Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations-Reference-Cited by-同舟云学术

Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations

Published:2007-01 Issue:1 Volume:44 Page:119-133
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Krumbein Andreas¹

Affiliation:

1. DLR, German Aerospace Center, 37073 Göttingen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.22254

Reference52 articles.

1. Rudnik, R., Ronzheimer, A., and Schenk, M. "Berechnung von zweiund dreidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes Gleichungen," Deutschen Gesellschaft für Luft- und Raumfahrt (DGLR), JT 96-104, Deutscher Luft- und Raumfahrtkongreß, DGLR-Jahrestagung, Deutsche Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth, DGLR, D-53175 Bonn,Germany, 1996, pp.717-726.

2. Laminar-turbulent transition prediction in three-dimensional flows

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