A stability criterion for panel flutter via the second method of Liapunov.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (1), 175-177
- https://doi.org/10.2514/3.3412
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Effect of Structural Damping on Panel FlutterAircraft Engineering and Aerospace Technology, 1960
- Some Panel-Flutter Studies Using Piston TheoryJournal of the Aerospace Sciences, 1958
- On the Aerodynamic Instability of Thin PanelsJournal of the Aeronautical Sciences, 1956