Rapid Calculation of Fatigue Crack Growth by Integration
- 1 January 1974
- book chapter
- Published by ASTM International
- p. 298-311
- https://doi.org/10.1520/stp38606s
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Preliminary Design of Aircraft Structures to Meet StructuralIntegrity RequirementsJournal of Aircraft, 1974
- Spectrum Loading and Crack GrowthJournal of Basic Engineering, 1972
- A Crack Growth Retardation Model Using an Effective Stress ConceptPublished by Defense Technical Information Center (DTIC) ,1971