Control of SWBLI in a 24deg Compression Ramp Flow with Air-jet Vortex-generator
Author:
Affiliation:
1. Rheinisch-Westfalische Technische Hochschule Aachen
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-2138
Reference77 articles.
1. Unsteadiness of shock-induced turbulent separated flows - Some key questions
2. Micro-Vortex Generator Flow Control for Supersonic Engine Inlets
3. Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield
4. Shock wave boundary layer interaction
5. Space and time organization in a shock-induced separated boundary layer
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1. Experimental Investigation on the Control of Hypersonic Shock Wave/Boundary Layer Interaction Using Surface Arc Plasma Actuators at Double Compression Corner;Aerospace;2023-12-06
2. A review of three-dimensional shock wave–boundary-layer interactions;Progress in Aerospace Sciences;2023-11
3. Forced Control of SWBLI in a 24deg Compression Ramp Flow with Air-jet Vortex-generator;AIAA AVIATION 2023 Forum;2023-06-08
4. Numerical simulation of mini-air-jet vortex generators on a supercritical wing in transonic flow and the effect of temperature on its aerodynamic performance;Aerospace Systems;2023-05-25
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