Experimental study on the hypersonic double incident shock wave/boundary layer interaction regulated by plasma actuation array

In the inlet passage of a hypersonic vehicle, multi-channel shock waves inevitably interact with the boundary layer, producing complex multi-channel shock wave/boundary layer interactions (SWBLIs). The flow separation caused by these interactions significantly decreases the intake efficiency and may...

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Veröffentlicht in:	Physics of fluids (1994) 2024-06, Vol.36 (6)
Hauptverfasser:	Yang, Hesen, Liang, Hua, Yang, Bo, Zong, Haohua, Li, Jinping, Zhang, Dongsheng, Xiong, Youde, Wu, Yun, Li, Yinghong
Format:	Artikel
Sprache:	eng
Schlagworte:	Actuation Arrays Boundary layer interaction Control methods Flow control Flow separation Frequency stability Hypersonic vehicles Intake systems Optimal control Plasma Shock wave interaction Shock waves
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