3. Deformation
So far, we've focused on the STRESS within structural
elements.
When you apply stress to an object, it deforms.
Think of a rubber band: you pull on it, and it gets longer – it
stretches.
Deformation is a measure of how much an object is
stretched, and strain is the ratio between the deformation
and the original length.
Think of strain as percent elongation – how much bigger (or
smaller) is the object upon loading it.
4. Deformation
In Engineering, deformation is a change in the shape or size
of an object due to:
an applied force (the deformation energy in this case is
transferred through work) or
a change in temperature (the deformation energy in this
case is transferred through heat).
The first case can be a result of tensile (pulling) forces,
compressive (pushing) forces, shear, bending or torsion
(twisting).
Deformation is often described as strain.
Strain is the measure of deformation
5. Cont…
As deformation occurs, internal inter-
molecular forces arise that oppose the
applied force.
If the applied force is not too large these
forces may be sufficient to completely resist
the applied force, allowing the object to
assume a new equilibrium state and to return
to its original state when the load is
removed.
A larger applied force may lead to a
permanent deformation of the object or even
to its structural failure.
6. Strain
Type of strain:
Normal Strain :- strain which is due to normal force.
Shearing Strain :- strain which is due to shearing (tangential)
force.
7. Normal Strain
Consider a prismatic bar of a homogeneous material is
subjected to an axial force P, the bar of length L shows
a change in length by δ (deformation).
The change in length per unit length is defined a
strain, and is denoted by the Greek letter ε (epsilon).
8. Cont…
• If the bar is in tension, the strain is called a
tensile strain representing an elongation of the
material.
• If the bar is in compression, the strain is a
compressive strain, the bar shortens.
• Sign convention: Tensile strain is taken as
positive and compressive strain as negative.
• It is a dimensionless quantity.
9. Shear Strain
A shear strain results from shear stress.
It is a strain computed from relative displacements that are
measured parallel to two reference planes.
Shear strains measure the relative parallel movement of one
reference plane with respect to another.
10. Shear Strain
The symbol for the shear strain is usually the lowercase Greek
symbol gamma (γ).
The unit of the shear stress is frequently expressed in radians
11. Stress - Strain Diagram
Tension or Compression Test - Property of Materials
12. Strength of a material can only be determined by
experiment
One test used by engineers is the tension or compression
test
This test is used primarily to determine the relationship
between the average normal stress and average normal
strain in common engineering materials, such as metals,
ceramics, polymers and composites
TENSION & COMPRESSION TEST
13. Performing the tension or compression test
Specimen of material is made into “standard” shape and size
Before testing, 2 small punch marks identified along specimen’s
length
Measurements are taken of both specimen’s initial x-sectional
area A0 and gauge-length distance L0; between the two marks
Seat the specimen into a testing machine shown below
TENSION & COMPRESSION TEST
14. Performing the tension or compression test
TENSION & COMPRESSION TEST
The machine will stretch specimen
at slow constant rate until
breaking point
At frequent intervals during test,
data is recorded of the applied
load P.
15. Performing the tension or compression test
Elongation δ = L − L0 is measured using either a caliper or an
extensometer
δ is used to calculate the normal strain in the specimen
Sometimes, strain can also be read directly using an electrical-
resistance strain gauge
TENSION & COMPRESSION TEST
16. A stress-strain diagram is obtained by plotting the various
values of the stress and corresponding strain in the specimen
Conventional stress-strain diagram
Using recorded data, we can determine nominal or
engineering stress by
STRESS-STRAIN DIAGRAM
P
A0
σ =
Assumption: Stress is constant over the x-section and throughout region between
gauge points
17. Conventional Stress-Strain Diagram
Likewise, nominal or engineering strain is found directly from
strain gauge reading, or by
STRESS-STRAIN DIAGRAM
δ
L0
=
Assumption: Strain is constant throughout region between gauge points
By plotting σ (ordinate) against (abscissa), we get a
conventional stress-strain diagram
18. Conventional stress-strain diagram
Figure shows the characteristic stress-strain diagram for steel,
a commonly used material for structural members and
mechanical elements
STRESS-STRAIN DIAGRAM
19. Conventional stress-strain diagram
STRESS-STRAIN DIAGRAM
Elastic behavior
A straight line
Stress is proportional to strain,
i.e., linearly elastic
Upper stress limit, or
proportional limit; σpl
If load is removed upon reaching
elastic limit, specimen will return
to its original shape
20. Conventional stress-strain diagram
STRESS-STRAIN DIAGRAM
Figure 3-4
Yielding
Material deforms
permanently; yielding; plastic
deformation
Yield stress, σY
Once yield point reached, specimen continues to elongate
(strain) without any increase in load
Material is referred to as being perfectly plastic
21. Conventional stress-strain diagram
STRESS-STRAIN DIAGRAM
Figure 3-4
Strain hardening
Ultimate stress, σu
While specimen is
elongating, its x-sectional
area will decrease
Decrease in area is fairly
uniform over entire gauge
length
22. Conventional stress-strain diagram
STRESS-STRAIN DIAGRAM
Figure 3-4
Necking
At ultimate stress, x-sectional
area begins to decrease in a
localized region
As a result, a constriction or
“neck” tends to form in this
region as specimen elongates
further
Specimen finally breaks at fracture stress, σf
24. True stress-strain diagram
STRESS-STRAIN DIAGRAM
Instead of using original cross-sectional area and length, we
can use the actual cross-sectional area and length at the
instant the load is measured
Values of stress and strain thus calculated are called true stress
and true strain, and a plot of their values is the true stress-
strain diagram
25. True stress-strain diagram
STRESS-STRAIN DIAGRAM
In strain-hardening range, conventional σ- diagram shows
specimen supporting decreasing load
While true σ- diagram shows material to be sustaining
increasing stress
26. True stress-strain diagram
STRESS-STRAIN DIAGRAM
Although both diagrams are different, most engineering design
is done within elastic range provided
1. Material is “stiff,” like most metals
2. Strain to elastic limit remains small
3. Error in using engineering values of σ and is very small
(0.1 %) compared to true values
27. E represents the constant of proportionality, also called the
modulus of elasticity or Young’s modulus
E has units of stress, i.e., pascals, MPa or GPa.
HOOKE’S LAW
Most engineering materials exhibit a linear relationship
between stress and strain with the elastic region
Discovered by Robert Hooke in 1676 using springs, known as
Hooke’s law
σ = E
28. As shown above, most grades of steel
have same modulus of elasticity, Est =
200 GPa
Modulus of elasticity is a mechanical
property that indicates the stiffness of
a material
Materials that are still have large E
values, while spongy materials
(vulcanized rubber) have low values
HOOKE’S LAW
29. IMPORTANT
• Modulus of elasticity E, can be used only if a material
has linear-elastic behavior.
• Also, if stress in material is greater than the
proportional limit, the stress-strain diagram ceases to
be a straight line and the equation is not valid
HOOKE’S LAW