
responsible for transmission the up and down
motion of the piston to the crankshaft of the engine,
by converting the reciprocating motion of the piston
to the rotary motion of crankshaft. While the one
end, small end the connecting rod is connecting to
the piston of the engine by the means of piston pin,
the other end, the bigger end being connected to the
crankshaft with lower end big end bearing by
generally two bolts.
Generally connecting rods are being made
up of stainless steel and aluminium alloy through
the forging process, as this method provides high
productivity and that too with a lower production
cost. Forces generated on the connected rod are
generally by weight and combustion of fuel inside
cylinder acts upon piston and then on the
connecting rod, which results in both the bending
and axial stresses.
Therefore it order to study the strain
intensity, stress concentration and deformation in
the crank end of the connection rod, firstly based on
the working parameter and the vehicle chosen the
design parameter or dimensions of the connecting
rod is calculated, then the model of the connecting
rod parts is prepared and finally it is analysed using
Finite Element Method and results thus achieved
will provide us the required outcome of the work
done here .Also further study can also be carried
out later on for the dynamic loading working
conditions of the connecting rod and also
improvement in design can also be made for
operation condition and longer life cycle against
failure.
Pro/ENGINEER Wildfire 4.0 software is
used for modelling of the connecting rod model and
ANSYS 13 is analysis. ANSYS being an analysis
system which stands for “Advanced Numerical
System Simulation”. It is an CAE software, which
RESEARCH ARTICLE OPEN ACCESS
Abstract:
Connecting Rods are practically generally used in all varieties of automobile engines. Acting as an
intermediate link between the piston and the crankshaft of an engine. It is responsible for transmission of the up
and down motion of the piston to the crankshaft of the engine, by converting the reciprocating motion of the
piston to the rotary motion of crankshaft. Thus, this study aims to carry out for the load, strain and stress analysis
of the crank end of the connecting rod of different materials. Based on which the High Strength Carbon Fiber
connecting rod will be compared with connecting rod made up of Stainless Steel and Aluminum Alloy. The
results can be used for optimization for weight reduction and for design modification of the connecting rod. Pro-E
software is used for modeling and analyses are carried out in ANSYS software. The results archived can also help
us identify the spot or section where chances of failure are high due to stress induced. Also the results obtained
can be used to modify the existing designs so that better performance and longer life cycle can be archived.
Keywords —Connecting Rod, Pro-E, FEA, ANSYS Workbench, Crank, Crankshaft, Piston, Carbon Fiber,
Stainless Steel, Aluminum Alloy.

has many capabilities, ranging from simple static
analysis to complex non-linear, dynamic analysis,
thermal analysis, transient state analysis, etc. By
solid modeling software, the geometric shape for
the model is described, and then the ANSYS
program is used for meshing the geometry for
nodes and elements. In order to obtain the desirable
results at each and every point of the model, the
fine meshing is done which also results in accurate
results output. In this study the elements formed
after meshing are tetrahedral in shape. Loads and
boundary constrains in the ANSYS can be applied
on the surfaces and volume as required. Finally the
results calculation is done by the ANSYS software
and the desired output results can achieved.
II. FINITE ELEMENT METHOD
The finite element method (FEM) is a
numerical technique for solving problems to find
out approximate solution of a problem which are
described by the partial differential equations or can
also be formulated as functional minimization. A
principle of interest is torepresented as an assembly
of finite elements. Approximating functions in the
finite elements are determined in the terms of the
nodal values of a physical field which is sought.
FEM subdivides a whole problem or entity into
numbers of smaller simpler parts, called finite
elements, and solve these parts for the problems.
The main advantage of FEM is that it can handle
complicated boundary and geometries with very
ease.
Steps for the Finite Element Method are:-
• Modelling the Model
• Import the model
• Defining element type
• Defining material properties
• Meshing of model
• Applying boundary constrains
• Applying load
• Results and Analysing it.
III. SPECIFICATION OF THE PROBLEM
The objective of the present work is to design and
optimize a connecting rod based upon its material
properties by using connecting rod of different
materials. Here Stainless Steel, Aluminum Alloy
and High Strength Carbon fiber 280gsm
bidirectional are used to analyze the connecting rod.
The material of connecting rod will be optimized
depending upon the analysis result output. CAD
model of connecting rod will be modelled in Pro-E
and then be analyzed in ANSYS Software. After
analysis a comparison will be made between
existing material and alternate material which will
be suggested for the connecting rod in terms of
deformation, stresses and strain.and the desired
output results can achieved.
IV. OBJECTIVE
1. Designing of the analysis rod based on the
input parameters and then modeling of the
connecting rod in the Pro/ENGINEER
Wildfire 3.0 software.
2. FEM tool software ANSYS 13.0 is given
model and material input based on the
parameters obtained.
3. To determine the Von Misses stresses,
Strain Intensity, Total Deformation and to
optimize in the existing Connecting rod
design.
4. To calculate stresses in critical areas and to
identify the spots in the connecting rod
where there are more chances of failure.
5. To reduce weight of the existing connecting
rod based on the magnitude of the output of
analysis.
The main aim of the project is to determine the
Von-Misses Stresses, Strain Intensity output and
optimize the new material used for connecting rod.
Based on which the new material can be compared
with the existing materials used for Connecting Rod.
V. PRESSURE CALCULATION FOR CONNECTING
ROD
Engine type air cooled 4-stroke
Bore x Stroke = 57.0 x 58.6 mm
Displacement = 149.5 cc

