Hypersonic Conical Shock-Wave/Turbulent-Boundary-Layer Interaction at High Reynolds Number

A parametric study of hypersonic impinging conical-shock-wave/turbulent-boundary-layer interaction (CSBLI) is carried out at hypersonic high-Reynolds-number conditions (Mach number 6.0, Reδ2≈10,000, based on the freestream momentum boundary-layer thickness and wall viscosity) by means of numerical s...

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Veröffentlicht in:	AIAA journal 2023-09, Vol.61 (9), p.3743-3760
1. Verfasser:	Zuo, Feng-Yuan
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layer interaction Elastic waves Fluid flow Heat transfer High Reynolds number Mach number Oblique shock waves Reynolds averaged Navier-Stokes method Reynolds number Shock wave interaction Temperature effects Thickness Turbulent boundary layer Turbulent flow Wall temperature
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