Vol.1 , No. 4, Publication Date: Jun. 12, 2015, Page: 156-173
[1] | Edisson S. G. Maciel, Aeronautical Engineering Division, ITA (Aeronautical Technological Institute), SP, Brazil. |
In the present work, the Van Leer and the Liou and Steffen Jr. flux vector splitting schemes are applied to the three-dimensional Favre-averaged Navier-Stokes equations. The Cebeci and Smith and Baldwin and Lomax algebraic models and the Jones and Launder and Wilcox and Rubesin two-equation models are used in order to close the problem. The physical problem under study is the supersonic flow around a blunt body. The results have demonstrated that the Van Leer scheme using the Wilcox and Rubesin turbulence model has yielded the best value of the stagnation pressure at the blunt body’s nose.
Keywords
Cebeci and Smith Turbulence Model, Jones and Launder Turbulence Model, Baldwin and Lomax Turbulence Model, Wilcox and Rubesin Turbulence Model, Navier-Stokes Equations, Three-Dimensions
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