Nonlinear flutter of orthotropic composite panel under aerodynamic heating
- 1 August 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (8), 1478-1488
- https://doi.org/10.2514/3.11798
Abstract
No abstract availableKeywords
This 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