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Mechanical Properties
Mechanical Properties
• TENSILE TEST
• FATIGUE TEST
• CREEP TEST
• HARDNESS TEST
Tensile Test
INTRODUCTION
❖ This test is performed to determine
mechanical properties like strength,
ductility, resilience, toughness and
Stiffness of ductile materials.
Tensile Test
• Definition of Stress-Strain
• Testing procedure
• Elastic limit
• Yield stress
• UTS
Tensile Test
• Resilience
• Toughness
• Stiffness
• Ductility
• True Stress- Strain
Tensile Test
)
)
o
o
length(l
Orignal
length(dl)
in
Change
Strain
g
Engineerin
)
on(A
crosssecti
of
area
Orignal
load(P)
Applied
E
Stress(
g
Engineerin
)
( =
=


Definition of stress-strain
NEXT
Tensile Test
Standard Tensile Test Specimen
lo
Ao
Gauge length
Tensile Test
Jaws
Hydraulic
machine
Load Cell
Specimen
TENSILE TESTING MACHINE
Tensile Test
Testing procedure
• The original gauge length (lo) is the
permanent marks made on the
specimen before commencement of the
test.
• The specimen is gripped at the two
ends in a Tensile Testing Machine, and
pulled apart by the application of load.
Tensile Test
• The load applied on the material is
measured by a transducer called load
cell.
• And the strain is measured using a
strain gauge called extensometer.
Tensile Test
Tensile stress-strain behavior for brittle and
ductile materials loaded to fracture
Ductile
Brittle
Engg. Strain
Engg.
Stress
Tensile Test
The Different regions of a stress-strain curve
Engg. Strain
Engg.
Stress
Fracture
UTS
σY
Offset
Elastic limit
Tensile Test
DESCRIPTION OF THE CURVE
• Initially the deformation is elastic up
to yield stress, and the variation of
stress and strain is proportional.
• Beyond yield stress the deformation
is plastic but the stress keeps on
increasing up to UTS due to strain
hardening.
Tensile Test
• Beyond UTS the necking (cross section
of the material reduces) takes place,
therefore the stress required for further
deformation decreases.
NEXT
Tensile Test
ELASTIC LIMIT (EL)
• It is the highest value of stress up to
which the deformation are elastic and
beyond which they are plastic or
permanent.
Tensile Test
• It has two regions as proportional
region (obeys Hooks law) and non
proportional region.
• In practice non proportional region is
assumed to be proportional.
NEXT
Tensile Test
YIELD STRESS (OR) PROOF STRESS (y)
• Yield stress (YS) is the stress value
where plastic deformation starts.
• In certain materials like low carbon
steels and mild steels there are two
yield stress values.
• The starting point of plastic
deformation is called upper yield
stress.
Tensile Test
• The stress value corresponding to the
plastic deformation at almost constant
stress is called lower yield stress.
• The lower yield stress is almost
remains unaffected with the condition
of the steel.
• Therefore, lower stress value is taken
as the yield stress of the material.
Tensile Test
Engg. Strain
Engg.
Stress
Upper Y.S
Lower Y.S
U.T.S
Proof
Stress
Engg. Strain
Offset
Tensile Test
• In materials like copper or aluminum
the yield point is not well defined.
• Therefore, the yield stress of these
materials are given by the stress
corresponding to the plastic strain of
0.2% and it is called as 0.2% offset yield
stress.
Tensile Test
• It is determined by drawing a parallel
line to the initial linear portion of the
curve and passing through the point
0.002 on the strain axis.
NEXT
Tensile Test
UTS AND FRACTURE STRESS
• UTS( Ultimate Tensile stress) is the
highest value of the stress the material
can sustain without fracture.
• Fracture stress is the stress where the
fracture occurs (material fails).
NEXT
Tensile Test
RESILIENCE
• It is defined as the total energy
absorbed by the material during its
elastic deformation.
• It is equal to the area under the stress-
strain curve up to elastic region.
Volume
Resilience
)
(u
Resilience
of
Modulus r =
Tensile Test
Engg. Strain
Engg.
Stress Modulus of Resilience (ur)
y
Stress-strain curve shows the
modulus of resilience
Tensile Test
E
2
)
u
Resilence(
of
Modulus
E
)
strain(
engg.
