A nonlinear low-Reynolds-number k-e model of was extended to predict the flows over a step with inclined wall, where a boundary-layer flow without separation and a separated and reattaching flow coexist. For a better prediction of the flows, a slight modification was made on the function of wall da
Modelling shock-affected near-wall flows with anisotropy-resolving turbulence closures
✍ Scribed by M.A. Leschziner; P. Batten; H. Loyau
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 668 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0142-727X
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✦ Synopsis
This paper reviews some recent research aiming to assess the performance of advanced forms of second-moment closure and nonlinear eddy-viscosity models for compressible ¯ows, with particular emphasis placed on strong shock-boundary-layer interaction involving separation. This topic is of particular relevance to high-speed aerospace and turbomachinery aerodynamics. Relevant closure forms and their merits, relative to simpler linear eddy-viscosity approximations, are reviewed ®rst, mainly in qualitative terms. The performance of some particular models is then examined by reference to solutions for a range of 2D and 3D compressible ¯ows.
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