PIV Study on Forebody Vortex Cores under Plasma Actuations
Author:
Affiliation:
1. Northwestern Polytechnical University
2. University of California, Irvine
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1087
Reference12 articles.
1. Proportional Control of Asymmetric Forebody Vortices
2. An Innovative Control Technique for Slender Bodies at High Angle of Attack
3. Flow Control over a Conical Forebody Using Duty-Cycled Plasma Actuators
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Pressure Investigations over a Conical Forebody under Duty-Cycled Plasma Actuations;46th AIAA Plasmadynamics and Lasers Conference;2015-06-18
2. Flow Control over Conical Forebody with Port Pulsed Plasma Actuator;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
3. Momentum Transfer in Millisecond Periodic-Pulsed Dielectric-Barrier-Discharge Plasma Actuator;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
4. Flow Asymmetry over a Conical Forebody Under Plasma Actuation;5th Flow Control Conference;2010-06-28
5. Ensemble and Phase-Locked Averaged Loads Controlled by Plasma Duty Cycles;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
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