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SIMPLE STRAIN
INTRODUCTION TO STRAIN • In general terms,
– Strain is a geometric quantity that measures the deformation of a body.
• There are two types of strain: – normal strain: characterizes dimensional
changes, – shear strain: describes distortion (changes
in angles).
INTRODUCTION TO STRAIN
• Stress and strain are two fundamental concepts of mechanics of materials.
• Their relationship to each other defines the mechanical properties of a material, the knowledge of which is of the utmost importance in design.
NORMAL STRAIN • Defined as the elongation per unit
length.
normal strainL
elongation
δε
δ
= =
→
TENSION TEST
TENSION TEST
TENSION TEST • Elastic Limit
– A material is said to be elastic if, after being loaded, the material returns to its original shape when the load is removed.
– The elastic limit is, as its name implies, the stress beyond which the material is no longer elastic.
– The permanent deformation that remains after the removal of the load is called the permanent set.
TENSION TEST • Yield Point
– The point where the stress-strain diagram becomes almost horizontal is called the yield point, and the corresponding stress is known as the yield stress or yield strength.
– Beyond the yield point there is an appreciable elongation, or yielding, of the material without a corresponding increase in load
TENSION TEST • Ultimate Stress
– The ultimate stress or ultimate strength, as it is often called, is the highest stress on the stress-strain curve.
• Rupture Stress
– The rupture stress or rupture strength is the stress at which failure occurs.
HOOKE’S LAW • Stress–Strain diagrams for most
engineering materials exhibit a linear relationship between stress and strain within the elastic region.
• Consequently, an increase in stress causes a proportionate increase in strain.
• Discovered by Robert Hooke in 1676 using springs and is known as Hooke’s law.
HOOKE’S LAW • expressed mathematically as
σ ε=
= Youngs Modulus or Modulus of Elasticity
E
whereE
DEFORMATIONS IN A SYSTEM OF AXIALLY LOADED BARS
L PLE EAσδ = =
(uniform stress/strain across)
0
L P dxEA
δ = ∫ (stress/strain varies)
SAMPLE PROBLEM 1 • The steel propeller shaft ABCD carries the
axial loads shown in Fig. (a). Determine the change in the length of the shaft caused by these loads. Use E = 29 x 106 psi for steel.
SAMPLE PROBLEM 2 • The cross section of the 10-m-long flat steel
bar AB has a constant thickness of 20 mm, but its width varies as shown in the figure. Calculate the elongation of the bar due to the 100-kN axial load. Use E = 200 GPa for steel.
SAMPLE PROBLEM 3 • The rigid bar BC in the figure is supported by
the steel rod AC of cross-sectional area 0.25 in2. Find the vertical displacement of point C caused by the 2000-lb load. Use E = 29 x 106 psi for steel.
POISSON’S RATIO
∈= −
∈t
x
v
• In 1811, Simeon D. Poisson showed that the ratio of the transverse strain to the axial strain is constant for stresses within the proportional limit.
UNIAXIAL STATE OF STRESS • The minus sign indicates that a positive strain (elongation) in
the axial direction causes a negative strain (contraction) in the transverse directions.
• Transverse strain is uniform throughout the cross section and is the same in any direction in the plane of the cross section.
∈ =∈ = − ∈y z xv
σ∈ =∈ = − xy z v E
SHEAR LOADING • Shear stress causes the
deformation shown in the figure.
• lengths of the sides do not change, but the element undergoes a distortion from a rectangle to a parallelogram.
SHEAR LOADING • The shear strain, which
measures the amount of distortion, is the angle always expressed in radians.
• It can be shown that the relationship between shear stress and shear strain is linear within the elastic range
shear Modulus or Modulus of rigidity
=2(1 )
τ γ=
=
+
GwhereG
Ev
γ
γτ
SAMPLE PROBLEM 1 • Two 1.75-in.-thick rubber
pads are bonded to three steel plates to form the shear mount shown. Find the displacement of the middle plate when the 1200-lb load is applied. Consider the deformation of rubber only. Use E = 500 psi and v = 0.48 for rubber.
SAMPLE PROBLEM 2 • An initially rectangular element of material is
deformed as shown in the figure . Calculate the normal strains and , and the shear strain for the element. x
ε yε γ
SIMPLE STRAININTRODUCTION TO STRAININTRODUCTION TO STRAINNORMAL STRAINTENSION TESTTENSION TESTTENSION TESTTENSION TESTTENSION TESTHOOKE’S LAWHOOKE’S LAWDEFORMATIONS IN A SYSTEM OF AXIALLY LOADED BARSSAMPLE PROBLEM 1SAMPLE PROBLEM 2SAMPLE PROBLEM 3POISSON’S RATIOUNIAXIAL STATE OF STRESSSHEAR LOADINGSHEAR LOADINGSAMPLE PROBLEM 1SAMPLE PROBLEM 2