Where,
2
resielence
of
Modulus
2
y
r
y
y





=

=

=
y - Yield strength
E - Elastic modulus NEXT
Tensile Test
TOUGHNESS
• It is defined as the total energy
absorbed by the material upto fracture.
• It is equal to the total area under the
stress-strain curve.
Volume
Toughness
)
(u
Toughness
of
Modulus t =
Tensile Test
Engg. Strain
Engg.
Stress
Modulus of Toughness (ut)
y
Stress-strain curve shows the
modulus of Toughness NEXT
Tensile Test
STIFFNESS
• It is the resistance of the material for
elastic deformation and it is nothing
but modulus of elasticity.
NEXT
Tensile Test
DUCTILITY
• It is the ability of the material to exhibit
large plastic deformation prior to
fracture under loading conditions.
• It is also defined as the ability of the
material to be drawn into wire.
100
)
)
)
X
o
o
f
length(l
Oringnal
length(l
Oringnal
length(l
Final
n
%Elongatio
−
=
NEXT
Tensile Test








=
+
+
+
=
=
o
i
2
2
3
1
1
2
o
o
1
i
i
l
l
ln
.....
l
l
-
l
l
l
-
l
l
l
-
l
Strain(e)
True
)
on(A
crosssecti
of
area
ous
Instantane
)
load(P
ous
Instantane
)
Stress(
True T

Definition of True stress-strain
Tensile Test
Relationship between True and Engg.
Stress-Strain
True stress(T) = E (1+)
True strain(e) = ln(1+ )
Tensile Test
FS
UTS
PS
FS
UTS
PS
True Stress-Strain
Engineering
Stress-Strain
Strain
Stress
NEXT
Fatigue Test
• INTRODUCTION
• DIFFERENT TYPES OF STRESS
• TESTING PROCEDURE
• FACTORS AFFECTING FATIGUE LIFE
• IMPROVING FATIGUE LIFE
Fatigue Test
DEFNITION
Due to cyclic loading (I.e. load
fluctuation) the material fails at a stress
level far below its static UTS. This
phenomena is called fatigue of
materials.
• The fatigue fracture is a brittle fracture.
Fatigue Test
• The fractured surface is usually normal
to the direction of the principle tensile
stress.
• Usually the progress of fracture is
indicated by a series of rings called
bench marks, progressing inward from
the point of initiation of the failure.
Fatigue Test
Typical Fatigue Fracture Surface
Origin of Crack
Fast Growth
Slow Growth
NEXT
Fatigue Test
Different Stress Cycles
There are different types of
cyclic loads as below:
a) Tension – Compression
b) Tension – Tension
c) Irregular or random
Fatigue Test
a) Tension - Compression
Cycles
max
S
min
Stress
+
- (Range)
Fatigue Test
b) Tension - Tension
max
min
+
-
Stress
Cycles
S
Fatigue Test
c) Irregular or Random stress
Cycles
+
-
Stress
Fatigue Test
• The value S = max - min is called the
range of stress.
• The stress amplitude (a) is defined as
half of the difference between the
maximum and minimum stress levels.
2
2
S min
max 



−
=
=
a
NEXT
Fatigue Test
Testing procedure
Motor
Bearing Specimen Lever
Load
Experimental setup for cantilever
fatigue test
Fatigue Test
• A cantilever type specimen is loaded at
one end through a ball bearing and is
rotated by means of a high speed
motor.
• During each revolution, the surface
layer pass through a full cycle of
tension and compression.
Fatigue Test
• The no. of cycles to cause failure will
vary with the applied stress( higher the
stress lower the cycles and vice versa).
• For materials like ferrous and its
alloys, there are stress values below
which the material doesn't fail for
infinite no. of cycles and the
corresponding stress value is called
fatigue limit or endurance limit.
Fatigue Test
• For materials like Cu, Al, etc doesn’t
have a well defined endurance limit.
• Therefore an operational endurance
limit ( usually 108 cycles) is defined for
those materials.
• Fatigue property is understood by S-N
curves.
