Elastic
Modulus—
The
ratio of stress and strain is known as Elastic Modulus.
Elastic Modulus (E) = Stress (σ) /
Strain (ϵ)
The constant of proportionality
depends on the material being deformed and the nature of the deformation. This
constant is called the elastic modulus.
The elastic modulus determines the
amount of force required per unit deformation.
Ø A material with large elastic modulus
is difficult to deform.
Ø With small elastic modulus is easier to
deform.
HOOKE’S LAW—
Within the elastic limit, Stress-
Strain ratio is constant. [Stress/Strain = Constant]
“In
an elastic member stress (σ) is directly proportional to the strain (ϵ) within
elastic Limit.”
σ ∝ ϵ
σ = E. ϵ
or, E =
σ / ϵ
Where,
σ = Stress
ϵ = Strain
E =
Constant (modulus of Elasticity / Young’s Modulus)
ϵ à
Initially, a stress-strain curve
is a straight line. As the stress increases, the curve is no longer
straight. When the stress exceeds the elastic limit, the object is permanently
distorted and does not return to its original shape after the stress is
removed. Hence, the shape of the object is permanently changed. As the stress
is increased even further, the material ultimately breaks.
Types of Elastic Modulus
1.
Young’s
Modulus (y)
2.
Bulk
Modulus (B)
3.
Rigidity
Modulus / Shear modulus (η)
Young’s Modulus (y)
Within the elastic limit, the ratio of
longitudinal stress (tensile/ compressive) and longitudinal strain (tensile/
Compressive) is called young’s
modulus of elasticity (y).
Young’s modulus (y) = Longitudinal stress / Longitudinal
strain
y = σ / ϵ
y = (F/ A)/(ΔL/L) = [FL/AΔL]
Bulk
Modulus (B)
Within
elastic limit the ratio of the volume stress (F/A) and the volume
strain (ΔV/V) is called bulk modulus of elasticity.
B = (σvol
/ ϵvol) = (F/A) / (-ΔV/V) = ΔP / (-ΔV/V)
B = = ΔP / (-ΔV/V)
Where,
ΔP = Pressure
applied
Rigidity Modulus / Shear modulus (η)
Within elastic limit, the ratio of shearing
stress (or) tangential stress and shearing strain (or) tangential strain is
called modulus of rigidity.
η = Shearing stress / shearing strain
η = τ / ϕ
Where,
η = shear modulus
τ = shear force (F/A)
ϕ = angle of shear
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