1. Scaling of interaction lengths for hypersonic shock wave/turbulent boundary layer interactions
- Author
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Yuting Hong, Jiming Yang, and Zhufei Li
- Subjects
Shock wave ,0209 industrial biotechnology ,Hypersonic speed ,Interaction length ,Aerospace Engineering ,02 engineering and technology ,01 natural sciences ,010305 fluids & plasmas ,Physics::Fluid Dynamics ,symbols.namesake ,020901 industrial engineering & automation ,Shock wave/turbulent boundary layer interactions ,0103 physical sciences ,Supersonic speed ,Physics::Chemical Physics ,Scaling ,Separation criterion ,Motor vehicles. Aeronautics. Astronautics ,Physics ,Scaling laws ,Turbulence ,Mechanical Engineering ,Reynolds number ,TL1-4050 ,Mechanics ,Boundary layer ,Hypersonic flow ,Mach number ,symbols - Abstract
The interaction length induced by Shock Wave/Turbulent Boundary-Layer Interactions (SWTBLIs) in the hypersonic flow was investigated using a scaling analysis, in which the interaction length normalized by the displacement thickness of boundary layer was correlated with a corrected non-dimensional separation criterion across the interaction after accounting for the wall temperature effects. A large number of hypersonic SWTBLIs were compiled to examine the scaling analysis over a wide range of Mach numbers, Reynolds numbers, and wall temperatures. The results indicate that the hypersonic SWTBLIs with low Reynolds numbers collapse on the supersonic SWTBLIs, while the hypersonic cases with high Reynolds numbers show a more rapid growth of the interaction length than that with low Reynolds numbers. Thus, two scaling relationships are identified according to different Reynolds numbers for the hypersonic SWTBLIs. The scaling analysis provides valuable guidelines for engineering prediction of the interaction length, and thus, enriches the knowledge of hypersonic SWTBLIs.
- Published
- 2021