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Comparison of turbulence methods in CFD analysis of compressible flows in radial turbomachines

R. Aghaei tog (Engineering Department of Islamic Azad University of Shahr‐e‐Rey Branch, Tehran, Iran)
A.M. Tousi (Aerospace Department of Amir Kabir University of Technology, Tehran, Iran)
A. Tourani (Engineering Department of Islamic Azad University of Shahr‐e‐Rey Branch, Tehran, Iran)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 17 October 2008

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Abstract

Purpose

The purpose of this paper is to show the superior turbulence method in CFD analysis of radial turbo machines and to introduce the best way to choose turbulence parameters whenever FLUENT user applies this software as a complementary design tool for high‐speed turbo machinery components.

Design/methodology/approach

One of the most important issues in CFD is analysis of flow field in turbo machines. Flow in high‐speed radial turbo machinery is a 3D, turbulent and unsteady behavior so needs suitable method for converging. It is clear that the turbulence model has an extraordinary effect on investigation of 3D flows in high‐speed turbo machinery. A centrifugal compressor of micro and radial turbines have been designed and simulated 3D using the commercial CFD‐code FLUENT 6. Three turbulence models kε/standard, renormalization‐group (RNG) and RSM were considered and results of three models were compared with experimental and 1D design results.

Findings

The study showed numerical results are compatible with experimental performance data. It determined that RNG method in CFD analysis of radial turbo machines has provided better results than the standard kε method. In addition, when using the RNG method, the phenomena of flow field were more visible than other methods.

Originality/value

This paper offers use of the RNG method as a superior turbulence method in CFD analysis of radial turbo machines.

Keywords

Citation

Aghaei tog, R., Tousi, A.M. and Tourani, A. (2008), "Comparison of turbulence methods in CFD analysis of compressible flows in radial turbomachines", Aircraft Engineering and Aerospace Technology, Vol. 80 No. 6, pp. 657-665. https://doi.org/10.1108/00022660810911608

Publisher

:

Emerald Group Publishing Limited

Copyright © 2008, Emerald Group Publishing Limited

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