Effects of angle of attack on transonic flutter of a supercritical wing
- 1 October 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (10) , 841-847
- https://doi.org/10.2514/3.44952
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Role of Shocks in the "Sub-Transonic" Flutter PhenomenonJournal of Aircraft, 1980
- Analysis of Supersonic-Hypersonic Flutter of Lifting Surfaces at Angle of AttackJournal of Aircraft, 1972
- Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.Journal of Aircraft, 1966