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- W2116770781 abstract "Abstract M = 2.25 shock‐wave/turbulent‐boundary‐layer interactions over a compression ramp for several angles (8, 13 and 18°) at Reynolds‐number Re =7 × 10 3 were simulated with three low‐Reynolds second‐moment closures and a linear low‐Reynolds standard k –ε model. A detailed assessment of the turbulence closures by comparison with both mean‐flow and turbulent experimental quantities is presented. The Reynolds‐stress model which is wall‐topology free and which uses an optimized redistribution closure, is in good agreement with experimental data both for wall‐pressure and mean‐velocity profiles. Detailed analysis of three components of the Reynolds‐stress tensor (comparison with measurements and transport‐equation budgets) provides a critical evaluation of full Reynolds‐stress models for the separated supersonic compression ramp. The discrepancy observed in the shock‐wave foot region, between computations and measurements for the Reynolds‐stresses profiles, could be explained by considering the experimental shock‐wave oscillation and directions for future modelling work are indicated. Copyright © 2007 John Wiley & Sons, Ltd." @default.
- W2116770781 created "2016-06-24" @default.
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- W2116770781 date "2007-07-24" @default.
- W2116770781 modified "2023-10-15" @default.
- W2116770781 title "Reynolds-stress modelling ofM = 2.25 shock-wave/turbulent boundary-layer interaction" @default.
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- W2116770781 doi "https://doi.org/10.1002/fld.1540" @default.
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