Maximum Power = 13.8bhp@8500rpm
Maximum Torque = 13.4Nm@6500rpm
Compression Ratio = 9.35: 1
Density of petrol
=737.22kg/m3=737.22E-9 kg/mm3
Flash point for petrol (Gasoline)
Flash point = -43°c (-45°F)
Auto ignition temp. = 280°c (536°F) = 553°k
Mass = Density x volume
= 737.22E-9 x 19.5E3
= 0.110214kg
Molecular weight of petrol = 114.228g/mole
= 0.11423 kg/mole
From gas equation,
PV=m * Rspecific * T
Where, P = Pressure, MPa
V = Volume
m = Mass, kg
Rspecific = Specific gas constant
T = Temperature, °k
Rspecific = R/M
Rspecific = 8.3143/0.114228
Rspecific = 72.76 Nm/kg K
P = m.Rspecific.T/V
P = (0.110214 x 72.757 x 553) / 149.5
= 29.67 MPa
Calculation of analysis is done for maximum
Pressure of 30 MPA and 15 MPA.
VI. DESIGN CALCULATION FOR THE
CONNECTING ROD
In general,
Figure 1: I Section Standard Dimensions of connecting rod
From standards,
• Thickness of the flange & web of the
section = t
• Width of the section, B = 4t
• Height of the section, H = 5t
• Area of the section, A = 11t2
• Moment of inertia about x-axis,Ixx=
34.91
• Moment of inertia about y-axis Iyy=
10.91
• Therefore Ixx/Iyy = 3.2
Length of the connecting rod (L) = 2 times stroke
L = 117.2 mm
Total Force acting F = -
Where = force acting on the piston
= force of inertia
=

4
×
= 39473.1543 N
=
1000
× ±
2
"#
wr = weight of the reciprocating parts
wr = 1.6 * 9.81 = 15.696 N
r = crank radius
r = stroke of piston / 2
r = 58.6/2 = 29.3
Also, = Crank angle from dead center
= 0 considering connecting rod is at TDC position
"#
= length of connecting rod / crank radius

