1. Three-dimensional supersonic flow around double compression ramp with finite span
- Author
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Yung-Hwan Byun, Gi-Jung Park, Joong-Bok Lee, Seung-Hwa Park, and Hyun-Il Lee
- Subjects
Physics ,020301 aerospace & aeronautics ,Supersonic wind tunnel ,Mechanical Engineering ,General Physics and Astronomy ,02 engineering and technology ,Mechanics ,Solver ,01 natural sciences ,010305 fluids & plasmas ,Physics::Fluid Dynamics ,Boundary layer ,symbols.namesake ,0203 mechanical engineering ,Mach number ,0103 physical sciences ,Double compression ,symbols ,Shadowgraph ,Choked flow ,Leakage (electronics) - Abstract
Three-dimensional flows of Mach number 3 around a double-compression ramp with finite span have been investigated numerically. Shadowgraph visualisation images obtained in a supersonic wind tunnel are used for comparison. A three-dimensional Reynolds-averaged Navier–Stokes solver was used to obtain steady numerical solutions. Two-dimensional numerical results are also compared. Four different cases were studied: two different second ramp angles of $${30}^{\circ }$$ and $${45}^{\circ }$$ in configurations with and without sidewalls, respectively. Results showed that there is a leakage of mass and momentum fluxes heading outwards in the spanwise direction for three-dimensional cases without sidewalls. The leakage changed the flow characteristics of the shock-induced boundary layer and resulted in the discrepancy between the experimental data and two-dimensional numerical results. It is found that suppressing the flow leakage by attaching the sidewalls enhances the two-dimensionality of the experimental data for the double-compression ramp flow.
- Published
- 2016
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