Flutter of simply supported, parallelogrammic, flat panels in supersonic flow.
- 1 September 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (9) , 1668-1673
- https://doi.org/10.2514/3.4266
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Theoretical considerations of panel flutter at high supersonic Mach numbers.AIAA Journal, 1966
- Some recent developments in flutter of flat panelsJournal of Aircraft, 1964
- A Note on the Supersonic Panel Flutter of Oblique Clamped PlatesJournal of the Royal Aeronautical Society, 1964
- Effect of aerodynamic damping on flutter of thin panelsAIAA Journal, 1964
- FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON THREE-DIMENSIONAL SUPERSONIC POTENTIAL FLOWAIAA Journal, 1963
- Flutter of Thin Plates under Combined Shear and Normal Edge ForcesAIAA Journal, 1963
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957