Fatigue Test
Ferrous metal &
alloys
Non-Ferrous metal &
alloys
No. of cycles to failure(N)
Maximum
Stress(S)
Typical fatigue curves (S-N curves)
NEXT
Fatigue Test
FACTORS AFFECTING FATIGUE LIFE
1. The form of stress cycle such as
square, triangular or sinusoidal waves
has no effect on fatigue life.
2. The frequency of cyclic loading has
only a small effect.
3. The environment in which the
component undergoes stress reversal
has a marked effect on fatigue. NEXT
Fatigue Test
IMPROVING FATIGUE LIFE
1. By preventing or delaying the
initiation of crack at the surface.
2. Carbarizing and Nitriding, introduces
residual compressive stress on the
surface (this tend to cancel out the
fatigue tensile stress on areas of
stress concentration there by
increasing the fatigue life).
Fatigue Test
3. A fine grain size improves the fatigue
life.
4. Polishing of surface increases the
fatigue life by reducing stress raisers.
NEXT
Creep Test
• Introduction
• Creep curves
• Creep mechanisms
• Creep reduction & prevention
Creep Test
DEFITION
Creep is the permanent deformation
of material under a constant load as a
function of time.
• Creep is more active only above 0.4Tm,
where Tm is the melting point of the
material in Kelvin.
Creep Test
• For example, room temperature is
0.16Tm for iron, 0.22Tm for copper and
0.5Tm for lead.
• Therefore, creep is observed for lead
and not observed in iron & copper at
room temperatures.
NEXT
Creep Test
Creep Curves
• A curve which is drawn between strain
() and time (t) for a constant load is
called creep curves.
• These curves consists of three stages
like primary creep (I stage), secondary creep (II
stage) and tertiary creep (III stage)
respectively.
Creep Test
Time (t)
Strain
()
I stage
Fracture
II stage
III stage
To
T1
T2
T0 < T1 < T2
Typical Creep Curves at different temperatures
NEXT
Creep Test
Creep mechanisms
• Mechanisms activating the creep
behavior are the diffusion of vacancies
through grain boundaries, dislocation
climb and grain boundary sliding.
• In the primary stage strain rate (or
creep rate) is decreasing with time due
to more work hardening effect than the
softening effect.
Creep Test
• In the second stage the work hardening
and softening exactly balance each
other.
• In the third stage the softening effect
dominates, at this stage voids form at
grain junctions, necking occurs and
fracture takes place at the end.
NEXT
Creep Test
Prevention or reducing the creep
• The material should have high melting
point.
• Strengthening mechanisms like solute
strengthening is effective for creep
resistance.
Creep Test
• Dispersion hardening ( Insoluble
particles like Oxides are embedded in
a metal matrix)
• Strain hardening cannot be used since
recrystalization and associated
softening mechanism can occur.
NEXT
Hardness Test
• INTRODUCTION
• MOH’S HARDNESS
• BRINELL HARDNESS
• ROCKWELL HARDNESS
Hardness Test
DEFINITION
In general Hardness can be defined as
the ability of a material to resist plastic
deformation, abrasion, etc .
•Hardness is expressed using different
scales such as Moh’s, Brinell,
Rockwell, Vickers, etc.
NEXT
Moh’s hardness
❑ Moh’s hardness test measures the
hardness of the material as resistance
to scratching.
❑The scale consists of 10 standard
minerals arranged in order of
increasing hardness and each mineral
is numbered according to its position
in the series.
Moh’s hardness
1. TALC
2. GYPSUM
3. CALCITE
4. FLUORITE
5. APPETITE
6. ORTHOCLASE
7. QUARTZ
8. TOPAZ
9. CORUNDUM
10.DIAMOND
Moh’s hardness
•In this method, a scratch is tried to
obtain on the specimen surface by
these standard minerals.
•If any one mineral doesn't produce a
scratch and the other mineral next
higher in the series produces a scratch
,then the hardness of the material is
between the hardness of these two
minerals.
Moh’s hardness
•This method finds limited application in
the engineering field because a large
number of metals and alloys show
same Moh’s hardness.
•However, it is widely used in the field of
Geology for identification of minerals.
