General Panel Sizing Computer Code and Its Application to Composite Structural Panels
- 1 August 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (8) , 892-897
- https://doi.org/10.2514/3.61242
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression PanelsAIAA Journal, 1976
- Analytical and experimental study of structurally efficient composite hat-stiffened panels loaded in axial compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadingsInternational Journal of Mechanical Sciences, 1974
- Structural optimization by methods of feasible directionsComputers & Structures, 1973