Influence of Subsonic Potential Flow on the Buckling of Thin Panels under Edge Compression
- 1 January 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (1) , 106-107
- https://doi.org/10.2514/3.49639
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Static and dynamic instability of panels and cylindrical shells in subsonic potential flowJournal of Sound and Vibration, 1974
- Analogie zwischen beulenden und flatternden PlattenActa Mechanica, 1972
- Model for mixing of a compressible free jet with a moving environment.AIAA Journal, 1967
- Aeroelastic instabilities of simply supported panels in subsonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Normal shock location in underexpanded gas and gas-particle jetsAIAA Journal, 1964