Evaluation of Crack Growth Models for Elevated-Temperature Fatigue
- 1 January 1988
- book chapter
- Published by ASTM International
- p. 206-220
- https://doi.org/10.1520/stp23243s
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Evaluation of cumulative damage models for fatigue crack growth in an aircraft engine alloyJournal of Propulsion and Power, 1985
- A Model for Creep/Fatigue Interactions in Alloy 718Published by ASTM International ,1985