Netting theory and its application to optimum design of laminated composite plates and shells
- 18 April 1988
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- On Isotropic Laminate ConfigurationsJournal of Composite Materials, 1990
- Optimal laminate configurations of cylindrical shells for axial bucklingAIAA Journal, 1985
- Optimal laminated composite shells for buckling and vibrationAIAA Journal, 1983
- A Note on Specially Orthotropic LaminatesJournal of Composite Materials, 1982
- Optimum Design of Laminated Plates under Axial CompressionAIAA Journal, 1979
- Optimal design of a composite-material plate to maximize its fundamental frequencyJournal of Sound and Vibration, 1977