Flutter of Flat Finite Element Panels in a Supersonic Potential Flow
- 1 November 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (11) , 1502-1507
- https://doi.org/10.2514/3.60562
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Comparison of theory and experiment for nonlinear flutter of loaded platesAIAA Journal, 1970
- Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flowAIAA Journal, 1970
- Some flutter solutions using finite elementsAIAA Journal, 1970
- Application of matrix displacement methods in the study of panel flutter.AIAA Journal, 1969
- Finite elements applied to panel flutter.AIAA Journal, 1967
- Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.AIAA Journal, 1965