A general panel sizing computer code and its application to composite structural panels
- 3 April 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 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