Finite-element panel flutter in three-dimensional supersonic unsteady potential flow
- 1 December 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (12) , 1677-1683
- https://doi.org/10.2514/3.7472
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Aeroelasticity of Plates and ShellsJournal of Applied Mechanics, 1976
- Flutter of Flat Finite Element Panels in a Supersonic Potential FlowAIAA Journal, 1975
- Finite element analysis of Supersonic panel flutterInternational Journal for Numerical Methods in Engineering, 1973
- 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
- Kinematically consistent unsteady aerodynamic coefficients in supersonic flowInternational Journal for Numerical Methods in Engineering, 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