Joint aircraft loading/structure response statistics of time to service crack initiation
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (4) , 270-278
- https://doi.org/10.2514/3.44524
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Reliability Analysis of Aircraft Structures under Random Loading and Periodic InspectionAIAA Journal, 1974
- Development of Titanium and Steel Fatigue Variability Model for Application of Reliability Analysis Approach to Aircraft StructuresPublished by Defense Technical Information Center (DTIC) ,1972