Chapter 8: Problem 45
Cite three metallurgical/processing techniques that are employed to enhance the creep resistance of metal alloys.
Chapter 8: Problem 45
Cite three metallurgical/processing techniques that are employed to enhance the creep resistance of metal alloys.
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Get started for freeA specimen of a 4340 steel alloy with a plane strain fracture toughness of \(54.8 \mathrm{MPa} \sqrt{\mathrm{m}}(50 \mathrm{ksi} \sqrt{\mathrm{in}}\).) is exposed to a stress of \(1030 \mathrm{MPa}\) (150,000 psi). Will this specimen experience fracture if the largest surface crack is \(0.5 \mathrm{~mm}\) (0.02 in.) long? Why or why not? Assume that the parameter \(Y\) has a value of \(1.0 .\)
(a) Using Figure 8.31, compute the rupture lifetime for an \(S-590\) alloy that is exposed to a tensile stress of \(400 \mathrm{MPa}\) at \(815^{\circ} \mathrm{C}\). (b) Compare this value to the one determined from the Larson-Miller plot of Figure \(8.33\), which is for this same S-590 alloy.
An aircraft component is fabricated from an aluminum alloy that has a plane- strain fracture toughness of \(40 \mathrm{MPa} \sqrt{\mathrm{m}}\) (36.4 ksi \sqrt{in.). It has been deter- } mined that fracture results at a stress of \(300 \mathrm{MPa}\) (43,500 psi) when the maximum (or critical) internal crack length is \(4.0 \mathrm{~mm}\) (0.16 in.). For this same component and alloy, will fracture occur at a stress level of \(260 \mathrm{MPa}\) ( 38,000 psi) when the maximum internal crack length is \(6.0 \mathrm{~mm}(0.24\) in.) \(?\) Why or why not?
List four measures that may be taken to increase the resistance to fatigue of a metal alloy.
What is the maximum carbon content possible for a plain carbon steel that must have an impact energy of at least \(200 \mathrm{~J}\) at \(-50^{\circ} \mathrm{C} ?\)
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