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T e n s i l e T e s t i n g a n d C o m p r e s s i v e T e s t i n g M e t h o d s
B Y : K A N U P R I Y A J H A N J I
A S S T . P R O F E S S O R
S C H O O L O F A E R O N A U T I C A L S C I E N C E S
H I N D U S T A N U N I V E R S I T Y
k a n u p r i y a j @ h i n d u s t a n u n i v . a c . i n
AIRCRAFT MATERIALS
UNIT-1
LECTURE2
INSTRUCTIONAL OBJECTIVES
• By the end of lecture, the students will learn the working principle of
ultimate testing machine and procedure of performing the tensile
and compressive tests.
• Students will also have knowledge about the various impact tests.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
CONTENTS
• Tensile testing
• Equipment for testing
• Process of testing
• Components of Universal Testing Machine
• Use of UTM
• Compressive strength
• Compressive test
• Charpy impact test
• Izod impact test
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
TENSILE TESTING
• Tensile testing, also known as tension
testing, is a fundamental materials
science test in which a sample is
subjected to a controlled tension until
failure.
• The results from the test are commonly
used to select a material for an
application, for quality control, and to
predict how a material will react under
other types of forces.
• Properties that are directly measured via
a tensile test are ultimate tensile
strength, maximum elongation and
reduction in area.
• The test specimen is shown in the figure.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
TENSILE TESTING
• From these measurements the following properties can also be
determined: Young's modulus, Poisson's ratio, yield strength,
and strain-hardening characteristics.
• Uniaxial tensile testing is the most commonly used for obtaining the
mechanical characteristics of isotropic materials.
• For anisotropic materials, such as composite materials and
textiles, biaxial tensile testing is required.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
EQUIPMENT
• The most common testing machine
used in tensile testing is
the universal testing machine.
• This type of machine has
two crossheads; one is adjusted for
the length of the specimen and the
other is driven to apply tension to
the test specimen.
• There are two types: hydraulic
powered
and electromagnetically powered
machines
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
PROCESS
• The test process involves placing the test specimen in the testing machine and slowly
extending it until it fractures.
• During this process, the elongation of the gauge section is recorded against the applied
force.
• The data is manipulated so that it is not specific to the geometry of the test sample.
• The elongation measurement is used to calculate the engineering strain, ε, using the
following equation:[
• where ΔL is the change in gauge length, L0 is the initial gauge length, and L is the final
length.
• The force measurement is used to calculate the engineering stress, σ, using the following
equation:
• where F is the tensile force and A is the nominal cross-section of the specimen. The
machine does these calculations as the force increases, so that the data points can be
graphed into a stress–strain curve.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
COMPONENTS OF UNIVERSAL TESTING
MACHINE
• Load frame - Usually consisting of two
strong supports for the machine. Some
small machines have a single support.
• Load cell - A force transducer or other
means of measuring the load is required.
Periodic calibration is usually required by
governing regulations or quality system.
• Cross head - A movable cross head
(crosshead) is controlled to move up or
down. Usually this is at a constant speed:
sometimes called a constant rate of
extension (CRE) machine.
• Some machines can program the
crosshead speed or conduct cyclical
testing, testing at constant force, testing at
constant deformation, etc.
Electromechanical, servo-hydraulic, linear
drive, and resonance drive are used.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
COMPONENTS OF UNIVERSAL TESTING
MACHINE
• Means of measuring extension or
deformation - Many tests require a measure
of the response of the test specimen to the
movement of the cross head.
• Extensometers are sometimes used.
• Output device - A means of providing the
test result is needed. Some older machines
have dial or digital displays and chart
recorders.
• Many newer machines have a computer
interface for analysis and printing.
• Conditioning - Many tests require controlled
conditioning (temperature, humidity,
pressure, etc.). The machine can be in a
controlled room or a special environmental
chamber can be placed around the test
specimen for the test.
• Test fixtures, specimen holding jaws, and
related sample making equipment are
called for in many test methods.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
USE OF UTM
• The set-up and usage are detailed in a test method, often published by a standards
organization.
• This specifies the sample preparation, fixturing, gauge length (the length which is under
study or observation), analysis, etc.
