NASA NTRS ยท 19950013068
Fatigue crack growth under variable amplitude loading
Abstract
Fatigue crack growth tests were conducted on an Fe 510 E C-Mn steel and a submerged arc welded joint from the same material under constant, variable, and random loading amplitudes. Paris-Erdogan's crack growth rate law was tested for the evaluation of m and C using the stress intensity factor K, the J-integral, the effective stress intensity factor K(sub eff), and the root mean square stress intensity factor K(sub rms) fracture mechanics concepts. The effect of retardation and residual stresses resulting from welding was also considered. It was found that all concepts gave good life predictions in all cases.
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Sidawi, Jihad A.. 1994-09-01. Fatigue crack growth under variable amplitude loading. https://ntrs.nasa.gov/citations/19950013068
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