Optimal Design of Composite-Material Panels for Business Aircraft
- 1 February 1977
- proceedings article
- Published by SAE International in SAE International Journal of Advances and Current Practices in Mobility
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Lamination Residual Strains and Stresses in Hybrid LaminatesPublished by ASTM International ,1977
- Optimal design of a composite-material plate to maximize its fundamental frequencyJournal of Sound and Vibration, 1977
- Analysis and design methods for composite structures - Overly intimidatingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Structural Cost Effectiveness of CompositesPublished by SAE International ,1973
- Role of boundary conditions on flutter of orthotropic panels.AIAA Journal, 1966
- Bending and Stretching of Certain Types of Heterogeneous Aeolotropic Elastic PlatesJournal of Applied Mechanics, 1961