If a flat plate is going to be subjected to repeated tensile-compressive cycling in which the mean stress is 25MPa, estimate the maximum tensile stress to yield a fatigue life of 3.2*10+5 cycles. The initial and critical crack lengths are 0.25mm and 5mm respectively and m=4, Y= 2, and A= 5*10-15 (for which stress is in MPa and a is in m)
This question was answered on: May 23, 2022
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