Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR TAU Code-Reference-Cited by-同舟云学术

Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR TAU Code

Published:2010 Issue: Volume: Page:101-108
ISSN:1612-2909
Container-title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Author:

Krumbein A.,Krimmelbein N.,Schrauf G.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-14243-7_13.pdf

Reference18 articles.

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2. Edwards, J.R., Chandra, S.: Comparison of Eddy Viscosity–Transport Turbulence Models for Three-Dimensional, Shock-Separated Flowfields. AIAA Journal 34(4), 756–763 (1996)

3. Krimmelbein, N., Radespiel, R., Nebel, C.: Numerical Aspects of Transition Prediction for Three-Dimensional Configurations. AIAA-2005-4764

4. Krimmelbein, N., Radespiel, R.: Transition prediction for three-dimensional flows using parallel computation. Computers & Fluids 38, 121–136 (2009)

5. Kroll, N., Rossow, C.-C., Schwamborn, D., Becker, K., Heller, G.: MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design. In: ICAS Congress 2002 [CD-Rom], ICAS, Toronto, Canada, pp. 1.105.1–1.105.20 (2002)

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