"#
= 117.2/29.3 = 4
g = acceleration due to gravity, 9.81
v = crank velocity m/s
w = 2 "/60
w = 2 8500/60 = 890.1179
v = rw = 29.3e-3*890.1179 = 26.08
On substituting these,
= 9285.5481
Thus,
F = 39473.1543 – 9285.5481
F = 30187.6062 N
Now, According to Rankine’s – Gordon formula,
=
$ A
1 + (
(
)**
)
Let,
A = Cross-section area of connecting rod,
L = Length of the connecting rod
$ = Compressive yield stress,
F = Buckling load
Ixx&Iyy = Radius of gyration of sectionabout the x
– x and y – y axis resp.
Kxx&Kyy = Radius of gyration of section about x –
x and y – y axis resp.
For Stainless Steel
On substituting these to Rankine’s formula
30187.6 =
170 ∗ 11
1 + 0.002(
2.
.2 3
)
Thus by solving we get,
= 4.7321
Therefore
Width B = 4t = 18.9284 mm
Height H = 5t = 23.6605 mm
Area A = 11t = 246.32 mm2
Height at the piston end = 0.75H – 0.9 H
= 0.75*23.66 = 17.745mm
Height at the crank end = 1.1H – 1.25H
= 1.1*23.66 = 26.026 mm
Length of the connecting rod (L) = 117.2 mm
Figure 2: Connecting Rod General Dimensions
Design of small end:
Load on the piston pin or the small end bearing ( )
= Projected area * Bearing pressure
= dplp * 456
= 39473.154 N load on the piston pin,
= Inner dia. of the small end
456= Bearing pressure
= 10.0 for oil engines.
= 12.7 for automotive engines.
We assume it is a 150cc engine, thus
456 = 10 MPa
7 = length of the piston pin
= 1.5
Substituting,
39473.154 = 1.5 . x 10
= 51.29 ≅ 51 mm
7 = 1.5 = 76.5 mm
Outer diameter of small end = +2 5+2 9
= 51 + [2×2] + [2×5]
= 65mm
Where,
Thickness of bush ( 5) = 3 to 5 mm
Marginal thickness ( 9) = 5 to 10 mm
Design of Big end:
Load on crankpin or the big end bearing ( ) =
Projected Area * Bearing pressure

= dplp * 456
= 39473.154 N force or load on piston pin
$ = Inner dia. of big end
7$ = length of crankpin
= 1.25 $
45$ = 7.5 MPa
Putting these,
39473.154 = 1.25 $ . $7.5
$ = 64.88 ≅ 65 mm
7$ = 1.5 = 97.5 mm
Outer diameter of the big end =
$+2 5+2 9+2 5
= 65 + [2×2] + [2×5] + [2×4]
= 87mm
Where,
Thickness of bush ( 5) = 3 - 5 mm
Marginal thickness ( 9) = 5 - 10 mm
Marginal thickness for bolt ( 5) = 3 - 6 mm
Design of Big end Bolts:
Force on bolts =
:
( $5) × ;3 × "5
$5 = Core dia. of bolts
;3 = Allowable tensile stress for material of the
bolts
= 12 MPa assume
"5 = Number of bolts(2 bolts are used)
=
:
( $5) × 12 × 2
= 18.85 ( $5)
Also,
The bolts and the big end cap are subjected to the
tensile forces which correspond to inertia forces on
the reciprocating parts at the TDC while on the
exhaust stroke.
We know that inertia force on the reciprocating
parts
=
1000
× ±
2
"#
As calculated above,
F = 9285.5481 N
Equating Inertia force, to force on bolts,
Table 1: Dimensional Specifications of the connecting rod
9285.5481 = 18.85 ( $5)
$5 = 22.19
Normal diameter of bolts ( $5)
$5 =
<=>
?.
= 27.28 mm
≅ 30 @@
Hence we will use M30 sized bolts.
The materials chosen for analysis of the connecting
rod here are Stainless Steel, Aluminum 7075 and
High Strength Carbon fiber. These materials where
tested using ANSYS software for the stress and
strain and other forces acting on the connecting rod
based on these material properties as shown in the
table 2, below
S.no. Parameters (mm)
1
Thickness of the connecting rod (t) = 4.7
2 Width of the section (B = 4t) = 18.92
3 Height of the section(H = 5t) = 23.66
4 Height at the big end = (1.1 to 1.125)H =
26.02
5 Height at the small end = 0.9H to 0.75H=
17.74
6 Inner diameter of the small end = 51
7 Outer diameter of the small end = 65
8 Inner diameter of the big end = 65
9 Outer diameter of the big end = 87

