Preliminary Design of Aircraft Structures to Meet StructuralIntegrity Requirements
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (3) , 136-143
- https://doi.org/10.2514/3.60338
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Engineering Criteria and Analysis Methodology for the Appraisal of Potential Fracture Resistant Primary Aircraft StructurePublished by Defense Technical Information Center (DTIC) ,1972
- An Approach to Predicting the Growth to Failure of Fatigue Cracks Subjected to Arbitrary Uniaxial Cyclic LoadingPublished by ASTM International ,1971
- Fatigue Crack Propagation in Stiffened PanelsPublished by ASTM International ,1971