Chapter 6: Problem 2
(a) Equations \(6.4 a\) and \(6.4 \mathrm{~b}\) are expressions for normal \(\left(\sigma^{\prime}\right)\) and shear \(\left(\tau^{\prime}\right)\) stresses, respectively, as a function of the applied tensile stress \((\sigma)\) and the inclination angle of the plane on which these stresses are taken ( \(\theta\) of Figure 6.4). Make a plot showing the orientation parameters of these expressions (i.e., \(\cos ^{2} \theta\) and \(\sin \theta \cos \theta\) ) versus \(\theta\). (b) From this plot, at what angle of inclination is the normal stress a maximum? (c) At what inclination angle is the shear stress a maximum?
Short Answer
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Key Concepts
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