Material
Selected
Stainless
Steel
Aluminum
Alloy 7075
High
Strength
Carbon
Fiber
Young’s
Modulus,
E
2.0*10^5
MPa
71.7 GPa 100 GPa
Poisson’s
ratio
0.30 0.33 0.10
Density 7850
kg/m^3
2700
kg/m^3
1600
kg/m^3
Shear
Modulus
29.6 GPa 26.9 GPa 0.6 Msi
Tensile
Strength,
Ultimate
460 MPa 572 MPa 75.85
N/mm^2
Shear
Strength
250 MPa 331 MPa 600 MPa
Table 2: Material Properties Used for Analysis
VII. MODELING OF THE CONNECTING ROD
USING PRO-E
Pro-Eis used to create a complete 3D digital
model of manufactured goods. The models consist
of 2D and 3D solid model data which can also be
used downstream in finite element analysis, rapid
prototyping, tooling design, and CNC
manufacturing.
Connecting rod of a Light Vehicle Engine
easily available in the market is selected and its
dimensions are calculated based on the design and
working parameters. According the dimensions
obtained the model of the connecting rod is
developed in the Pro/ENGINEER Wildfire 4.0.
Model of the connecting rod and its Big end
Bearing Lower half the separately developed of this
study as shown in figures below,
Figure 3: Model of connecting rod in Pro-E
Figure 4: Model of Crank end Bearing Lower half
VIII. FINITE ELEMENT ANALYSIS USING ANSYS
The analysis of connecting rod models are carried
out using ANSYS software using Finite Element
Method. Firstly the model files prepared in the Pro-
E, then are exported to ANSYS software as an
IGES files as shown in figure 5 & 6 below;

Figure 5: Imported model of Connecting Rod to
ANSYS
Figure 6: Imported model of the Lower Bearing of
Connecting Rod to ANSYS
After this areas and sections are segmented as
importing the model to ANSYS results in some
imperfection. Thus the geometry clean-up is done.
Now the material properties are defined on the
model for the material used as shown in table above.
After that, the meshing of model is to be done. Here
a model is divided into a number of elements and
nodes. The meshed models of the connecting rod
are as shown in figure 7 & 8 below,
Figure 7: Meshed model of connecting rod on
ANSYS
Figure 8: Meshed Model of the Lower Bearing of
Connecting Rod in ANSYS
Once meshing is done the boundary conditions i.e...
DOF constrains, forces, loads are to be applied on
the model. As shown fig 9, the pressure is applied
on the Crank end bearing of the connecting rod,
while keeping piston end fixed. The pressure of 15
& 30 Mpa is used.

Figure 9: Load constrained section of connecting rod.
Now the Lower half Crank end bearing is taken and
boundary constrained and loads are applied on it.
As shown in fig 10, the pressure is applied on the
bearing face of the model, while keeping bolt area
fixed. The pressure of 15 & 30Mpa is used.
Figure 10: Load constrained section of Lower Crank
end Bearing.
IX. RESULTS OUTPUT OF ANALYSIS:
The static analysis of connecting rod models was
conducted for different materials to identify the
fatigue locations on it. The tern “static” implies that
the forces do not change with time. Results of the
static analysis output are shown via stress, strain
and deformation under the applied load. The output
results of static analysis of both the components are
shown in fig below;
Results obtained by ANSYS for the crank end
bearing lower half and the connecting rod for
stainless steel at the applied pressure of 15mpa.
Figure 11: Displacement Output of the Lower
Bearing of Stainless Steel Connecting Rod in ANSYS
Figure 12: Displacement Output of the Connecting
Rod in ANSYS
From the fig 11 the maximum displacement occurs
in the Lower Bearing of connecting rod is 0.019415
mm. From the fig 12 the maximum displacement
occurs in the connecting rod is 0.012095 mm.

Figure 13: Von-Misses Stress Output of the Lower
Figure 14: Von-Misses Stress Output of the Stainless
Steel Connecting Rod in ANSYS
From the fig 13 the maximum Von-Misses Stress
occurs in the Lower Bearing of connecting rod is
0.140E+09 MPa. From the fig 14 the maximum
Von-Misses Stress occurs in the connecting rod is
0.113E+09 MPa.
Figure 15: Total Stain Intensity Output of the Lower
Figure 16: Total Stain Intensity Output of the
Stainless Steel Connecting Rod in ANSYS
From the fig 15 the maximum Strain occurs in the
Lower Bearing of connecting rod is 0.960E-03.
connecting rod is 0.796E-03.

aluminium alloy at the applied pressure of 15mpa.
Figure 17: Displacement Output of the Aluminium
Alloy Connecting Rod in ANSYS
Bearing of Aluminium Alloy Connecting Rod in ANSYS
Figure 19: Von-Misses Stress Output of the
Aluminium Alloy Connecting Rod in ANSYS
Bearing of Aluminium Alloy Connecting Rod in ANSYS
0.115E+09 MPa.

