A Crack-Closure Model for Predicting Fatigue Crack Growth under Aircraft Spectrum Loading
- 1 January 1981
- book chapter
- Published by ASTM International
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Dugdale crack closure analysis of fatigue cracks under constant amplitude loadingPublished by Elsevier ,2003
- Yielding of steel sheets containing slitsPublished by Elsevier ,2002
- A Finite-Element Analysis of Fatigue Crack ClosurePublished by ASTM International ,1976
- Spectrum Crack Growth Prediction Method Based on Crack Surface Displacement and Contact AnalysesPublished by ASTM International ,1976
- Fracture Analysis of Various Cracked Configurations in Sheet and Plate MaterialsPublished by ASTM International ,1976
- Cyclic analysis of a propagating crack and its correlation with fatigue crack growthEngineering Fracture Mechanics, 1975
- Elastic-Plastic Analysis of a Propagating Crack under Cyclic LoadingAIAA Journal, 1975
- The Significance of Fatigue Crack ClosurePublished by ASTM International ,1971