The use of crack size distribution and crack detection for determining the probability of fatigue failure
- 17 April 1974
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Fracture toughness and ndt requirements for aircraft designNon-Destructive Testing, 1973
- FRACTURE MECHANICS GUIDELINES FOR AIRCRAFT STRUCTURAL APPLICATIONSPublished by Defense Technical Information Center (DTIC) ,1970
- Numerical Analysis of Crack Propagation in Cyclic-Loaded StructuresJournal of Basic Engineering, 1967