Supersonic Flow Control of Swept Shock Wave / Turbulent Boundary Layer Interactions using Plasma Actuators
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3479
Reference44 articles.
1. Progress in shock wave/boundary layer interactions
2. Interactions between shock waves and turbulent boundary layers
3. Unsteadiness in shock wave boundary layer interactions with separation
4. Shock Wave–Boundary-Layer Interactions
5. Micro-Vortex Generator Flow Control for Supersonic Engine Inlets
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1. Swept Fin-Induced Shock/Boundary-Layer Separation Control Using Corotating Vortex Generators;AIAA Journal;2022-11
2. Study on the mechanism of shock wave and boundary layer interaction control using high-frequency pulsed arc discharge plasma;Physics of Fluids;2022-08
3. Swept shock wave/boundary layer interaction control based on surface arc plasma;Physics of Fluids;2022-08
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