SEDL / STP / STP748-EB
STP748 Methods and Models for Predicting Fatigue Crack Growth Under Random Loading Chang JB, Hudson CM Pages: 146 Published: 1981
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This book describes the procedures used by various analysis groups to predict fatigue-crack growth under random loading. This aspect is important in the design, analysis, and test evaluation of a structure.
Table of Contents Introduction Hudson C. Summary Chang J. Round-Robin Crack Growth Predictions on Center-Cracked Tension Specimens under Random Spectrum Loading Chang J. A Root-Mean-Square Approach for Predicting Fatigue Crack Growth under Random Loading Hudson C. A Crack-Closure Model for Predicting Fatigue Crack Growth under Aircraft Spectrum Loading Newman J. Multi-Parameter Yield Zone Model for Predicting Spectrum Crack Growth Johnson W. Crack Growth Behavior of Center-Cracked Panels under Random Spectrum Loading Engle R., Rudd J. Random Spectrum Fatigue Crack Life Predictions With or Without Considering Load Interactions Chang J., Liu K., Szamossi M. Index Committee: E08 Paper ID: STP748-EB DOI: 10.1520/STP748-EB ISBN-EB: 978-0-8031-4814-7 ASTM International is a member of CrossRef. 0-8031-0715-3 978-0-8031-0715-1 STP748-EB