Optimal laminated composite shells for buckling and vibration
- 1 March 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (3) , 430-437
- https://doi.org/10.2514/3.8090
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Improved Methods for Large Scale Structural SynthesisAIAA Journal, 1981
- Buckling of Shells-Pitfall for DesignersAIAA Journal, 1981
- Optimal design of laminated composite shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Optimum structural design with plate bending elements - A surveyAIAA Journal, 1981
- Optimum Design of Laminated Plates under Axial CompressionAIAA Journal, 1979
- Optimal frequency separation of cylindrical shellsAIAA Journal, 1978
- Optimum Design of Composite Structures with Stress and Displacement ConstraintsAIAA Journal, 1976
- Optimization of ring stiffened cylindrical shellsAIAA Journal, 1975
- A discrete search procedure for the minimization of stiffened cylindrical shell stability equationsAIAA Journal, 1970