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Plastic Deformation
• Most of the metal forming processes involve large
plastic deformation of the work piece.
• So it is important to understand the behavior of
common metals and alloys when they undergo
plastic deformation.
• The simplest method to understand mechanical
a uniaxial
behavior of a metal is to carry out
tension test.
• Standard method: ASTM E8M
Tensile test on a round bar
Specimens before and after testing
Engineering stress strain curve
Different stages in a tensile test
Tensile test
• The shape of the stress strain curve depends on
composition, prior history of plastic deformation,
strain rate and temperature during the test.
• Important parameters used to describe the curve
are:
• Yield strength and Ultimate tensile strength
(measures of strength)
• Percentage elongation and percentage reduction in
area (measures of ductility)
Strength
• Yield strength: Stress required produce a
small specified amount of plastic
deformation. Usually measured as stress at
0.2% off set. (i.e. e = 0.002).
• UTS: The maximum stress that a material
can withstand in a uniaxial tension test.
Given by Maximum load/Original area of
cross section.
Strength
• Al, Mg, Zn, Sn and Pb alloys
are examples of low strength
materials (UTS: 10-200
MPa).
• Steels, Ni, Ti, Mo and W
alloys are examples of high
strength materials (UTS: 200-
2000MPa).
• High YS is important for load
bearing and structural parts.
Ductility
• It is an indication of the ability of a material to
deform plastically before fracture. It determines to
what extent a material can be deformed in metal
forming processes without failure.
• Elongation in a tensile test is the total change in
gauge length with respect to initial gauge length
(expressed as %).
• % elongation = (lf-lo)/lo x 100
• If cross sectional area is measured at the location
of fracture after the test, then
• % reduction in area, r = (A0-Af)/A0 x 100
Ductility
• Total
usually
elongation is
10-60% for
most of the common
engineering
materials at RT.
• Brittle materials have
very low elongations
or zero ductility.
Comparison of different materials
Malleability
Toughness
• Toughness depends on both strength and ductility.
Strain hardening
• It is a phenomenon by which metals harden
due to deformation at room temperature
(cold working).
• Movement of dislocations is one of the
chief mechanisms by which plastic
deformation occurs.
• Grain boundaries, impurities, precipitates
act as barriers or obstacles to the movement
of dislocations. Dislocations get piled up at
the grain boundaries.
Strain Hardening
• To overcome the barriers and cause
continuous plastic flow, higher energy is
required. So the stress required to cause
further plastic flow increases.
• As a result the strength and hardness
increase with increase in strain.
Lecture 2 (1).pptx
Specific energy or ideal plastic work
(per unit volume)
Uniform and Non-uniform Elongation
Necking/instability in a tensile test
Necking or localized deformation begins at
maximum load when the increase in stress due
to decrease in cross sectional area becomes
greater than the increase in load-carrying
capacity of the metal due to strain hardening.
Necking and fracture
• True strain up to point of necking/instability is called true
uniform strain and it is equal to strain hardening exponent.
• Beyond this point, deformation outside the neck region ceases
and further deformation of the neck requires decreasing load.
• Diffuse necking may terminate in fracture but is often
followed in sheet metals by localized necking, which takes
place at an angle to the specimen axis.
Summary
Effect of temperature on flow stress
Effect of temperature on flow stress
• Above a certain temperature, strain hardening is nullified
by softening mechanisms like recovery and recrystallisation
that occur simultaneously with deformation (dynamic
recrystallization).
• Flow stress decreases with temperature and above
recrystallisation temperature, flow stress remains almost
constant as the deformation proceeds.
Superplasticity
• It is the phenomenon by which some alloys exhibit very
large elongations (more than 1000%) under controlled
conditions of tensile deformation.
• Examples are some Al based and Ti based alloys.
• Used in aerospace applications.
• Often used in combination with diffusion bonding.
Optimum conditions for
superplasticity
• Very low strain rate (10-8 to 10-5 /sec)
• Uniform and equiaxed grain structure
• Very fine grain size (less than 10 microns)
• Sufficiently high temperature
• High value of strain rate sensitivity index (m > 0.5)
Applications of SPF
Hardness
Resistance offered by a material to permanent
indentation or abrasion.
A measure of wear resistance.
Usually measured by making a small indentation
on the work piece with a harder tool (indenter).
Hardness testing
Does not have
units, expressed by a
number.
Rockwell hardness
test
Vickers
test
Brinnels
test.
hardness
hardness
Hardness
Important for:
 Cutting tools
 Abrasives for
grinding and other
finishing
operations
 Tools for casting,
forming and
shaping
 Parts subjected to
wear and abrasion.
Modification of Properties
• Alloying
• Mechanical Working
• Heat Treatment
Alloying
• The properties of metals can be improved by
alloying additions.
• Tool steel (High Speed Steel)
18%W, 4%Cr, 1% V, 0.8% C
• Stainless steel
17-19%Cr, 8-10% Ni, 2%Mn, 1%Si, 0.15% C
• As % Zn increases, strength and hardness of brass
increase. Ductility increases and then decreases.
Mechanical Working
Cold working Hot Working
Heat Treatment
Subjecting the material to a controlled cycle of
heating and cooling to obtain desired properties.
• Annealing: Reduces strength and hardness,
improves ductility and machinability.
• Normalising: Hardness and strength higher than
annealed material.
• Hardening: Done by either oil or water quenching.
Hardness and brittleness increase and toughness
reduces.
Lecture 2 (1).pptx
Surface hardening or case hardening
• Used in situations where
only alteration of surface
properties is desirable.
• Improves surface hardness
and retains the toughness of
the core.
