Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression Panels
- 1 November 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (11) , 1618-1626
- https://doi.org/10.2514/3.61497
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadingsInternational Journal of Mechanical Sciences, 1974