Fatigue life of panels with multiple site damage
- 1 September 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (5) , 1003-1013
- https://doi.org/10.2514/3.47047
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Stress intensity factors for some through-cracked fastener holesInternational Journal of Fracture, 1975