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Navier-Stokes analysis of a circulation control airfoil
Authors:Liu Jingchang  Sun Mao  Wu Liyi
Institution:(1) Beijing University of Aeronautics and Astronautics, 100083 Beijing, China;(2) Present address: Institute of Engineering Thermophysics, Chinese Acadamy of Sciences, 100080 Beijing, China
Abstract:The two-dimensional, compressible, mass-averaged Navier-Stokes equations are used to investigate flows about a typical circulation control airfoil. The governing equations are solved using the implicit approximate-factorization algorithm of Beam-Warming with a modified algebraic eddy viscosity model. Results are compared with experimental data, and excellent agreement is obtained. The effects of different jet momentum coefficients and angles of attack on the flow are studied. The mechanism of genenating large lift by circulation control is discussed.
Keywords:circulation control airfoil  Navier-Stokes equations
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