Nonlinear flutter of orthotropic composite panel under aerodynamic heating
- 16 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- The Static Stability of a Two-Dimensional Curved Panel in a Supersonic Flow, with an Application to Panel FlutterJournal of the Aeronautical Sciences, 1954