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- W2024147829 abstract "A rapid relaxation algorithm for the numerical solution of the conservative full potential equation is described and used to predict transonic potential flow past thick swept wings. A sheared parabolic coordinate system is used to simplify the treatment of boundary conditions and an upwind bias is applied to the density in supersonic regions. A unique feature of the present work is the extension of a strongly implicit procedure, that has, in the past, been applied only to elliptic equations, to the present elliptic-hyperbolic problem. Numerical results are presented to demonstrate that the present method is considerably faster than existing line relaxation procedures." @default.
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- W2024147829 date "1982-05-01" @default.
- W2024147829 modified "2023-09-25" @default.
- W2024147829 title "A Strongly Implicit Procedure for Steady Three-Dimensional Transonic Potential Flows" @default.
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- W2024147829 doi "https://doi.org/10.2514/3.51117" @default.
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