Chapter 8: Problem 24
Briefly explain the difference between fatigue striations and beachmarks both in terms of (a) size and (b) origin.
Chapter 8: Problem 24
Briefly explain the difference between fatigue striations and beachmarks both in terms of (a) size and (b) origin.
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Get started for freeCite five factors that may lead to scatter in fatigue life data.
Cite three metallurgical/processing techniques that are employed to enhance the creep resistance of metal alloys.
List four measures that may be taken to increase the resistance to fatigue of a metal alloy.
Suppose that a wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of \(26 \mathrm{MPa} \sqrt{\mathrm{m}}\) \((23.7 \mathrm{ksi} \sqrt{\mathrm{in.}}) .\) It has been determined that fracture results at a stress of \(112 \mathrm{MPa}\) \((16,240 \text { psi })\) when the maximum internal crack length is \(8.6 \mathrm{mm}(0.34 \text { in. }) .\) For this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of \(6.0 \mathrm{mm}(0.24\) in.)
Steady-state creep data taken for an iron at a stress level of \(140 \mathrm{MPa}(20,000 \mathrm{psi})\) are given here $$\begin{array}{cc}\hline \dot{\epsilon}_{s}\left(h^{-1}\right) & T(K) \\\\\hline 6.6 \times 10^{-4} & 1090 \\\8.8 \times 10^{-2} & 1200 \\\\\hline\end{array}.$$ If it is known that the value of the stress exponent \(n\) for this alloy is \(8.5,\) compute the steady-state creep rate at \(1300 \mathrm{K}\) and a stress level of 83 MPa \((12,000 \text { psi })\).
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