Aluminum Alloy Connecting Rod in ANSYS
Bearing of Aluminum Alloy Connecting Rod in ANSYS
Lower Bearing of connecting rod is 0.003099. From
the fig 21 the maximum Strain occurs in the
connecting rod is 0.002319.
bearing lower half and the connecting rod for high
strength carbon fiber at the applied pressure of
15mpa.
Figure 23: Displacement Output of the High Strength
Carbon fiber Connecting Rod in ANSYS
Bearing of High Strength Carbon fiber Connecting Rod in
ANSYS

Figure 25: Von-Misses Stress Output of the High
Strength Carbon fiber Connecting Rod in ANSYS
ANSYS
0.121E+09 MPa.
Figure 27: Total Stain Intensity Output of the High
ANSYS

stainless steel at the applied pressure of 30mpa.
Figure 30: Displacement Output of the Stainless
Figure 32: Von-Misses Stress Output of the Stainless
0.229E+09 MPa.

Stainless Steel Connecting Rod in ANSYS
aluminium alloy at the applied pressure of 30mpa.
Figure 35: Displacement Output of Lower Bearing of
the Aluminium Alloy Connecting Rod in ANSYS
Figure 36: Displacement Output of the Aluminium
Alloy Connecting Rod in ANSYS

Figure 37: Von-Misses Stress Output of Lower
Bearing of the Aluminum Alloy Connecting Rod in ANSYS
Figure 38: Von-Misses Stress Output of the
0.229E+09 MPa.
Figure 39: Total Stain Intensity Output of Lower
Bearing of the Aluminum Alloy Connecting Rod in ANSYS

bearing lower half and the connecting rod for high
strength carbon fiber at the applied pressure of
30mpa.
Figure 41: Displacement Output of Lower Bearing of
the High Strength Carbon fiber Connecting Rod in ANSYS
Figure 42: Displacement Output of the High Strength
Carbon fiber Connecting Rod in ANSYS
0.243E+09 MPa.

Figure 45: Total Stain Intensity Output of Lower
Bearing of the High Strength Carbon fiber Connecting Rod
in ANSYS
Figure 46: Total Stain Intensity Output of the High
Based on the results obtained by the ANSYS
software for the displacement, Von-Misses Stress
and Strain Intensity at the pressure of 15 MPa and
30 MPa the valves for the output obtained can be
represented as shown in the tables below.
Table 3: Analysis data for Crank End Bearing lower half at
15MPa
Table 4: Analysis data for Connecting Rod at 15MPa
For 15Mpa
Pressure
Stainless
Steel
Aluminum
Alloy 7075
High
Strength
Carbon
Fiber
Displacement 0.019415 0.054893 0.036934
Von-Misses
Stress
0.149E+09 0.156E+09 0.142E+09
Total strain
intensity
0.969E-03 0.003099 0.00159
For 15Mpa
Pressure
Stainless
Steel
Aluminu
m Alloy
7075
High
Strength
Carbon
Fiber
Displacemen
t
0.012095 0.03481 0.023777
Von-Misses
Stress
0.113E+0
9
0.115E+0
9
0.121E+0
9
Total strain
intensity
0.796E-03 0.002319 0.001381

