Theoretical considerations of panel flutter at high supersonic Mach numbers.
- 1 July 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (7) , 1257-1266
- https://doi.org/10.2514/3.3657
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.AIAA Journal, 1965
- THEORETICAL CONSIDERATIONS OF PANEL FLUTTER AT HIGH SUPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1965
- Pure bending flutter of a swept wing in a high- density, low-speed flowAIAA Journal, 1965
- Some recent developments in flutter of flat panelsJournal of Aircraft, 1964
- FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOWAIAA Journal, 1963
- 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
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- On the Concept of Elastic StabilityPublished by Elsevier ,1956