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- W2022804540 abstract "The classical problem of steady inviscid plane subsonic flow past an aerofoil is formulated as a variational principle, the Bateman-Dirichlet Principle. A finite difference method is used to calculate approximations to the extremals for flow past ellipses and Karman-Trefftz profiles of different thickness ratios. The obtained solutions for the ellipses compare well with other approximate solutions except near the stagnation points where differences of up to 5% are encountered." @default.
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- W2022804540 date "1974-02-01" @default.
- W2022804540 modified "2023-09-27" @default.
- W2022804540 title "Application of a Variational Method in Plane Compressible Flow Calculation" @default.
- W2022804540 doi "https://doi.org/10.1093/imamat/13.1.47" @default.
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