• The specimen is placed in the machine between the grips and an extensometer if
required can automatically record the change in gauge length during the test.
• If an extensometer is not fitted, the machine itself can record the displacement between
its cross heads on which the specimen is held.
• However, this method not only records the change in length of the specimen but also all
other extending / elastic components of the testing machine and its drive systems
including any slipping of the specimen in the grips.
• Once the machine is started it begins to apply an increasing load on specimen.
• Throughout the tests the control system and its associated software record the load and
extension or compression of the specimen.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
COMPRESSIVE STRENGTH
• The compressive strength is the
capacity of a material or structure to
withstand loads tending to reduce
size.
• It can be measured by plotting
applied force against deformation in
a testing machine.
• Some materials fracture at their
compressive strength limit; others
deform irreversibly, so a given amount
of deformation may be considered as
the limit for compressive load.
• Compressive strength is a key value
for design of structures.
• Compressive strength is often
measured on a universal testing
machine.
• The compressive test specimen is
shown in figure.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
COMPRESSIVE TEST
• . • Compression is the opposite of tensile
testing. This kind of testing is used for
brittle materials.
• The compressive strength is usually
obtained experimentally by means of
a compressive test.
• The apparatus used for this
experiment is the same as that used
in a tensile test.
• However, rather than applying a
uniaxial tensile load, a uniaxial
compressive load is applied.
• As can be imagined, the specimen
(usually cylindrical) is shortened as
well as spread laterally
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TEST
• The purpose of impact testing is to determine the ability of materials
to withstand impact or shock or suddenly applied load while in
service.
• It is usually thought of in terms of two objects striking each other at
high relative speeds.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
INTRODUCTION
• The CHARPY Impact Tests are conducted on instrumented machines
capable of measuring less than 1 foot-pound. to 300 foot-pounds. at
temperatures ranging from -320°F to over 2000°F.
• Impact test specimen types include notch configurations such as V-
Notch, U-Notch, Key-Hole Notch, as well as Un-notched and ISO
(DIN) V-Notch, with capabilities of impact testing sub-size specimens
down to ¼ size.
• IZOD Impact Testing can be done up to 240 foot-pounds. on
standard single notch and type-X3 specimens.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
TYPES OF IMPACT TEST SPECIMENS
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TESTING
• Notched-bar impact test of
metals provides information on
failure mode under high
velocity loading conditions
leading sudden fracture where
a sharp stress raiser (notch) is
present.
• The energy absorbed at
fracture is generally related to
the area under the stress-strain
curve which is termed as
toughness in some references
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TESTING
• Figure (b) below shows the
brittle fracture in mild steel
• Brittle materials have a small
area under the stress-strain
curve (due to its limited
toughness) and as a result, little
energy is absorbed during
impact failure.
• The fracture surfaces for low
energy impact failures,
indicating brittle behaviour, are
relatively smooth and have
crystalline appearance in the
metals
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TESTING
• Figure (a) below shows cup
cone fracture in aluminum
• As plastic deformation
capability of the materials
(ductility) increases, the area
under the curve also increases
and absorbed energy and
respectively toughness
increase.
• The fracture surfaces for high
energy fractures have regions
of shear where the fracture
surface is inclined about 45° to
the tensile stress, and have
rougher and more highly
deformed appearance, called
fibrous fracture.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TESTING
• The stress- strain curve for both
ductile and brittle materials is
shown in figure.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
CHARPY IMPACT TEST
• Although two standardized tests, the Charpy and Izod, were designed and
used extensively to measure the impact energy, Charpy v-notched impact
tests are more common in practice.
• The apparatus for performing impact tests is illustrated schematically in
Figure
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
CHARPY IMPACT TEST
• The Charpy Impact Test is
commonly used on metals, but
is also applied to composites,
ceramics and polymers.
• The standard Charpy Impact
Test specimen consist of a bar
of metal, or other material,
55x10x10mm having a notch
machined across one of the
larger dimensions.
• Typical v-notched specimen is
shown in figure
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
CHARPY IMPACT TEST
• The load is applied as an impact blow from a weighted pendulum
hammer that is released from a position at a fixed height h.
• The specimen is positioned at the base and with the release of
pendulum, which has a knife edge, strikes and fractures the
specimen at the notch.
