Role of Shocks in the "Sub-Transonic" Flutter Phenomenon
- 1 March 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (3) , 187-197
- https://doi.org/10.2514/3.57891
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Transonic Flow about a Thick Circular-Arc AirfoilAIAA Journal, 1976
- Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.Journal of Aircraft, 1966