Formation Mechanism of Wall Jet Generated by Plasma Actuators in Quiescent Air
Author:
Affiliation:
1. China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China
2. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Funder
State Key Laboratory of Aerodynamics Foundation of China
National Natural Science Foundation of China
China Scholarship Council
Sichuan Science and Technology Program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061440
Reference61 articles.
1. Numerical Simulation of Direct Current Glow Discharges for High-Speed Flow Control
2. Multichannel Plasma Synthetic Jet Actuator Driven by Marx High-Voltage Generator
3. Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing Control
4. Experimental Study of Plasma Flow Control on Highly Swept Delta Wing
5. Numerical study of tip leakage flow control in turbine cascades using the DBD plasma model improved by the parameter identification method
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