Author(s)

Hechmi Khlifi, Adnan Bourehla

Laboratory of Aeronautical Structure and Control of System Flows, SACES (UR17DN01), School of Military Avition, Borj el Amri, Tunisia.

The incompressible models for the pressure-strain correlation are unable to correctly predict the turbulence flows evolving with significant compressibility. Huang and Fu use a damping function of the turbulent Mach number to modify two numerical coefficients of the incompressible model for the pressure strain developed by Launder, Reece and Rodi. This model predicts the spreading rate and the shear stress behavior in compressible turbulent mixing well. However, the model does not show the well-known compressibility effects on the compressible homogenous shear flow. In the present work, the model of Huang-Fu is revised, all resulting model coefficients become dependent on the turbulent Mach number, the gradient Mach number and the convective Mach number. The proposed model is tested in different compressible turbulent homogeneous shear flow and mixing layers cases. In general, the predicted results from the proposed model are in an acceptable agreement with DNS and experiment data.

Turbulence, Compressible, Model, Pressure-Strain

Khlifi, H. and Bourehla, A. (2022) A Comparative Study for Compressible Turbulence Models. World Journal of Mechanics, 12, 1-16. doi: 10.4236/wjm.2022.121001.