The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells
- 1 December 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (12) , 945-956
- https://doi.org/10.2514/8.9264
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- On the Vibration of Thin Cylindrical Shells Under Internal PressureJournal of the Aeronautical Sciences, 1957
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Supersonic Flutter of a Cylindrical ShellJournal of the Aeronautical Sciences, 1957
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- An experimental investigation of the interaction between shock waves and boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1954
- Generalized Aerodynamic Forces on the Delta Wing with Supersonic Leading EdgesJournal of the Aeronautical Sciences, 1954
- Tables for Frequencies and Modes of Free Vibration of Infinitely Long Thin Cylindrical ShellsJournal of Applied Mechanics, 1954