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- W2993643976 abstract "Three higher-order turbulence models—the low-Reynolds-number form of a standard two-equation model, the two-layer algebraic stress model, and the Reynolds-stress model—are combined with Navier-Stokes equations to compute the supersonic flows behind a missile-type afterbody and two-dimensional two-stream flow behind a thick base. The governing equations are numerically solved by an implicit total variation diminishing algorithm for high accuracy. The preconditioned bi-conjugate-gradient stable scheme is also employed to accelerate and stabilize the convergence. Those results demonstrate that the Reynolds-stress model is better than the other two models in predicting the mean flow, turbulent quantities, and surface pressure distribution in the recirculating regions/Nevertheless, improvements in the Reynolds-stress model are suggested so as to more accurately predict the turbulent properties of shock-shear-layer interaction around the recompression region. All three turbulence models fail to achieve a sufficient velocity recovery rate in the redevelopment region of a supersonic base flow." @default.
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- W2993643976 date "1996-01-15" @default.
- W2993643976 modified "2023-09-26" @default.
- W2993643976 title "Supersonic base flow computation using higher order closure turbulence models" @default.
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- W2993643976 doi "https://doi.org/10.2514/6.1996-566" @default.
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