Vortex Shedding Frequency Scaling of Coherent Structures Induced by a Plasma Actuator
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China
2. Science and Technology on Plasma Dynamics Laboratory, 710038 Xi’an, People’s Republic of China
Funder
CARDC Fundamental and Frontier Technology Research Fund
State Key Laboratory of Aerodynamics Foundation of China
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060903
Reference76 articles.
1. PoggieJ. “High-Order Compact Difference Methods for Glow Discharge Modeling,” AIAA Paper 2009-1047, June 2009. 10.2514/6.2009-1047
2. Dynamics and control of the vortex flow behind a slender conical forebody by a pair of plasma actuators
3. 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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