Forced Flow Reattachment Process and the Effect of Pressure Gradient
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, New York 12180
Funder
New York State Energy Research and Development Authority
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J058175
Reference33 articles.
1. Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators
2. Aerodynamic Flow Control Using Synthetic Jet Actuators
3. Actuators for Active Flow Control
4. Helicopter Fuselage Drag Reduction Using Active Flow Control: A Comprehensive Experimental Investigation
5. Aerodynamic flow control for a generic truck cabin using synthetic jets
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