Velocity distribution on wing sections of arbitrary shape in compressible potential flow III : circulatory flows obeying the simplified density-speed relation

Lipman Bers
naca-tn-2056
Mar 1950


The method of computing velocity and pressure distributions along wing profiles under the assumption of the simplified density-speed relation, outlined in NACA Technical Note 1006, is extended to the case of a nonsymmetrical profile and a flow with circulation. The shape of the profile, the speed of the undisturbed flow, and a parameter determining the angle of attack may be prescribed.

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