Numerical Simulation of Aerodynamic Problems with the SSG/LRR-ω Reynolds Stress Turbulence Model Using the Unstructured TAU Code-Reference-Cited by-同舟云学术

Numerical Simulation of Aerodynamic Problems with the SSG/LRR-ω Reynolds Stress Turbulence Model Using the Unstructured TAU Code

Published: Issue: Volume: Page:356-363
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Container-title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)
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Author:

Eisfeld Bernhard

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-540-74460-3_44.pdf

Reference15 articles.

1. J. Barche (Ed): ”Experimental Data Base for Computer Program Assessment”, AGARD-Report AGARD-AR-138, 1979

2. B. Eisfeld: ”Numerical simulation of aerodynamic problems with a Reynolds stress model”. In: H.-J. Rath, C. Holze, H.-J. Heinemannm R. Henke, H. Hönlinger (Eds.): New Results in Numerical and Experimental Fluid Mechanics V, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 92, pp. 413–419, 2006

3. B. Eisfeld, ”Computation of Complex Compressible Aerodynamic Flows with a Reynolds Stress Turbulence Model”. In: G. Lube, G. Rapin (Eds.): International Conference on Boundary and Interior Layers, BAIL 2006, Göttingen, 2006

4. B. Eisfeld, O. Brodersen: ”Advanced Turbulence Modelling and Stress Analysis for the DLR-F6 Configuration”. AIAA-Paper 2005–4727, 2005

5. J. K. Fassbender: ”Improved Robustness for Numerical Simulation of Turbulent Flows around Civil Transport Aircraft at Right Reynolds Numbers”. Dissertation, Technische Universität Braunschweig, DLR Forschungsbericht, DLR-FB 2003-09, 2004

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