Dynamic Response of an Oblique Shock Wave Generated by a Q-DC Discharge in Pulse-Repetitive Mode
Author:
Affiliation:
1. University of Notre Dame
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3476
Reference16 articles.
1. Effects of Inlet Distortion on Cavity Ignition in Supersonic Flow
2. Control of mean separation in shock boundary layer interaction using pulsed plasma jets
3. Shock Wave Control by Nonequilibrium Plasmas in Cold Supersonic Gas Flows
4. Control of oblique shock wave/boundary layer interactions using plasma actuators
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