Unsteady supersonic aerodynamic forces on an oscillating circular cylindrical shell.
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (12) , 2358-2362
- https://doi.org/10.2514/3.6519
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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- Supersonic flutter of circular cylindrical heterogeneous orthotropic thin panels of finite lengthJournal of Sound and Vibration, 1968
- Circumferentially traveling wave flutter of a circular cylindrical shell.AIAA Journal, 1968
- Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraintPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Some aspects of cylindrical shell panel flutter.AIAA Journal, 1968
- Comparing theory and experiment for the supersonic flutter of circular cylindrical shells.AIAA Journal, 1967
- Flutter of infinitely long plates and shells. II - Cylindrical shell.AIAA Journal, 1966
- Supersonic flutter of circular cylindrical shells subjected to internal pressure and axial compression.AIAA Journal, 1966
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956