Problems with Leading-Edge Flow Control Experiments
Author:
Affiliation:
1. The University of Manchester, Manchester, M30 7RU England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.29240
Reference20 articles.
1. Effect of Leading-Edge Curvature on Airfoil Separation Control
2. Delay of airfoil stall by periodic excitation
3. Effect of Piezoelectric Actuation on a NACA 0015 Aerofoil at Subsonic Speeds
4. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
5. Oscillatory control of separation and high Reynolds numbers
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1. Flow Separation Control over a Thin Post-Stall Airfoil: Effects of Excitation Frequency;AIAA Journal;2019-05
2. Flow Separation Control over a Boeing Vertol VR-7 using NS-DBD Plasma Actuators;54th AIAA Aerospace Sciences Meeting;2016-01-02
3. CFD simulation of momentum injection control past a streamlined body;International Journal of Numerical Methods for Heat & Fluid Flow;2011-11
4. Dielectric-Barrier Discharge Plasmas for Flow Control at higher Mach Numbers;5th Flow Control Conference;2010-06-28
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