Elastic stability of biaxially loaded longitudinally stiffened composite structures
- 20 March 1973
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Integration of Composite Structures into Aircraft DesignJournal of Composite Materials, 1972
- Numerical Results for the Initial Buckling of Some Stiffened Panels in CompressionAeronautical Quarterly, 1972
- Discussion of “Bounding of Frame Buckling Loads”Journal of the Structural Division, 1971
- Thin Shell TheoryPublished by Springer Nature ,1964