October, 2008

Solution to Problem 203 Stress-strain Diagram

Strength of Materials 4th Edition by Pytel and Singer
Problem 203 page 39

Given:
Material: 14-mm-diameter mild steel rod
Gage length = 50 mm
Test Result:

Load (N) Elongation (mm) Load
(N)
Elongation (mm)
0 0 46 200 1.25
6 310 0.010 52 400 2.50
12 600 0.020 58 500 4.50
18 800 0.030 68 000 7.50
25 100 0.040 59 000 12.5
31 300 0.050 67 800 15.5
37 900 0.060 65 000 20.0
40 100 0.163 65 500 Fracture
41 600 0.433

Required:
Stress-strain diagram, Proportional limit, modulus of elasticity, yield point, ultimate strength, and rupture strength

Axial Deformation

Axial deformation of non-uniform cross-section

In the linear portion of the stress-strain diagram, the tress is proportional to strain and is given by

\sigma = E \varepsilon

since \sigma = P / A and \varepsilon = \delta / L, then \dfrac{P}{A} = E \dfrac{\delta}{L}

\delta = \dfrac{PL}{AE} = \dfrac{\sigma L}{E}

To use this formula, the load must be axial, the bar must have a uniform cross-sectional area, and the stress must not exceed the proportional limit.

Stress-strain Diagram

Stress-strain diagram of typical structural material

Suppose that a metal specimen be placed in tension-compression-testing machine. As the axial load is gradually increased in increments, the total elongation over the gauge length is measured at each increment of the load and this is continued until failure of the specimen takes place. Knowing the original cross-sectional area and length of the specimen, the normal stress \sigma and the strain \varepsilon can be obtained. The graph of these quantities with the stress \sigma along the y-axis and the strain \varepsilon along the x-axis is called the stress-strain diagram. The stress-strain diagram differs in form for various materials. The diagram shown below is that for a medium-carbon structural steel.

Simple Strain

Also known as unit deformation, strain is the ratio of the change in length caused by the applied force, to the original length.

Simple strain

\varepsilon = \dfrac{\delta}{L}

where \delta is the deformation and L is the original length, thus \varepsilon is dimensionless.

Chapter 2 - Strain

  1. Simple Strain
  2. Stress-Strain Diagram
  3. Axial Deformation
  4. Shearing Deformation
  5. Poisson’s Ratio
  6. Statically Indeterminate Members
  7. Thermal Stress

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