Optimization of Buckling and Yield Strengths of Laminated Composites
- 1 September 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (9), 1131-1132
- https://doi.org/10.2514/3.60515
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Strength Optimization for Cylindrical Shells of Laminated CompositesJournal of Composite Materials, 1975
- Anisotropic Plate Analysis-Boundary ConditionsJournal of Composite Materials, 1970
- Strength of laminated composite materials.AIAA Journal, 1966