Engineering Stress-Strain Curve
The engineering stress-strain curve gives the relationship between
stress and strain for a ductile material. It is generally obtained by applying
load to a tensile specimen. The curve reveal many properties of a material such
as Young's Modulus(E), Yield point, UTS etc.
Stress :
The stress in the engineering stress-strain diagram is given by load
divided by the original area.
Strain :
The strain in the engineering stress-strain curve is giver by ratio of
change in length / elongation to its initial length.
Strain
has no unit since it’s a ratio of two quantities.
Proportionality limit :
In the curve, OA is linear. This is due to the fact that the stress is
directly proportional to the strain i.e. it follows Hooke’s law. Hooke’s law
states that within the elastic limit the stress is directly proportional to the
strain. The point A represents the proportionality limit. Up to A if the load
is removed the material regains its original shape along AO.
The
constant of proportionality k is known Modulus of elasticity or Young’s
Modulus. Thus, this is equal to the slope of the curve from OA.
Elastic limit :
The
elastic limit is the point beyond which the material will no longer go back to its
original shape when the load is removed. Here OC is the elastic limit.
Permanent set :
Beyond
A the curve is not linear and in the region AC the material is partially
plastic and partially elastic. The if we apply load and remove it deforms along
C to the strain axis. Thus it doesn’t retain its original shape. Thus this
permanent strain caused in the material offsets the OA by 0.2% and is
considered as the permanent set.
Elastic and plastic regions :
The
region from O to A is the elastic region and the region from A to B is
partially plastic and partially elastic. And the region from B to E is plastic
region.
Yield point :
Beyond
B even a small amount of stress will lead to enormous strain. Thus, the point B
is known as the yield point. Beyond this point the material starts to undergo
plastic deformation. Now it is permanently deformed when the load is removed.
The stress to produce continued plastic deformation increases with strain i.e.
the material strain-hardens. The volume of specimen remains constant until
point D. Thus from law of constancy of volume,
AL = AoLo
Ultimate Tensile Strength(UTS) :
The
maximum load that the material will withstand is denoted by the point D known
as UTS. It is given by :
This
is useful for purpose of specifications and quality control of a product.
Beyond this point necking occurs.
Rupture strength :
The
point D represents the UTS and further increase in load will lead to decrease
in cross-sectional area a phenomenon known as necking. Now, because the
cross-sectional area is decreasing the actual load required to deform a
material decreases. Further increase in load will finally lead to fracture
represented by point E. The strength of the material at this point is known as
the fracture strength or rupture strength.
Resilience :
The
ability of a material to absorb energy without creating any permanent
distortion is known as resilience.
Modulus of resilience :
The
work done on unit volume of a material as the force increases from O to A is
known as the modulus of resilience. This can be calculated from the area under
the curve from O to the elastic limit.
Here, s2 is the yield strength of the material and E is
the Young’s modulus of the material. Its unit is .
Toughness :
The
ability of a material to absorb energy without breaking is known as toughness.
Modulus of toughness :
The
work done on unit volume of a material as the force increases from O to E is
known as the modulus of toughness. This can be calculated from the area under
the curve from O to E i.e. the entire stress strain curve.
Measure of ductility :
The
measures of ductility in a material is the reduction in area of the material at
the fracture and its elongation.
Both
elongations and reduction in area is
represented in percentage.
Allowable stress :
The
maximum safe stress that a material can withstand is knows as allowable stress.
This must me usually within the proportionality limit.
Working stress :
The
stress of a material under a given load is known as working stress.
Factor of safety :
The
factor of safety is defined as the ratio of UTS to the working stress.
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