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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2056.pdf