Aeroelastic oscillations caused by transitional boundary layers and their attenuation
- 1 July 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (7) , 463-469
- https://doi.org/10.2514/3.45502
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On measuring transonic dips in the flutter boundaries of a supercritical wing in the wind tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Wind-Tunnel Study of the Flutter Characteristics of a Supercritical WingJournal of Aircraft, 1982
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969