Effect of Boundary-Conditions in Shock-Wave/Turbulent-Boundary-Layer Interaction Computations

2003 ◽  
Author(s):  
G. Gerolymos ◽  
E. Sauret ◽  
I. Vallet
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Turbulent Boundary Layer ◽  
Boundary Conditions ◽  
Layer Interaction ◽  
Boundary Layer Interaction

Letter: Görtler-like vortices in an impinging shock wave/turbulent boundary layer interaction flow

2018 ◽  
Vol 30 (6) ◽  
pp. 061702 ◽  
Author(s):  
Yi Zhuang ◽  
Hui-jun Tan ◽  
Xin Li ◽  
Fa-jia Sheng ◽  
Yu-chao Zhang
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Turbulent Boundary Layer ◽  
Layer Interaction ◽  
Boundary Layer Interaction

scholarly journals A Study on the Separation Length of Shock Wave/Turbulent Boundary Layer Interaction

2019 ◽  
Vol 2019 ◽  
pp. 1-10 ◽  
Author(s):  
Yong-yi Zhou ◽  
Yi-long Zhao ◽  
Yu-xin Zhao
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Turbulent Boundary Layer ◽  
Incident Shock ◽  
Computational Domain ◽  
Layer Interaction ◽  
Flow Parameters ◽  
Boundary Layer Interaction ◽  
High Mach ◽  
Wave Boundary

The separation length of shock wave/boundary layer interaction (SWBLI) was studied by a numerical method, which was validated by experimental results. The computational domain was two-dimensional (2-D). The flow field was an incident oblique shock interacting with a turbulent boundary layer on a flat adiabatic plate. According to the simulation data, the dependency of the separation length on the relevant flow parameters, such as the incident shock strength, Reynolds number, and Mach number, was analyzed in the range of 2≤M≤7. Based on the relations with the flow parameters, two models of the separation length at low and high Mach numbers were proposed, respectively, which can be used to predict the extent of the separation in the SWBLI.

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