Flutter of Thin Plates under Combined Shear and Normal Edge Forces
- 1 March 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (3) , 620-626
- https://doi.org/10.2514/3.54847
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Breathing Vibrations of a Partially Filled Cylindrical Tank—Linear TheoryJournal of Applied Mechanics, 1963
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- The Static Stability of a Two-Dimensional Curved Panel in a Supersonic Flow, with an Application to Panel FlutterJournal of the Aeronautical Sciences, 1954