• The pendulum continues its swing, rising a maximum height h ' which
should be lower than h naturally.
• The energy absorbed at fracture E can be obtained by simply
calculating the difference in potential energy of the pendulum
before and after the test such as,
E = m.g.(h-h ')
• where m is the mass of pendulum and g is the gravitational
acceleration.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IZOD IMPACT TEST
• Izod test is carried out on a cantilever test specimen 10 X 10 X 75mm
long having a standard 45⁰ notch 2 mm deep.
• In the presence of notch ductile material behave like a brittle one so
that rupture can takes place during impact. This property is called
notch sensitivity.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
IMPACT TESTING
MACHINE
• The same testing machine is
used for both charpy and izod
impact testing.
• The impact testing machine is
shown in figure.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
TESTING PROCEDURE
• The specimen is held vertically
as a cantilever between two
jaws in such a way that the
striking hammer in the swinging
pendulum strikes the specimen
on the same face as that of
notch.
• The specimen is broken by
means of that pendulum which
is allowed to fall from a certain
height to cause an impact
load on the specimen
• The angle of rise of the
pendulum after the rupture of
the specimen or the energy to
rupture the specimen is
indicated on the graduated
scale by the pointer.
• The energy required to rupture
the specimen is a function of
angle of rise.
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
TEST CALCULATIONS
• Let “W” be the weight of
pendulum and “α” be the
angle through which
pendulum falls and “β”
be the angle through
which pendulum rises
and “R” is the distance
between the center of
gravity of pendulum and
axis of rotation.
• From the geometry of the
testing machine,
• Initial energy of the
pendulum before
striking= WR(1-cos α)
• Final energy of the
pendulum after breaking
the specimen=WR(1-cos
β)
• Assuming there are no
losses, energy required to
breakaway the specimen
=WR(1-cos α)-WR(1-cos β)
= WR(cos β - cos α)
= W(h1 – h2)
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY
DUCTILE-BRITTLE TRANSITION IN
IMPACT TEST
• The notched bar impact test is
also used to determine the
ductile brittle transition
temperature of a material at
which there is a big change in
the energy absorbed.
• A curve plotted between
impact energy and
temperature of the specimen
and using that the transition
temperature can be
determined as shown in figure
SCHOOL OF AERONAUTICAL SCIENCES
HINDUSTAN UNIVERSITY

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Aircraft materials lecture 2

  • 1. T e n s i l e T e s t i n g a n d C o m p r e s s i v e T e s t i n g M e t h o d s B Y : K A N U P R I Y A J H A N J I A S S T . P R O F E S S O R S C H O O L O F A E R O N A U T I C A L S C I E N C E S H I N D U S T A N U N I V E R S I T Y k a n u p r i y a j @ h i n d u s t a n u n i v . a c . i n AIRCRAFT MATERIALS UNIT-1 LECTURE2
  • 2. INSTRUCTIONAL OBJECTIVES • By the end of lecture, the students will learn the working principle of ultimate testing machine and procedure of performing the tensile and compressive tests. • Students will also have knowledge about the various impact tests. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 3. CONTENTS • Tensile testing • Equipment for testing • Process of testing • Components of Universal Testing Machine • Use of UTM • Compressive strength • Compressive test • Charpy impact test • Izod impact test SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 4. TENSILE TESTING • Tensile testing, also known as tension testing, is a fundamental materials science test in which a sample is subjected to a controlled tension until failure. • The results from the test are commonly used to select a material for an application, for quality control, and to predict how a material will react under other types of forces. • Properties that are directly measured via a tensile test are ultimate tensile strength, maximum elongation and reduction in area. • The test specimen is shown in the figure. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 5. TENSILE TESTING • From these measurements the following properties can also be determined: Young's modulus, Poisson's ratio, yield strength, and strain-hardening characteristics. • Uniaxial tensile testing is the most commonly used for obtaining the mechanical characteristics of isotropic materials. • For anisotropic materials, such as composite materials and textiles, biaxial tensile testing is required. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 6. EQUIPMENT • The most common testing machine used in tensile testing is the universal testing machine. • This type of machine has two crossheads; one is adjusted for the length of the specimen and the other is driven to apply tension to the test specimen. • There are two types: hydraulic powered and electromagnetically powered machines SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 7. PROCESS • The test process involves placing the test specimen in the testing machine and slowly extending it until it fractures. • During this process, the elongation of the gauge section is recorded against the applied force. • The data is manipulated so that it is not specific to the geometry of the test sample. • The elongation measurement is used to calculate the engineering strain, ε, using the following equation:[ • where ΔL is the change in gauge length, L0 is the initial gauge length, and L is the final length. • The force measurement is used to calculate the engineering stress, σ, using the following equation: • where F is the tensile force and A is the nominal cross-section of the specimen. The machine does these calculations as the force increases, so that the data points can be graphed into a stress–strain curve. