Chapter 10: Problem 1
Prove that the sum of the normal strains in perpendicular directions is constant.
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Chapter 10: Problem 1
Prove that the sum of the normal strains in perpendicular directions is constant.
These are the key concepts you need to understand to accurately answer the question.
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Derive an expression for an equivalent bending moment \(M_{e}\) that, if applied alone to a solid bar with a circular cross section, would cause the same energy of distortion as the combination of an applied bending moment \(M\) and torque \(T\).
The state of strain at the point on the bracket has components \(\epsilon_{x}=-200\left(10^{-6}\right), \quad \epsilon_{y}=-650\left(10^{-6}\right)\), \(\gamma_{x y}=-175\left(10^{-6}\right) .\) Use the strain-transformation equations to determine the equivalent in-plane strains on an element oriented at an angle of \(\theta=20^{\circ}\) counterclockwise from the original position. Sketch the deformed element due to these strains within the \(x-y\) plane.
Consider the general orientation of three strain gauges at a point as shown. Write a computer program that can be used to determine the principal in-plane strains and the maximum in-plane shear strain at the point. Show an application of the program using the values \(\theta_{a}=40^{\circ}\), \(\boldsymbol{\epsilon}_{a}=160\left(10^{-6}\right), \theta_{b}=125^{\circ}, \boldsymbol{\epsilon}_{b}=100\left(10^{-6}\right), \theta_{c}=220^{\circ},\) \(\boldsymbol{\epsilon}_{c}=80\left(10^{-6}\right)\).
The state of plane strain on an element is \(\epsilon_{x}=-300\left(10^{-6}\right), \quad \epsilon_{y}=0, \quad\) and \(\quad \gamma_{x y}=150\left(10^{-6}\right)\). Determine the equivalent state of strain which represents (a) the principal strains, and (b) the maximum in-plane shear strain and the associated average normal strain. Specify the orientation of the corresponding elements for these states of strain with respect to the original element.
Strain gauge \(b\) is attached to the surface of the gas \(\operatorname{tank}\) at an angle of \(45^{\circ}\) with \(x\) axis as shown. When the tank is pressurized, the strain gauge gives a reading of \(\epsilon_{b}=250\left(10^{-6}\right) .\) Determine the pressure in the tank.The tank has an inner diameter of \(1.5 \mathrm{m}\) and wall thickness of \(25 \mathrm{mm}\). It is made of steel having a modulus of elasticity \(E=200\) GPa and Poisson's ratio \(\nu=\frac{1}{3}\).
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