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- W2474291260 abstract "Once the linearised lift problem for a supersonic wing has been solved and the disturbance velocity potential or the pressure is known at every point on the surface, the complete flow round the wing and the downwash behind the wing may be found by the following procedure." @default.
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- W2474291260 date "1949-05-01" @default.
- W2474291260 modified "2023-09-26" @default.
- W2474291260 title "Calculation of Downwash Behind a Supersonic Wing" @default.
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- W2474291260 doi "https://doi.org/10.1017/s0001925900000056" @default.
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