NEXT
Brinell hardness
• PRINCIPLE
• HARDNESS CALCULATION
• INDENDER SELECTION
• LOAD SELECTION
Brinell hardness
• GENERAL PRECAUTIONS
• ADVANTAGES
• DRAWBACKS
Brinell hardness
PRINCIPLE
•Brinell hardness test is the indentation
test which consists of applying a
constant load (force) usually between
500 and 3000 Kg for a specific time(10
to 30s) using a 5 or 10 mm diameter
hardened steel or tungsten carbide ball
on a flat surface of the work piece.
Brinell hardness
Force
10mm ball
Specimen
Schematic of Brinell hardness testing
PRINCIPLE
Impression
Brinell hardness
•After full application of load for the
above times, load is slowly removed
and the indenter is taken out.
•The diameter of the circular impression
is measured in millimeters using a low
power microscope.
NEXT
Brinell hardness
The Brinell hardness number(HB) is
calculated as below:
mm.
in
n
indentatio
the
of
Diameter
-
d
mm.
in
ball
the
of
Diameter
-
D
Kg.
in
applied
load
-
P
Where,
)
D
-
D
D(
2P
sq.mm
in
n
indentatio
of
Area
kg
in
applied
Load
2
2
d
BHN
−
=
=

NEXT
Brinell hardness
Indenter selection and geometry
• Hardened steel balls can be used for
testing materials up to 444HB ( 2.9mm
dia), since testing at higher hardness
may cause appreciable error due to
possible flattering and permanent
deformation of the steel ball.
• Tungsten carbide ball indenter is used
for hardness of 444 to 627HB (2.9-
2.45mm) NEXT
Brinell hardness
Load Selection
• Standard loads used are 500, 1000,
1500, 2000, 2500 and 3000 kgs.
• For softer materials like Cu and Al
alloys the 500kg load is usually used
and the 3000kg load is often used for
testing harder materials like steels and
cast irons.
Brinell hardness
• Also the test load should be chosen
such that the diameter of the
impression be in the range of 25 to 60%
of ball diameter (i.e 2.5 – 6 mm)
NEXT
Brinell hardness
General Precaution for BH testing
• The thickness of the specimen should
be at least ten times the depth of the
indentation.
• Curved test surfaces of less than
25.4mm (1”) radius should not be
tested.
Brinell hardness
• The distance from the center of the
indentation to any edge of the work
piece should be more than three times
the diameter of the indentation.
• The distance between the centers of
the adjacent indentation should be at
least three times the diameter of the
indentation.
Brinell hardness
• The surface of the work piece should
be milled, ground, or polished before
testing to get the accuracy.
NEXT
Brinell hardness
ADVANTAGES
• For materials with varying hardness
from point to point, the Brinell
hardness is better (because, the larger
sized indenter measures the average
hardness).
• BH testing is useful in measuring
hardness of cast components like cast
iron and porous powder metallurgical
components. NEXT
Brinell hardness
Drawbacks of BH testing
• The impression produced on the test
specimen is larger and this may
decrease the life of the component.
• The ball indenter is likely to deform
while testing hard materials hence
increases the diameter and lower the
hardness value.
Brinell hardness
• Thin materials cannot be tested
because of larger depth of indentation.
• For some materials (like Pb, Sn, Mg,
etc) ridging or piling up effect is
observed and for some other materials(
like austenitic stainless steels and
manganese steels) sinking effect is
observed.
Brinell hardness
• Due to this effect measured diameter of
impression will be larger than actual
and results in lesser hardness value.
Actual
d
Actual
d
Measured
d Measured
d
a) Ridging b) Sinking
NEXT
Rockwell hardness
• Test procedure
• Precautions
• Advantage
• Disadvantage
Rockwell hardness
TEST PROCEDURE
• In this method the hardness of a
material is correlated with the depth of
indentation and not with the area of
indentation as in Brinell and Vickers
tests.
• The hardness of the material is
inversely proportional to the depth of
indentation.
Rockwell hardness
Anvil
Dial
Indenter
Hand wheel
Loading Lever
Elevating Screw
Weights
Rockwell Hardness Tester
Rockwell hardness
• A dial is present in the Rockwell
hardness testing machine and it will
give the hardness of the material
directly as per the depth of indentation.
• Initially a minor load is applied and a
zero datum position is established in
the dial.
Rockwell hardness
• A major load is then applied for a
specified period and removed leaving
the minor load applied.