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 8. COMPONENTS OF UNIVERSAL TESTING MACHINE • Load frame - Usually consisting of two strong supports for the machine. Some small machines have a single support. • Load cell - A force transducer or other means of measuring the load is required. Periodic calibration is usually required by governing regulations or quality system. • Cross head - A movable cross head (crosshead) is controlled to move up or down. Usually this is at a constant speed: sometimes called a constant rate of extension (CRE) machine. • Some machines can program the crosshead speed or conduct cyclical testing, testing at constant force, testing at constant deformation, etc. Electromechanical, servo-hydraulic, linear drive, and resonance drive are used. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 9. COMPONENTS OF UNIVERSAL TESTING MACHINE • Means of measuring extension or deformation - Many tests require a measure of the response of the test specimen to the movement of the cross head. • Extensometers are sometimes used. • Output device - A means of providing the test result is needed. Some older machines have dial or digital displays and chart recorders. • Many newer machines have a computer interface for analysis and printing. • Conditioning - Many tests require controlled conditioning (temperature, humidity, pressure, etc.). The machine can be in a controlled room or a special environmental chamber can be placed around the test specimen for the test. • Test fixtures, specimen holding jaws, and related sample making equipment are called for in many test methods. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 10. USE OF UTM • The set-up and usage are detailed in a test method, often published by a standards organization. • This specifies the sample preparation, fixturing, gauge length (the length which is under study or observation), analysis, etc. • The specimen is placed in the machine between the grips and an extensometer if required can automatically record the change in gauge length during the test. • If an extensometer is not fitted, the machine itself can record the displacement between its cross heads on which the specimen is held. • However, this method not only records the change in length of the specimen but also all other extending / elastic components of the testing machine and its drive systems including any slipping of the specimen in the grips. • Once the machine is started it begins to apply an increasing load on specimen. • Throughout the tests the control system and its associated software record the load and extension or compression of the specimen. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 11. COMPRESSIVE STRENGTH • The compressive strength is the capacity of a material or structure to withstand loads tending to reduce size. • It can be measured by plotting applied force against deformation in a testing machine. • Some materials fracture at their compressive strength limit; others deform irreversibly, so a given amount of deformation may be considered as the limit for compressive load. • Compressive strength is a key value for design of structures. • Compressive strength is often measured on a universal testing machine. • The compressive test specimen is shown in figure. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 12. COMPRESSIVE TEST • . • Compression is the opposite of tensile testing. This kind of testing is used for brittle materials. • The compressive strength is usually obtained experimentally by means of a compressive test. • The apparatus used for this experiment is the same as that used in a tensile test. • However, rather than applying a uniaxial tensile load, a uniaxial compressive load is applied. • As can be imagined, the specimen (usually cylindrical) is shortened as well as spread laterally SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 13. IMPACT TEST • The purpose of impact testing is to determine the ability of materials to withstand impact or shock or suddenly applied load while in service. • It is usually thought of in terms of two objects striking each other at high relative speeds. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 14. INTRODUCTION • The CHARPY Impact Tests are conducted on instrumented machines capable of measuring less than 1 foot-pound. to 300 foot-pounds. at temperatures ranging from -320°F to over 2000°F. • Impact test specimen types include notch configurations such as V- Notch, U-Notch, Key-Hole Notch, as well as Un-notched and ISO (DIN) V-Notch, with capabilities of impact testing sub-size specimens down to ¼ size. • IZOD Impact Testing can be done up to 240 foot-pounds. on standard single notch and type-X3 specimens. