Numerical investigation of nanosecond pulsed plasma actuators for control of shock-wave/boundary-layer separation
Author:
Affiliation:
1. Research and Development Directorate, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan
2. Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey 08544, USA
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5051823
Reference24 articles.
1. J. Delery and G. Marvin, “Shockwave boundary layer interactions,” AGARD-AG-280, North Atlantic Treaty Organization, Neuilly-Sur-Seine, France, 1986.
2. Structural characteristics of the shock-induced boundary layer separation extended to the leading edge
3. Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M=2.25
4. Control of Shock-Wave/Boundary-Layer Interaction Using Nanosecond-Pulsed Plasma Actuators
5. SDBD plasma actuator with nanosecond pulse-periodic discharge
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