Velocity Distribution On Wing Sections Of Arbitrary Shape In Compressible Potential Flow 2 Subsonic Symmetric Adiabatic Flows
Download Velocity Distribution On Wing Sections Of Arbitrary Shape In Compressible Potential Flow 2 Subsonic Symmetric Adiabatic Flows PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Velocity Distribution On Wing Sections Of Arbitrary Shape In Compressible Potential Flow 2 Subsonic Symmetric Adiabatic Flows book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow
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.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1945