Flutter of Orthotropic Panels in Supersonic Flow Using Affine Transformations
- 1 February 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (2) , 283-289
- https://doi.org/10.2514/3.60111
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Theoretical considerations of panel flutter at high supersonic Mach numbers.AIAA Journal, 1966
- Flutter of a flat panel subjected to a nonlinear temperature distribution.AIAA Journal, 1965
- Effect of aerodynamic damping on flutter of thin panelsAIAA Journal, 1964
- FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOWAIAA Journal, 1963
- On the Aeroelastic Stability of Orthotropic Panels in Supersonic FlowJournal of the Aerospace Sciences, 1962
- On Two-Dimensional Panel FlutterJournal of the Aerospace Sciences, 1958