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A RootMeanSquare Approach for Predicting Fatigue Crack
MultiParameter Yield Zone Model for Predicting Spectrum Crack
Crack Growth Behavior of CenterCracked Panels under Random
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acceleration air-to-ground aluminum alloy American Society amplitude loading analytical predictions ASTM STP ASTM Task Group calculated CCT specimens compressive load constant-amplitude loading contact stresses crack growth behavior crack growth lives crack growth predictions crack growth rate crack growth retardation crack tip crack-opening stresses crack-surface displacements da/dN effective stress EFFGRO experimental fatigue crack growth Fighter A-G flight Flight Dynamics Fracture Mechanics fracture toughness growth rate constants growth rate data interac Kmax load cycles load history load interaction effects load interaction model maximum stress MPYZ overload retardation overload shut-off ratio parameters plane-stress plastic deformation plastic zone predict crack growth predict fatigue crack prediction ratio Random Loading random spectrum loadings range-pair counted rate equation retardation effects root-mean-square round-robin analysis simulated Society for Testing spectra stress levels stress-intensity factor range stress-intensity range tensile overload test data Testing and Materials typical fighter U.S. Customary units yield stress