Use of Piezoelectric Actuators for Airfoil Separation Control
- 1 August 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 36 (8) , 1535-1537
- https://doi.org/10.2514/2.549
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Oscillatory control of separation and high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Delay of airfoil stall by periodic excitationJournal of Aircraft, 1996
- Exploratory study of vortex-generating devices for turbulent flow separation controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991