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- W1996235461 abstract "A three dimensional fully viscous computer analysis was evaluated to determine its usefulness in the design of supersonic inlets. This procedure takes advantage of physical approximations to limit the high computer time and storage associated with complete Navier-Stokes solutions. Computed results are presented for a Mach 3.0 supersonic inlet with bleed and a Mach 7.4 hypersonic inlet. Good agreement was obtained between theory and data for both inlets. Results of a mesh sensitivity study are also shown." @default.
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- W1996235461 date "1980-01-14" @default.
- W1996235461 modified "2023-09-27" @default.
- W1996235461 title "Numerical simulation of supersonic inlets using a three-dimensional viscous flow analysis" @default.
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- W1996235461 doi "https://doi.org/10.2514/6.1980-384" @default.
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