Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow
- 1 June 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (6) , 1090-1099
- https://doi.org/10.2514/3.49051
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Flutter analysis of composite panels using high-precision finite elementsComputers & Structures, 1989
- Nonlinear panel flutter using high-order triangular finite elementsAIAA Journal, 1983
- Flutter of Orthotropic Panels in Supersonic Flow Using Affine TransformationsAIAA Journal, 1983
- A Finite-Element Approach for Nonlinear Panel FlutterAIAA Journal, 1977
- Aeroelasticity of Plates and ShellsJournal of Applied Mechanics, 1976
- Finite-Element Analysis of Vibration and Flutter of Cantilever Anisotropic PlatesJournal of Applied Mechanics, 1974
- Perturbation and harmonic balance methods for nonlinear panel flutter.AIAA Journal, 1972
- Panel flutter - A review of the aeroelastic stability of plates and shellsAIAA Journal, 1970
- Theoretical considerations of panel flutter at high supersonic Mach numbers.AIAA Journal, 1966
- FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOWAIAA Journal, 1963