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- W2066973295 abstract "Upwinding is incorporated into a numerical technique for predicting hypersonic viscous flows over lifting configurations at moderate angles of attack. A general real-gas flux-vector-splitting technique based on Van Leer's (1982) approach is employed to model upwinding, and three techniques are examined for flux-vector differencing. The three methods are evaluated by applying them to an axisymmetric configuration with a 10-deg afterbody flare. The results indicate that an oscillation-free shock front can be described by using first-order full upwinding across the embedded shock and central-differencing for the other zones. This combined approach is found to be highly convergent for the near-wall region, and its performance is examined for predicting a Mach 15 flow over a finned missile. Attention is given to the effects of gas chemistry which can significantly affect the flows over the missile configurations." @default.
- W2066973295 created "2016-06-24" @default.
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- W2066973295 date "1992-01-06" @default.
- W2066973295 modified "2023-09-26" @default.
- W2066973295 title "An improved PNS scheme for predicting complex three-dimensional hypersonic flows" @default.
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- W2066973295 doi "https://doi.org/10.2514/6.1992-753" @default.
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