Effect of aerodynamic damping on flutter of thin panels
- 1 January 1964
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (1) , 119-120
- https://doi.org/10.2514/3.2233
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Flutter of Thin Plates under Combined Shear and Normal Edge ForcesAIAA 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
- Action of an Intermittent Beam of Radiant Heat Upon Gaseous Matter 1Nature, 1881