• Now the dial pointing towards some
number which is corresponding to the
hardness of the material.
• The entire procedure requires 5 to 10
sec.
Rockwell hardness
Surface
of
specimen
The difference
between depth due to
major and minor load
Diamond Indenter
Depth to which
indenter is forced by
major load
Depth to which
indenter is forced by
minor load
Principle of Rockwell test
NEXT
Rockwell hardness
PRECATIONS
• Measurement shouldn't be made too
close to the edge.
• Surface should be more polished than
Brinell hardness testing.
• More readings should be taken in order
to reduce error.
NEXT
Rockwell hardness
ADVANTAGES
• More flexible than Brinell (wide range of
materials can be tested by using many
combination of loads and indenters)
• Lesser time is required for test.
• Impression produced is less.
NEXT
Rockwell hardness
DISADVANTAGES
• Greater care is required in preparation
of samples.
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Mechanical properties .pdf

  • 2. Mechanical Properties • TENSILE TEST • FATIGUE TEST • CREEP TEST • HARDNESS TEST
  • 3. Tensile Test INTRODUCTION ❖ This test is performed to determine mechanical properties like strength, ductility, resilience, toughness and Stiffness of ductile materials.
  • 4. Tensile Test • Definition of Stress-Strain • Testing procedure • Elastic limit • Yield stress • UTS
  • 5. Tensile Test • Resilience • Toughness • Stiffness • Ductility • True Stress- Strain
  • 7. Tensile Test Standard Tensile Test Specimen lo Ao Gauge length
  • 9. Tensile Test Testing procedure • The original gauge length (lo) is the permanent marks made on the specimen before commencement of the test. • The specimen is gripped at the two ends in a Tensile Testing Machine, and pulled apart by the application of load.
  • 10. Tensile Test • The load applied on the material is measured by a transducer called load cell. • And the strain is measured using a strain gauge called extensometer.
  • 11. Tensile Test Tensile stress-strain behavior for brittle and ductile materials loaded to fracture Ductile Brittle Engg. Strain Engg. Stress
  • 12. Tensile Test The Different regions of a stress-strain curve Engg. Strain Engg. Stress Fracture UTS σY Offset Elastic limit
  • 13. Tensile Test DESCRIPTION OF THE CURVE • Initially the deformation is elastic up to yield stress, and the variation of stress and strain is proportional. • Beyond yield stress the deformation is plastic but the stress keeps on increasing up to UTS due to strain hardening.
  • 14. Tensile Test • Beyond UTS the necking (cross section of the material reduces) takes place, therefore the stress required for further deformation decreases. NEXT
  • 15. Tensile Test ELASTIC LIMIT (EL) • It is the highest value of stress up to which the deformation are elastic and beyond which they are plastic or permanent.
  • 16. Tensile Test • It has two regions as proportional region (obeys Hooks law) and non proportional region. • In practice non proportional region is assumed to be proportional. NEXT
  • 17. Tensile Test YIELD STRESS (OR) PROOF STRESS (y) • Yield stress (YS) is the stress value where plastic deformation starts. • In certain materials like low carbon steels and mild steels there are two yield stress values. • The starting point of plastic deformation is called upper yield stress.
  • 18. Tensile Test • The stress value corresponding to the plastic deformation at almost constant stress is called lower yield stress. • The lower yield stress is almost remains unaffected with the condition of the steel. • Therefore, lower stress value is taken as the yield stress of the material.
  • 19. Tensile Test Engg. Strain Engg. Stress Upper Y.S Lower Y.S U.T.S Proof Stress Engg. Strain Offset
  • 20. Tensile Test • In materials like copper or aluminum the yield point is not well defined. • Therefore, the yield stress of these materials are given by the stress corresponding to the plastic strain of 0.2% and it is called as 0.2% offset yield stress.
