Experimental Investigation on the Control of Hypersonic Shock Wave/Boundary Layer Interaction Using Surface Arc Plasma Actuators at Double Compression Corner

Experimental Investigation on the Control of Hypersonic Shock Wave/Boundary Layer Interaction Using Surface Arc Plasma Actuators at Double Compression Corner

Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In previous studies, the separation flow is usually caused by a single shock wave. However, in the actual aircraft surface configuration...

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Bibliographic Details
Main Authors: Bo Yang, Hesen Yang, Chuanbiao Zhang, Ning Zhao, Hua Liang, Dongsheng Zhang
Format: Article
Language:English
Published: MDPI AG 2023-12-01
Series:Aerospace
Subjects:
hypersonic
double compression corner
shock wave/boundary interaction
plasma actuation
flow control
Online Access:https://www.mdpi.com/2226-4310/10/12/1016

Internet

https://www.mdpi.com/2226-4310/10/12/1016

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