Some aspects of cylindrical shell panel flutter.
- 1 January 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (1) , 37-43
- https://doi.org/10.2514/3.4438
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Supersonic wind-tunnel tests of wavy-walled cylinders.AIAA Journal, 1967
- Generalized aerodynamic forces on an oscillating cylindrical shellQuarterly of Applied Mathematics, 1966
- THE ACCURACY OF LINEAR PISTON THEORY WHEN APPLIED TO CYLINDRICAL SHELLSAIAA Journal, 1963
- On the Numerical Solution of Characteristic Equations in Flutter AnalysisJournal of the ACM, 1958