  • 21. Tensile Test • It is determined by drawing a parallel line to the initial linear portion of the curve and passing through the point 0.002 on the strain axis. NEXT
  • 22. Tensile Test UTS AND FRACTURE STRESS • UTS( Ultimate Tensile stress) is the highest value of the stress the material can sustain without fracture. • Fracture stress is the stress where the fracture occurs (material fails). NEXT
  • 23. Tensile Test RESILIENCE • It is defined as the total energy absorbed by the material during its elastic deformation. • It is equal to the area under the stress- strain curve up to elastic region. Volume Resilience ) (u Resilience of Modulus r =
  • 24. Tensile Test Engg. Strain Engg. Stress Modulus of Resilience (ur) y Stress-strain curve shows the modulus of resilience
  • 26. Tensile Test TOUGHNESS • It is defined as the total energy absorbed by the material upto fracture. • It is equal to the total area under the stress-strain curve. Volume Toughness ) (u Toughness of Modulus t =
  • 27. Tensile Test Engg. Strain Engg. Stress Modulus of Toughness (ut) y Stress-strain curve shows the modulus of Toughness NEXT
  • 28. Tensile Test STIFFNESS • It is the resistance of the material for elastic deformation and it is nothing but modulus of elasticity. NEXT
  • 29. Tensile Test DUCTILITY • It is the ability of the material to exhibit large plastic deformation prior to fracture under loading conditions. • It is also defined as the ability of the material to be drawn into wire. 100 ) ) ) X o o f length(l Oringnal length(l Oringnal length(l Final n %Elongatio − = NEXT
  • 31. Tensile Test Relationship between True and Engg. Stress-Strain True stress(T) = E (1+) True strain(e) = ln(1+ )
  • 33. Fatigue Test • INTRODUCTION • DIFFERENT TYPES OF STRESS • TESTING PROCEDURE • FACTORS AFFECTING FATIGUE LIFE • IMPROVING FATIGUE LIFE
  • 34. Fatigue Test DEFNITION Due to cyclic loading (I.e. load fluctuation) the material fails at a stress level far below its static UTS. This phenomena is called fatigue of materials. • The fatigue fracture is a brittle fracture.
  • 35. Fatigue Test • The fractured surface is usually normal to the direction of the principle tensile stress. • Usually the progress of fracture is indicated by a series of rings called bench marks, progressing inward from the point of initiation of the failure.
  • 36. Fatigue Test Typical Fatigue Fracture Surface Origin of Crack Fast Growth Slow Growth NEXT
  • 37. Fatigue Test Different Stress Cycles There are different types of cyclic loads as below: a) Tension – Compression b) Tension – Tension c) Irregular or random
  • 38. Fatigue Test a) Tension - Compression Cycles max S min Stress + - (Range)
  • 39. Fatigue Test b) Tension - Tension max min + - Stress Cycles S
  • 40. Fatigue Test c) Irregular or Random stress Cycles + - Stress
  • 41. Fatigue Test • The value S = max - min is called the range of stress. • The stress amplitude (a) is defined as half of the difference between the maximum and minimum stress levels. 2 2 S min max     − = = a NEXT
  • 42. Fatigue Test Testing procedure Motor Bearing Specimen Lever Load Experimental setup for cantilever fatigue test
  • 43. Fatigue Test • A cantilever type specimen is loaded at one end through a ball bearing and is rotated by means of a high speed motor. • During each revolution, the surface layer pass through a full cycle of tension and compression.
  • 44. Fatigue Test • The no. of cycles to cause failure will vary with the applied stress( higher the stress lower the cycles and vice versa). • For materials like ferrous and its alloys, there are stress values below which the material doesn't fail for infinite no. of cycles and the corresponding stress value is called fatigue limit or endurance limit.
  • 45. Fatigue Test • For materials like Cu, Al, etc doesn’t have a well defined endurance limit. • Therefore an operational endurance limit ( usually 108 cycles) is defined for those materials. • Fatigue property is understood by S-N curves.
  • 46. Fatigue Test Ferrous metal & alloys Non-Ferrous metal & alloys No. of cycles to failure(N) Maximum Stress(S) Typical fatigue curves (S-N curves) NEXT
  • 47. Fatigue Test FACTORS AFFECTING FATIGUE LIFE 1. The form of stress cycle such as square, triangular or sinusoidal waves has no effect on fatigue life. 2. The frequency of cyclic loading has only a small effect. 3. The environment in which the component undergoes stress reversal has a marked effect on fatigue. NEXT
  • 48. Fatigue Test IMPROVING FATIGUE LIFE 1. By preventing or delaying the initiation of crack at the surface. 2. Carbarizing and Nitriding, introduces residual compressive stress on the surface (this tend to cancel out the fatigue tensile stress on areas of stress concentration there by increasing the fatigue life).
