Stiffness design method of symmetric laminates using lamination parameters
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (11), 2791-2793
- https://doi.org/10.2514/3.11304
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Layup optimization against buckling of shear panelsStructural and Multidisciplinary Optimization, 1991
- Stiffness Optimization of Orthotropic Laminated Composites Using Lamination ParametersAIAA Journal, 1991