Synthetic Jet Flow Separation Control for Thin Wing Fighter Aircraft
Author:
Affiliation:
1. Lockheed Martin Aeronautics Company
2. General Electric Global Research Center
3. NAVAIR/Flight Vehicle Performance
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-885
Reference8 articles.
1. Control of turbulent boundary-layer separation using micro-vortex generators
2. Active Flow Separation Control on Wall-Mounted Hump at High Reynolds Numbers
3. Active Control of Flow Separation from the Slat Shoulder of a Supercritical Airfoil
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