AbstractA 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 in order to perform Reynolds-averaged Navier–Stokes computations of three-dimensional, finite wings with automatic laminar-turbulent transition prediction. The results from computations based on two database methods and a local, linear stability code together with the eN-method are compared for a three-dimensional wing configuration.
eN transition prediction for 3D wing configurations using database methods and a local, linear stability code
Aerospace Science and Technology ; 12 , 8 ; 592-598
2008-01-30
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Automatic Transition Prediction Application to Three-Dimensional Wing Configurations
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