Momentum Transfer in Millisecond Periodic-Pulsed Dielectric-Barrier-Discharge Plasma Actuator
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/10.2514/6.2011-739
Reference8 articles.
1. Proportional Control of Asymmetric Forebody Vortices
2. Investigations on a dynamic forebody flow control system
3. An Innovative Control Technique for Slender Bodies at High Angle of Attack
4. Flow Control over a Conical Forebody Using Duty-Cycled Plasma Actuators
5. Mechanisms for Conical Forebody Flow Control Using Plasma Actuators
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1. Research on Aerodynamic Flow Acceleration Induced by One Atmosphere Uniform DBD Plasma Based on PIV;Advanced Materials Research;2013-09
2. Study of the Boundary Layer on a Plate Aerodynamically Induced by Multiple DBD Plasma Based on PIV;Applied Mechanics and Materials;2013-09
3. Aerodynamic Flow Acceleration with One Atmosphere Uniform Induced by Single and Multiple DBD Plasma Actuation Based on PIV;43rd Fluid Dynamics Conference;2013-06-22
4. Body Force Produced by a SDBD Plasma Actuator Using PIV Measurement;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
5. Pulsed-Discharge Flow Control over a Conical Forebody;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
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