Ch 1. Stress and Strain Multimedia Engineering Mechanics NormalStress Shear andBearing Stress NormalStrain Hooke'sLaw ThermalEffects IndeterminateStructures
 Chapter 1. Stress/Strain 2. Torsion 3. Beam Shr/Moment 4. Beam Stresses 5. Beam Deflections 6. Beam-Advanced 7. Stress Analysis 8. Strain Analysis 9. Columns Appendix Basic Math Units Basic Equations Sections Material Properties Structural Shapes Beam Equations Search eBooks Dynamics Fluids Math Mechanics Statics Thermodynamics Author(s): Kurt Gramoll ©Kurt Gramoll

MECHANICS - THEORY

Normal Strain

Prismatic Bar Undergoing Elongation

Strain, represented by the Greek letter ε, is a term used to measure the deformation or extension of a body that is subjected to a force or set of forces. The strain of a body is generally defined as the change in length divided by the initial length.

 ε = ΔL/L

Often, the change in length of the bar, ΔL, is simply referred to as the total displacement, or δ. In that case, strain is then

 ε = δ/L

The elongation of the bar is assumed normal, or perpendicular, to the cross section. Therefore, like stress, the strain is called a normal strain. Similar to stress, a tensile strain is generally considered positive and a compressive strain is considered negative.

Stress-Strain Relationship

Spring Analogy for
Stress/Strain Relationship

For linearly elastic materials, Hooke's Law relates the stress of a body to the strain in the elastic range. Through experiments, it can be shown that most materials act like springs in that the force is proportional to the displacement (F = kδ). However, unlike a spring, a bar has a cross-sectional area that effects the displacement. Therefore, it is simpler to relate the stress (F/A) to the strain (δ/L). This gives the relationship,

 σ = Eε

where E is the material property that represents the stiffness of the material (called Young's Modulus). Simply stated, the stress is directly proportional to the strain. Young's modulus is determined through experiments and are commonly listed in engineering handbooks (appendix has a partial list for many common structural materials).

This stress-strain relationship is called Hooke's Law. In the next section, this relationship will be expanded to two dimensions.

Stress-Strain Curve

Prismatic Bar Undergoing Elongation

General Stress-Strain Curves
for Various Materials

The previous paragraphs developed the basic linear elastic stress-strain relationship assuming there was no plastic deformation. However, if most materials are strained enough, they will permanently deform. When a material deforms, the stress-strain relationship is no longer linear.

It is common to plot the stress as a function of the strain. This curve is called the 'Stress-Strain Curve'. Each material has a unique curve, but for most materials, the initial curve is a straight line reflecting the linear relationship between the stress and strain. This is called the 'Elastic' range. Hooke's Law only applies in this range.

If the material is stressed past its elastic limit, the material will be permanently deformed and plastic deformation will occur. This means the material has yielded and will stretch easily with little additional load. Next, the material cross-section will become smaller which is called "necking".

Since the cross-sectional area is reducing, the effective, or true stress goes up. However, many times the stress calculations will use the original cross sectional area (called the nominal area) and this makes the stress-strain curve appear to go down.

While most material have an elastic range, some do not. Rubber has no linear range. Most glasses at room temperature have only an elastic range. Some examples of basic stress-strain curves are given at the left.

Uniaxial Deflection - Constant Load, Area and Stiffness

Total Deformation
δ = PL/AE

For a simple homogenous bar with a constant cross section and a constant applied load, the total deflection of the bar can be determined in terms of P, L, A, and E. Starting with the one dimensional Hooke's Law,

σ = Eε

and substituting P/A for stress and δ/L for strain gives,

P/A = E (δ/L)

This can be rearranged to give,

Total Deformation
δ = PL1/A1E1 + PL2/A2E2 + PL3/A3E3

If there are a series of bars, then the deflection of each section can be determined and then all deflections summed. This can be written in equation form as

Uniaxial Deflection - Variable Load, Area and Stiffness

Integraion Required when