Investigation of the Resolution Requirements for a Hybrid RANS/LES Simulation of a Multi-element Airfoil

Author:

Reuß S.,Knopp T.,Schwamborn D.

Publisher

Springer Berlin Heidelberg

Reference13 articles.

1. Spalart, P.R., Jou, W.H., Strelets, M.K., Allmaras, S.R.: Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach. In: 1. AFOSR Int. Conf. Advances in DNS/LES, August 4-8 (1997)

2. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 103: DESider A European Effort on Hybrid RANS-LES Modelling (2009)

3. Schwamborn, D., Gardner, A., von Geyr, H., Krumbein, A., Lüdeke, H., Stürmer, A.: Development of the TAU-Code for aerospace applications. In: 50th NAL International Conference on Aero-space Science and Technology (2008), http://www.nal.res.in/nal50/incast/incast/01-Invited

4. Spalart, P.R., Deck, S., Shur, M.L., Squires, K.D., Strelets, M.K., Travin, A.: A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities. Theoretical and Computational Fluid Dynamics 20(3), 181–195 (2006)

5. Shur, M.L., Spalart, P.R., Strelets, M.K., Travin, A.: A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities. International Journal of Heat and Fluid Flow 29(6), 1638–1649 (2008)

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