SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCH
- 1 April 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (4) , 898-909
- https://doi.org/10.2514/3.1661
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical ShellsJournal of the Aerospace Sciences, 1961
- Supersonic Panel Flutter of a Cylindrical Shell of Finite LengthJournal of the Aerospace Sciences, 1961
- On Panel Flutter in the Presence of a Boundary LayerJournal of the Aerospace Sciences, 1959
- On the Vibration of Thin Cylindrical Shells Under Internal PressureJournal of the Aeronautical Sciences, 1957
- Supersonic Flutter of a Cylindrical ShellJournal of the Aeronautical Sciences, 1957
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- On the Aerodynamic Instability of Thin PanelsJournal of the Aeronautical Sciences, 1956
- Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 1953
- The Aerodynamic Forces on an Oscillating Airfoil at Supersonic SpeedsJournal of the Aeronautical Sciences, 1947