Design for global damage tolerance and associated mass penalties
- 1 January 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (1), 83-88
- https://doi.org/10.2514/3.44832
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Low‐velocity impact damage in graphite‐fiber reinforced epoxy laminatesPolymer Composites, 1981
- Preliminary Design of Composite Wings for Buckling, Strength, and Displacement ConstraintsJournal of Aircraft, 1979
- DANGERS OF STRUCTURAL OPTIMIZATIONEngineering Optimization, 1974