Flow Control in Supersonic-Cavity-Based Airflow by Quasi-Direct-Current Electric Discharge
Author:
Affiliation:
1. UES, Inc., Dayton, Ohio 45432
Funder
Innovative Scientific Solutions Inc.
Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058057
Reference19 articles.
1. Effects of Inlet Distortion on Cavity Ignition in Supersonic Flow
2. Characterization of Transient Operation of a Quasi-DC Electrical Discharge in Supersonic Flow
3. Near-Surface Electrical Discharge in Supersonic Airflow: Properties and Flow Control
4. Control of separation phenomena in a high-speed flow by means of the surface electric discharge
5. Mechanisms of Flow Control by Near-Surface Electrical Discharge Generation
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