• Gear teeth,
fasteners, clutch
bearings,
plates,
cutting tools, dies etc.
Carburising,
Nitriding,
Carbonitriding,
Cyaniding,
Boronising

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Lecture 2 (1).pptx

  • 1. Plastic Deformation • Most of the metal forming processes involve large plastic deformation of the work piece. • So it is important to understand the behavior of common metals and alloys when they undergo plastic deformation. • The simplest method to understand mechanical a uniaxial behavior of a metal is to carry out tension test. • Standard method: ASTM E8M
  • 2. Tensile test on a round bar
  • 3. Specimens before and after testing
  • 5. Different stages in a tensile test
  • 6. Tensile test • The shape of the stress strain curve depends on composition, prior history of plastic deformation, strain rate and temperature during the test. • Important parameters used to describe the curve are: • Yield strength and Ultimate tensile strength (measures of strength) • Percentage elongation and percentage reduction in area (measures of ductility)
  • 7. Strength • Yield strength: Stress required produce a small specified amount of plastic deformation. Usually measured as stress at 0.2% off set. (i.e. e = 0.002). • UTS: The maximum stress that a material can withstand in a uniaxial tension test. Given by Maximum load/Original area of cross section.
  • 8. Strength • Al, Mg, Zn, Sn and Pb alloys are examples of low strength materials (UTS: 10-200 MPa). • Steels, Ni, Ti, Mo and W alloys are examples of high strength materials (UTS: 200- 2000MPa). • High YS is important for load bearing and structural parts.
  • 9. Ductility • It is an indication of the ability of a material to deform plastically before fracture. It determines to what extent a material can be deformed in metal forming processes without failure. • Elongation in a tensile test is the total change in gauge length with respect to initial gauge length (expressed as %). • % elongation = (lf-lo)/lo x 100 • If cross sectional area is measured at the location of fracture after the test, then • % reduction in area, r = (A0-Af)/A0 x 100
  • 10. Ductility • Total usually elongation is 10-60% for most of the common engineering materials at RT. • Brittle materials have very low elongations or zero ductility.
  • 13. Toughness • Toughness depends on both strength and ductility.
  • 14. Strain hardening • It is a phenomenon by which metals harden due to deformation at room temperature (cold working). • Movement of dislocations is one of the chief mechanisms by which plastic deformation occurs. • Grain boundaries, impurities, precipitates act as barriers or obstacles to the movement of dislocations. Dislocations get piled up at the grain boundaries.
  • 15. Strain Hardening • To overcome the barriers and cause continuous plastic flow, higher energy is required. So the stress required to cause further plastic flow increases. • As a result the strength and hardness increase with increase in strain.
  • 17. Specific energy or ideal plastic work (per unit volume)
  • 19. Necking/instability in a tensile test Necking or localized deformation begins at maximum load when the increase in stress due to decrease in cross sectional area becomes greater than the increase in load-carrying capacity of the metal due to strain hardening.
  • 20. Necking and fracture • True strain up to point of necking/instability is called true uniform strain and it is equal to strain hardening exponent. • Beyond this point, deformation outside the neck region ceases and further deformation of the neck requires decreasing load. • Diffuse necking may terminate in fracture but is often followed in sheet metals by localized necking, which takes place at an angle to the specimen axis.
  • 22. Effect of temperature on flow stress
  • 23. Effect of temperature on flow stress • Above a certain temperature, strain hardening is nullified by softening mechanisms like recovery and recrystallisation that occur simultaneously with deformation (dynamic recrystallization). • Flow stress decreases with temperature and above recrystallisation temperature, flow stress remains almost constant as the deformation proceeds.
  • 24. Superplasticity • It is the phenomenon by which some alloys exhibit very large elongations (more than 1000%) under controlled conditions of tensile deformation. • Examples are some Al based and Ti based alloys. • Used in aerospace applications. • Often used in combination with diffusion bonding.
  • 25. Optimum conditions for superplasticity • Very low strain rate (10-8 to 10-5 /sec) • Uniform and equiaxed grain structure • Very fine grain size (less than 10 microns) • Sufficiently high temperature • High value of strain rate sensitivity index (m > 0.5)
  • 27. Hardness Resistance offered by a material to permanent indentation or abrasion. A measure of wear resistance. Usually measured by making a small indentation on the work piece with a harder tool (indenter).
  • 28. Hardness testing Does not have units, expressed by a number. Rockwell hardness test Vickers test Brinnels test. hardness hardness
  • 29. Hardness Important for:  Cutting tools  Abrasives for grinding and other finishing operations  Tools for casting, forming and shaping  Parts subjected to wear and abrasion.
  • 30. Modification of Properties • Alloying • Mechanical Working • Heat Treatment
  • 31. Alloying • The properties of metals can be improved by alloying additions. • Tool steel (High Speed Steel) 18%W, 4%Cr, 1% V, 0.8% C • Stainless steel 17-19%Cr, 8-10% Ni, 2%Mn, 1%Si, 0.15% C • As % Zn increases, strength and hardness of brass increase. Ductility increases and then decreases.
  • 33. Heat Treatment Subjecting the material to a controlled cycle of heating and cooling to obtain desired properties. • Annealing: Reduces strength and hardness, improves ductility and machinability. • Normalising: Hardness and strength higher than annealed material. • Hardening: Done by either oil or water quenching. Hardness and brittleness increase and toughness reduces.
  • 35. Surface hardening or case hardening • Used in situations where only alteration of surface properties is desirable. • Improves surface hardness and retains the toughness of the core. • Gear teeth, fasteners, clutch bearings, plates, cutting tools, dies etc. Carburising, Nitriding, Carbonitriding, Cyaniding, Boronising