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Predicting Fatigue Lives Under Complex Loading ConditionsCyclic 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.
Document ID
19950065432
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcgaw, Michael A.
(NASA Lewis Research Center, Cleveland, OH.)
Nelson, R. S.
(United Technologies Corp.)
Janitor, L. A.
(United Technologies Corp.)
Date Acquired
August 17, 2013
Publication Date
June 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 6
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15965
Accession Number
95B10273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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