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 15. TYPES OF IMPACT TEST SPECIMENS SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 16. IMPACT TESTING • Notched-bar impact test of metals provides information on failure mode under high velocity loading conditions leading sudden fracture where a sharp stress raiser (notch) is present. • The energy absorbed at fracture is generally related to the area under the stress-strain curve which is termed as toughness in some references SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 17. IMPACT TESTING • Figure (b) below shows the brittle fracture in mild steel • Brittle materials have a small area under the stress-strain curve (due to its limited toughness) and as a result, little energy is absorbed during impact failure. • The fracture surfaces for low energy impact failures, indicating brittle behaviour, are relatively smooth and have crystalline appearance in the metals SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 18. IMPACT TESTING • Figure (a) below shows cup cone fracture in aluminum • As plastic deformation capability of the materials (ductility) increases, the area under the curve also increases and absorbed energy and respectively toughness increase. • The fracture surfaces for high energy fractures have regions of shear where the fracture surface is inclined about 45° to the tensile stress, and have rougher and more highly deformed appearance, called fibrous fracture. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 19. IMPACT TESTING • The stress- strain curve for both ductile and brittle materials is shown in figure. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 20. CHARPY IMPACT TEST • Although two standardized tests, the Charpy and Izod, were designed and used extensively to measure the impact energy, Charpy v-notched impact tests are more common in practice. • The apparatus for performing impact tests is illustrated schematically in Figure SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 21. CHARPY IMPACT TEST • The Charpy Impact Test is commonly used on metals, but is also applied to composites, ceramics and polymers. • The standard Charpy Impact Test specimen consist of a bar of metal, or other material, 55x10x10mm having a notch machined across one of the larger dimensions. • Typical v-notched specimen is shown in figure SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 22. CHARPY IMPACT TEST • The load is applied as an impact blow from a weighted pendulum hammer that is released from a position at a fixed height h. • The specimen is positioned at the base and with the release of pendulum, which has a knife edge, strikes and fractures the specimen at the notch. • The pendulum continues its swing, rising a maximum height h ' which should be lower than h naturally. • The energy absorbed at fracture E can be obtained by simply calculating the difference in potential energy of the pendulum before and after the test such as, E = m.g.(h-h ') • where m is the mass of pendulum and g is the gravitational acceleration. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 23. IZOD IMPACT TEST • Izod test is carried out on a cantilever test specimen 10 X 10 X 75mm long having a standard 45⁰ notch 2 mm deep. • In the presence of notch ductile material behave like a brittle one so that rupture can takes place during impact. This property is called notch sensitivity. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 24. IMPACT TESTING MACHINE • The same testing machine is used for both charpy and izod impact testing. • The impact testing machine is shown in figure. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 25. TESTING PROCEDURE • The specimen is held vertically as a cantilever between two jaws in such a way that the striking hammer in the swinging pendulum strikes the specimen on the same face as that of notch. • The specimen is broken by means of that pendulum which is allowed to fall from a certain height to cause an impact load on the specimen • The angle of rise of the pendulum after the rupture of the specimen or the energy to rupture the specimen is indicated on the graduated scale by the pointer. • The energy required to rupture the specimen is a function of angle of rise. SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 26. TEST CALCULATIONS • Let “W” be the weight of pendulum and “α” be the angle through which pendulum falls and “β” be the angle through which pendulum rises and “R” is the distance between the center of gravity of pendulum and axis of rotation. • From the geometry of the testing machine, • Initial energy of the pendulum before striking= WR(1-cos α) • Final energy of the pendulum after breaking the specimen=WR(1-cos β) • Assuming there are no losses, energy required to breakaway the specimen =WR(1-cos α)-WR(1-cos β) = WR(cos β - cos α) = W(h1 – h2) SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY
  • 27. DUCTILE-BRITTLE TRANSITION IN IMPACT TEST • The notched bar impact test is also used to determine the ductile brittle transition temperature of a material at which there is a big change in the energy absorbed. • A curve plotted between impact energy and temperature of the specimen and using that the transition temperature can be determined as shown in figure SCHOOL OF AERONAUTICAL SCIENCES HINDUSTAN UNIVERSITY