Table 5: Analysis data for Crank End Bearing lower half at
30MPa.
Table 6: Analysis data for Connecting Rod at 30MPa
For comparisons of the results obtained the
cumulative graph can be made for both Crank End
Bearing Lower half & Connecting Rod for
Displacement, Von-Misses Stress and Strain
Intensity respectively can as shown below.
BE- Crank End Bearing Lower half Cr-
Connecting Rod
Graph 1: Displacement Output data for Bearing Lower half
and Connecting Rod.
Graph 2: Von-Misses Stress Output data for Crank End
Bearing Lower half and Connecting Rod
0
0.02
0.04
0.06
0.08
0.1
0.12
Stainless Steel
Aluminum Alloy
7075
High Strength
Carbon Fiber
0.00E+00
5.00E+07
1.00E+08
1.50E+08
2.00E+08
2.50E+08
3.00E+08
3.50E+08
AxisTitle
Axis Title
Chart Title
Stainless Steel
Aluminum Alloy
7075
High Strength
Carbon Fiber
For 30Mpa
Pressure
Stainless
Steel
Aluminum
Alloy
7075
High
Strength
Carbon
Fiber
Displaceme
nt
0.038749 0.108868 0.07386
8
Von-Misses
Stress
0.302E+0
9
0.311E+0
9
0.283E
+09
Total strain
intensity
0.002071 0.006146 0.00318
For 30Mpa
Pressure
Stainless
Steel
Aluminu
m Alloy
7075
High
Strength
Carbon
Fiber
Displacemen
t
0.024635 0.069038 0.047555
Von-Misses
Stress
0.229E+0
9
0.229E+0
9
0.243E+0
9
Total strain
intensity
0.001605 0.004598 0.002761

Graph 3: Strain Intensity Output data for Crank End Bearing
Lower half and Connecting Rod
X. CONCLUSIONS
The forces were applied on the piston head and the
effect of it on the connecting rod was studied in this
analysis. The pressure developed in the big
end/crank end of the connecting rod is analysed in
two different parts i.e... Crank end Bearing Lower
half and connecting rod for displacement, von-
misses stress and strain intensity output. The results
or conclusion thus that can made on the bases of the
output results by ANSYS can be as followed:
• It is observed that displacement, Stress and
Strain Intensity induced in the Connecting
Rod made up of Carbon fiber is
comparatively slightly greater than as
compare to the Connecting Rod made up of
Stainless Steel, thus more advancement in
the field of Carbon Fiber is required to be as
equivalent and efficiently used as Stainless
Steel.
• Also it was observed that Connecting Rod
made up of Aluminium Alloy has higher
intensity of Stress and Strain induced as
compare to Connecting Rod made up of
Carbon Fiber, thus Carbon Fiber can be a
good replacement of Aluminium Alloy.
• It was observed that Von-misses Stress
Intensity in the both the component Crank
end Bearing Lower Half and the Connecting
Rod for carbon fiber is lesser as compare to
the that of Stainless Steel and Aluminium
Alloy. Also manufacturing of complex
shape and curved surfaces from Carbon
Fiber is much easier and convenient than
that of other materials used here.
• Though the intensity of displacement in
Carbon fiber is much greater than that of
Stainless Steel, but this can in minimize by
adding more layers of carbon fiber during
manufacturing process as it will increase the
overall strength of component that too at
much lesser increase in overall weight.
• It can observed from the displacement, Von-
misses stress and Strain Intensity Output
obtained that the hot spot or the areas where
the stresses and strain intensity in higher can
be minimize by adding material i.e.…
increasing the thickness of that area and also
the areas where the stress and strain
intensity in less, the materials can be
removed from that spot or area in order to
decrease the weight of the component.
• The composite material like carbon fiber has
good strength and also being lighter than
both Stainless steel and Aluminium Alloy
7075 can be used for connecting rod with
the more easily in the near future.
• Also lighter weight of connecting rod (made
up of High Strength Carbon fiber) can also
help in reducing weight of engine block of
the automobile, thus increasing fuel
economy and thus also decreasing the
emission from the automobile.
• Thought the stresses and strain intensity
induced in the Connecting Rod made up
Carbon Fiber is more than that induced in
the Stainless Steel, but with the
advancement in technology in the field of
carbon fiber more higher Strength Carbon
Fiber will be there in the near future for
automobile industry.
• Thought the cost factor and time factor in
the manufacturing of components by Carbon
0.00E+00
1.00E-03
2.00E-03
3.00E-03
4.00E-03
5.00E-03
6.00E-03
7.00E-03
BETotalstrain…
BETotalstrain…
CRTotalstrain…
CRTotalstrain…
AxisTitle
Axis Title
Chart Title
Stainless Steel
Aluminum Alloy
7075
High Strength
Carbon Fiber