  • 49. Fatigue Test 3. A fine grain size improves the fatigue life. 4. Polishing of surface increases the fatigue life by reducing stress raisers. NEXT
  • 50. Creep Test • Introduction • Creep curves • Creep mechanisms • Creep reduction & prevention
  • 51. Creep Test DEFITION Creep is the permanent deformation of material under a constant load as a function of time. • Creep is more active only above 0.4Tm, where Tm is the melting point of the material in Kelvin.
  • 52. Creep Test • For example, room temperature is 0.16Tm for iron, 0.22Tm for copper and 0.5Tm for lead. • Therefore, creep is observed for lead and not observed in iron & copper at room temperatures. NEXT
  • 53. Creep Test Creep Curves • A curve which is drawn between strain () and time (t) for a constant load is called creep curves. • These curves consists of three stages like primary creep (I stage), secondary creep (II stage) and tertiary creep (III stage) respectively.
  • 54. Creep Test Time (t) Strain () I stage Fracture II stage III stage To T1 T2 T0 < T1 < T2 Typical Creep Curves at different temperatures NEXT
  • 55. Creep Test Creep mechanisms • Mechanisms activating the creep behavior are the diffusion of vacancies through grain boundaries, dislocation climb and grain boundary sliding. • In the primary stage strain rate (or creep rate) is decreasing with time due to more work hardening effect than the softening effect.
  • 56. Creep Test • In the second stage the work hardening and softening exactly balance each other. • In the third stage the softening effect dominates, at this stage voids form at grain junctions, necking occurs and fracture takes place at the end. NEXT
  • 57. Creep Test Prevention or reducing the creep • The material should have high melting point. • Strengthening mechanisms like solute strengthening is effective for creep resistance.
  • 58. Creep Test • Dispersion hardening ( Insoluble particles like Oxides are embedded in a metal matrix) • Strain hardening cannot be used since recrystalization and associated softening mechanism can occur. NEXT
  • 59. Hardness Test • INTRODUCTION • MOH’S HARDNESS • BRINELL HARDNESS • ROCKWELL HARDNESS
  • 60. Hardness Test DEFINITION In general Hardness can be defined as the ability of a material to resist plastic deformation, abrasion, etc . •Hardness is expressed using different scales such as Moh’s, Brinell, Rockwell, Vickers, etc. NEXT
  • 61. Moh’s hardness ❑ Moh’s hardness test measures the hardness of the material as resistance to scratching. ❑The scale consists of 10 standard minerals arranged in order of increasing hardness and each mineral is numbered according to its position in the series.
  • 62. Moh’s hardness 1. TALC 2. GYPSUM 3. CALCITE 4. FLUORITE 5. APPETITE 6. ORTHOCLASE 7. QUARTZ 8. TOPAZ 9. CORUNDUM 10.DIAMOND
  • 63. Moh’s hardness •In this method, a scratch is tried to obtain on the specimen surface by these standard minerals. •If any one mineral doesn't produce a scratch and the other mineral next higher in the series produces a scratch ,then the hardness of the material is between the hardness of these two minerals.
  • 64. Moh’s hardness •This method finds limited application in the engineering field because a large number of metals and alloys show same Moh’s hardness. •However, it is widely used in the field of Geology for identification of minerals. NEXT
  • 65. Brinell hardness • PRINCIPLE • HARDNESS CALCULATION • INDENDER SELECTION • LOAD SELECTION
  • 66. Brinell hardness • GENERAL PRECAUTIONS • ADVANTAGES • DRAWBACKS
  • 67. Brinell hardness PRINCIPLE •Brinell hardness test is the indentation test which consists of applying a constant load (force) usually between 500 and 3000 Kg for a specific time(10 to 30s) using a 5 or 10 mm diameter hardened steel or tungsten carbide ball on a flat surface of the work piece.
