Fatigue crack growth under spectrum loads: a symposium presented at the Seventy-eighth Annual Meeting, American Society for Testing and Materials, Montreal, Canada, 23-24 June, 1975, R. P. Wei and R. I. Stephens, symposium cochairmen
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Fatigue Crack Growth with Negative Stress Ratio Following
Effect of Single OverloadUnderload Cycles on Fatigue Crack
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Aa/AN Aircraft Structures AKeff AKth aluminum American Society amplitude analysis ASTM STP behavior block calculated constant constant-amplitude loading crack closure crack extension crack length crack surface crack tip crack-growth rates curve da/dN delay cycles Ducol effective stress Elber Engineering Fracture Mechanics experimental fail-safe Fatigue Crack Growth Fatigue Crack Propagation fatigue materials flight Flight Dynamics Fracture Toughness function gmax growth rate Growth Under Spectrum high loads Hillberry increase interaction effects Kmax Lehigh University load cycles load histories load sequence load spectra Man-Ten maximum mean stress measurements method number of cycles overload ratio parameters percent plane strain plane stress plastic deformation plastic zone precrack predictions residual strength residual stresses Schijve shown in Fig Society for Testing specimen Spectrum Loads steel stress cycles stress intensity factor stress intensity range stress range stress ratio tensile Testing and Materials thickness threshold values variable-amplitude loading variables versus yield strength yield stress