Role of boundary conditions on flutter of orthotropic panels.
- 1 July 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (7), 1241-1248
- https://doi.org/10.2514/3.3655
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.AIAA Journal, 1965
- Some recent developments in flutter of flat panelsJournal of Aircraft, 1964
- On the Aeroelastic Stability of Orthotropic Panels in Supersonic FlowJournal of the Aerospace Sciences, 1962