  • 68. Brinell hardness Force 10mm ball Specimen Schematic of Brinell hardness testing PRINCIPLE Impression
  • 69. Brinell hardness •After full application of load for the above times, load is slowly removed and the indenter is taken out. •The diameter of the circular impression is measured in millimeters using a low power microscope. NEXT
  • 70. Brinell hardness The Brinell hardness number(HB) is calculated as below: mm. in n indentatio the of Diameter - d mm. in ball the of Diameter - D Kg. in applied load - P Where, ) D - D D( 2P sq.mm in n indentatio of Area kg in applied Load 2 2 d BHN − = =  NEXT
  • 71. Brinell hardness Indenter selection and geometry • Hardened steel balls can be used for testing materials up to 444HB ( 2.9mm dia), since testing at higher hardness may cause appreciable error due to possible flattering and permanent deformation of the steel ball. • Tungsten carbide ball indenter is used for hardness of 444 to 627HB (2.9- 2.45mm) NEXT
  • 72. Brinell hardness Load Selection • Standard loads used are 500, 1000, 1500, 2000, 2500 and 3000 kgs. • For softer materials like Cu and Al alloys the 500kg load is usually used and the 3000kg load is often used for testing harder materials like steels and cast irons.
  • 73. Brinell hardness • Also the test load should be chosen such that the diameter of the impression be in the range of 25 to 60% of ball diameter (i.e 2.5 – 6 mm) NEXT
  • 74. Brinell hardness General Precaution for BH testing • The thickness of the specimen should be at least ten times the depth of the indentation. • Curved test surfaces of less than 25.4mm (1”) radius should not be tested.
  • 75. Brinell hardness • The distance from the center of the indentation to any edge of the work piece should be more than three times the diameter of the indentation. • The distance between the centers of the adjacent indentation should be at least three times the diameter of the indentation.
  • 76. Brinell hardness • The surface of the work piece should be milled, ground, or polished before testing to get the accuracy. NEXT
  • 77. Brinell hardness ADVANTAGES • For materials with varying hardness from point to point, the Brinell hardness is better (because, the larger sized indenter measures the average hardness). • BH testing is useful in measuring hardness of cast components like cast iron and porous powder metallurgical components. NEXT
  • 78. Brinell hardness Drawbacks of BH testing • The impression produced on the test specimen is larger and this may decrease the life of the component. • The ball indenter is likely to deform while testing hard materials hence increases the diameter and lower the hardness value.
  • 79. Brinell hardness • Thin materials cannot be tested because of larger depth of indentation. • For some materials (like Pb, Sn, Mg, etc) ridging or piling up effect is observed and for some other materials( like austenitic stainless steels and manganese steels) sinking effect is observed.
  • 80. Brinell hardness • Due to this effect measured diameter of impression will be larger than actual and results in lesser hardness value. Actual d Actual d Measured d Measured d a) Ridging b) Sinking NEXT
  • 81. Rockwell hardness • Test procedure • Precautions • Advantage • Disadvantage
  • 82. Rockwell hardness TEST PROCEDURE • In this method the hardness of a material is correlated with the depth of indentation and not with the area of indentation as in Brinell and Vickers tests. • The hardness of the material is inversely proportional to the depth of indentation.
  • 83. Rockwell hardness Anvil Dial Indenter Hand wheel Loading Lever Elevating Screw Weights Rockwell Hardness Tester
  • 84. Rockwell hardness • A dial is present in the Rockwell hardness testing machine and it will give the hardness of the material directly as per the depth of indentation. • Initially a minor load is applied and a zero datum position is established in the dial.
  • 85. Rockwell hardness • A major load is then applied for a specified period and removed leaving the minor load applied. • Now the dial pointing towards some number which is corresponding to the hardness of the material. • The entire procedure requires 5 to 10 sec.
  • 86. Rockwell hardness Surface of specimen The difference between depth due to major and minor load Diamond Indenter Depth to which indenter is forced by major load Depth to which indenter is forced by minor load Principle of Rockwell test NEXT
  • 87. Rockwell hardness PRECATIONS • Measurement shouldn't be made too close to the edge. • Surface should be more polished than Brinell hardness testing. • More readings should be taken in order to reduce error. NEXT
  • 88. Rockwell hardness ADVANTAGES • More flexible than Brinell (wide range of materials can be tested by using many combination of loads and indenters) • Lesser time is required for test. • Impression produced is less. NEXT
  • 89. Rockwell hardness DISADVANTAGES • Greater care is required in preparation of samples.