Evaluation of RANS and LES turbulence models for simulating a steady 2-D plane wall jet
Abstract
Purpose
This paper examines various turbulence models for numerical simulation of a steady, two-dimensional (2-D) plane wall jet without co-flow using the commercial CFD software (ANSYS FLUENT 14.5). The purpose of this paper is to decide the most suitable and most economical method for steady, 2-D plane wall jet simulation.
Design/methodology/approach
Seven Reynolds-averaged Navier–Stokes (RANS) turbulence models were evaluated with respect to typical jet scaling parameters such as the jet half-height and the decay of maximum jet velocity, as well as coefficients from the law of the wall and for skin friction. Then, a plane wall jet generating from a rectangular slot of 1:6 aspect ratio located adjacent to the wall was investigated in a three-dimensional (3-D) model using large eddy simulation (LES) and the Stress-omega Reynolds stress model (SWRSM), with the results compared to experimental measurements.
Findings
The comparisons of these simulated flow characteristics indicated that the SWRSM was the best of the seven RANS models for simulating the turbulent wall jet. When scaled with outer variables, LES and SWRSM gave generally indistinguishable mean velocity profiles. However, SWRSM performed better for near-wall mean velocity profiles when scaled with inner variables. In general, the results show that LES performed reasonably well when predicting the Reynolds stresses.
Originality/value
The main contribution of this article is in determining the capabilities of different RANS turbulence closures and LES for the prediction of the 2-D steady wall jet flow to identify the best modelling approach.
Keywords
Acknowledgements
This work was supported by the National Natural Science Fund (China, 51478069, 51778097) and Chongqing Natural Science fund (cstc2017jcyjB0210).
Citation
Yan, Z., Zhong, Y., Lin, W.E., Savory, E. and You, Y. (2018), "Evaluation of RANS and LES turbulence models for simulating a steady 2-D plane wall jet", Engineering Computations, Vol. 35 No. 1, pp. 211-234. https://doi.org/10.1108/EC-11-2016-0397
Publisher
:Emerald Publishing Limited
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