Fiber in more at present time as compare to
manufacturing by Stainless Steel and
Aluminium Alloy, but mass production will
greatly reduce the cost incurred and also
time occurred will also reduce with the
advancement in technology.
Hence at last in can be concluded that Carbon
Fiber are the future material that can be used for the
manufacturing of Connecting Rod, for being lighter
and comparable strength with that of Stainless Steel
and Aluminium Alloy.
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1. Pro/ENGINEER Wildfire 4.0 manual.
2. ANSYS WORKBENCH 13 manual.
3. G.M Sayeed Ahmed, SirajuddinElyasKhany , Syed
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ANALYSIS OF A CONNECTING ROD WITH
ALUMINUM ALLOYS AND CARBON
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Vol. 3, Issue 10, October 2014.
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Mahesh M.Patil “FINITE ELEMENT ANALYSIS OF
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Cochin, India, ISBN: 978-93-84209-88-9.
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6. Kuldeep B, Arun L.R, Mohammed Faheem “ANALYSIS
AND OPTIMIZATION OF CONNECTING ROD USING
ALFASiC COMPOSITES”, ISSN: 2319-875, International
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and Technology, Vol. 2, Issue 6, June 2013.
7. Priyank D. Toliya, Ravi C. Trivedi, Prof. Nikhil J. Chotai
“DESIGN AND FINITE ELEMENT ANALYSIS OF
ALUMINIUM-6351 CONNECTING ROD” Volume/Issue:
Vol.2 - Issue 5 (May - 2013), e-ISSN: 2278-0181.
8. Prof. Vivek C. Pathade , Dr. Dilip S. Ingole “STRESS
ANALYSIS OF I.C.ENGINE CONNECTING ROD BY
FEM AND PHOTOELASTICITY” IOSR Journal of
Mechanical and Civil Engineering (IOSR-JMCE) e-ISSN:
2278-1684 Volume 6, Issue 1 (Mar. - Apr. 2013), PP 117-
125.
9. Aniket B. Phatangare, Prof. M.S. Mhaske, Prof.
S.B.Belkar, SwapnilKulkarni “USING FINITE ELEMENT
ANALYSIS FOR DETERMINING FATIGUE LIFE OF
CONNECTING ROD AS USED IN A MOTOR-BIKE”
International Journal of Advanced Engineering Research
and Studies E-ISSN: 2249–8974.
10. P S Shenoy and A Fatemi, “DYNAMIC ANALYSIS OF
LAODS AND STRESSES IN CONNECTING”,
Proc.IMechE Vol. 220 Part C: J. Mechanical Engineering
Science.
11. Ram Bansal “DYNAMIC SIMULATION OF A
CONNECTING ROD MADE OF ALUMINIUM ALLOY
USING FINITE ELEMENT ANALYSIS APPROACH”
IOSR Journal of Mechanical and Civil Engineering
(IOSR-JMCE) e-ISSN: 2278-1684 Volume 5, Issue 2 (Jan.
- Feb. 2013), PP 01-05.
12. AbhinavGautam, K PriyaAjit “STATIC STRESS
ANALYSIS OF CONNECTING ROD USING FINITE
ELEMENT APPROACH” IOSR Journal of Mechanical
and Civil Engineering (IOSR-JMCE) e-ISSN: 2278-
1684,p-ISSN: 2320-334X, Volume 10, Issue 1 (Nov. - Dec.
2013), PP 47-51.
13. S. Shaari, M.M. Rahman, M.M. Noor, K. Kadirgama and
A.K. Amirruddin “DESIGN OF CONNECTING ROD OF
INTERNAL COMBUSTION ENGINE: ATOPOLOGY
OPTIMIZATION APPROACHM” National Conference in
Mechanical Engineering Research and Postgraduate
Studies (2nd NCMER 2010)3-4 December 2010, pp.155-
166.
14. Bhuptani K. M“STRUCTURAL ANALYSIS OF BUSH
BEARING FOR SMALL END CONNECTING ROD
USING “PROMECHANICA” ISSN 0975 – 668X| NOV 12
TO OCT 13 | VOLUME – 02. 2344-02.

[IJET-V1I3P7] Authors : Prateek Joshi, Mohammad UmairZaki

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[IJET-V1I3P7] Authors : Prateek Joshi, Mohammad UmairZaki