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- W1999282912 abstract "This article represents a first attempt at numerical simulation of the flow field around a complete lifting body configuration utilizing the Reynolds-averaged Navier-Stokes equations. The numerical solution generated for the experimental aircraft concept X24C-10D, at a Mach number of 5.95, exhibited accurate prediction of detailed flow properties and integrated areodynamic coefficients as well. In addition, the present analysis demonstrated that a vectorized processor with an external memory device is an efficient and viable means for processing the Navier-Stokes equations." @default.
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- W1999282912 date "1986-12-01" @default.
- W1999282912 modified "2023-10-17" @default.
- W1999282912 title "Navier-Stokes solution for a complete re-entry configuration" @default.
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- W1999282912 doi "https://doi.org/10.2514/3.45396" @default.
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