Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds
- 1 August 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (8) , 563-573
- https://doi.org/10.2514/8.3908
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- A First-Order Formulation of the Unsteady Supersonic Flow Problem for Finite WingsJournal 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
- Analysis of Flutter in Compressible Flow of a Panel on Many SupportsJournal of the Aeronautical Sciences, 1954
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949