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- W2094133397 abstract "A nonlinear method based on the full potential equation in conservation form, cast in an arbitrary coordinate system, has been developed to treat predominantly supersonic flows with embedded subsonic regions. This type of flow field occurs frequently near the fuselage-canopy junction area and wing leading edge regions for a moderately swept fighter configuration. The method uses the theory of characteristics to accurately monitor the type-dependent flow field. A conservative switching scheme is developed to transition from the supersonic marching algorithm to a subsonic relaxation procedure, and vice versa. An implicit approximate factorization scheme is employed to solve the finite-differenced equation. Results are shown for a few configurations, including a wing-body-wake realistic fighter model having embedded subsonic regions." @default.
- W2094133397 created "2016-06-24" @default.
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- W2094133397 date "1983-07-13" @default.
- W2094133397 modified "2023-09-26" @default.
- W2094133397 title "A conservative type-dependent full potential method for the treatment of supersonic flows with embedded subsonic regions" @default.
- W2094133397 cites W2072086438 @default.
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- W2094133397 doi "https://doi.org/10.2514/6.1983-1887" @default.
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