OSCILLATORY PRESSURES IN AN IDEALIZED BOUNDARY LAYER WITH AN APPLICATION TO THE PANEL FLUTTER OF CYLINDRICAL SHELLS
- 16 August 1965
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCHAIAA Journal, 1963
- The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical ShellsJournal of the Aerospace Sciences, 1961
- On Panel Flutter in the Presence of a Boundary LayerJournal of the Aerospace Sciences, 1959
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- On Some Special Problems in Linearized Axially Symmetric FlowJournal of the Aeronautical Sciences, 1951