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NASA NTRS · 19950065432

Predicting Fatigue Lives Under Complex Loading Conditions

Abstract

Cyclic Damage Accumulation (CDA) computer program performs high-temperature, low-cycle-fatigue life prediction for materials analysis. Designed to account for effects on creep-fatigue life of complex loadings involving such factors as thermomechanical fatigue, hold periods, wave-shapes, mean stresses, multiaxiality, cumulative damage, coatings, and environmental attack. Several features practical for application to actual component analysis using modern finite-element or boundary-element methods. Although developed for use in predicting crack-initiation lifetimes of gas-turbine-engine materials, also applied to other materials as well. Written in FORTRAN 77.

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BibTeXRIS

Mcgaw, Michael A., Nelson, R. S., Janitor, L. A.. 1995-06-01. Predicting Fatigue Lives Under Complex Loading Conditions. https://ntrs.nasa.gov/citations/19950065432

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