A Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and different transition prediction methods for the prediction of Tollmien-Schlichting and cross flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general three-dimensional aircraft configurations during the ongoing flow computation. In this article, the procedure is applied to a two-dimensional three-element high-lift airfoil configuration which is characterized by the existence of laminar separation bubbles. The automatic transition prediction procedure is applied using different operation modes and different transition prediction strategies.
Application of Transition Prediction
2009
14 Seiten
Conference paper
English
Application of Transition Prediction
British Library Conference Proceedings | 2009
|Application of Transition Prediction
Springer Verlag | 2009
|Application of Similarity in Hypersonic Transition Prediction (TN)
Online Contents | 1995
|Automatic Transition Prediction Application to Three-Dimensional Wing Configurations
Online Contents | 2007
|