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Hybrid RANS-LES Modeling Using a Low-Reynolds-Number k−ω Based Model

Sebastian Arvidson (Institutionen för tillämpad mekanik, Strömningslära) ; Lars Davidson (Institutionen för tillämpad mekanik, Strömningslära) ; Shia-Hui Peng (Institutionen för tillämpad mekanik, Strömningslära)
52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, National Harbor, United States, 13-17 January 2014 p. 22. (2014)
[Konferensbidrag, refereegranskat]

Hybrid RANS-LES modeling is proposed using a Low-Reynold-Number (LRN) k − ω model. The model is demonstrated in a zonal RANS-LES approach and in an embedded LES approach. The model is calibrated and evaluated using Decaying Homogeneous Isotropic Turbulence (DHIT), turbulent channel flow and turbulent flow over a hump. The effect of different LES length scales on log-layer mismatch and turbulence resolving capability is demonstrated using the proposed model. Interface conditions are proposed in the embedded LES approach in order to reduce the grey area zone in the LES domain downstream of the RANS region. To further improve the development of turbulence resolving flow in the LES region downstream of the interface, anisotropic turbulent velocity fluctuations from synthetic turbulence are added. The hybrid RANS-LES modeling approaches that are presented, using the LRN k − ω based model, show that predictions of turbulence resolving flows are in reasonable agreement with experimental data and DNS data. Moreover, the choice of the LES length scale using the proposed model is shown to be of great importance in reducing the log-layer mismatch.

Nyckelord: CFD, turbulence modeling, hybrid RANS-LES, embedded LES

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Denna post skapades 2014-04-01. Senast ändrad 2017-10-03.
CPL Pubid: 196076


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Institutioner (Chalmers)

Institutionen för tillämpad mekanik, Strömningslära (2005-2017)



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C3SE/SNIC (Chalmers Centre for Computational Science and Engineering)

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Methodologies for RANS-LES interfaces in turbulence-resolving simulations