Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow: 3 - Circulatory Flows Obeying the Simplified Density-speed Relation
Lipman Bers
Jan 1950 · National Advisory Committee for Aeronautics
Ebook
36
Pages
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About this ebook
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 determing the angle of attack may be prescribed. The problem is reduced to a nonlinear integral equation which can be solved numerical by an iteration method. A numerical example is given.
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