Sliding discharge plasma actuation for forebody vortex control on a slender body at high angles of attack
Author:
Affiliation:
1. Xi’an University of Technology, Xi’an, Shaanxi 710048, China
2. Northwestern Polytechnical University, Xi’an 710072, China
Funder
National Natural Science Foundation of China
Foundation for Key Laboratories of National Defense Science and Technology
Shaanxi Natural Science Basic Research Program
Xi’an Science and Technology Project
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0005366
Reference22 articles.
1. Sources of High Alpha Vortex Asymmetry at Zero Sideslip
2. Continuous control of asymmetric forebody vortices in a bi-stable state
3. Asymmetric Vortices on a Slender Body of Revolution
4. Recent progress on the study of asymmetric vortex flow over slender bodies
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1. Experimental Study on the Working Characteristics of Tri-Electrode Plasma Actuator Utilizing a Combination of Corona and Barrier Discharges;Actuators;2022-11-07
2. Sliding discharge plasma jet actuators for circular-cylinder wake modification;Modern Physics Letters B;2022-09-10
3. Adaptive Compensation at High Angles of Attack;Adaptive Compensation of Nonlinear Actuators for Flight Control Applications;2021-07-23
4. Effects of plasma kinetic modeling on performance characterization of plasma actuators for active flow control;E3S Web of Conferences;2020
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