A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and a fully automated local, linear stability code for the prediction of Tollmien-Schlichting and cross-flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general aircraft configurations during the ongoing flow computation. The procedure is applied to a three-dimensional wing-body configuration and the sensitivity of the coupled system to a variety of coupling parameters is investigated.
Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR TAU Code
2010
8 Seiten
Conference paper
English
Automatic Transition Prediction Application to Three-Dimensional Wing Configurations
Online Contents | 2007
|Transition Prediction for Three-Dimensional Configurations
British Library Conference Proceedings | 2009
|Transition Prediction for Three-Dimensional Configurations
Springer Verlag | 2009
|Transition Prediction for Three-Dimensional Configurations
Tema Archive | 2009
|