The application of a computational method to predict transition for three-dimensional configurations is presented. The method consists of a coupled program system including a 3D Navier-Stokes solver, a transition prediction module, a boundary-layer code and a stability solver. Focus is placed on the industrialization of the method. For this, approaches to treat different, complex three-dimensional aircraft geometries and to account for limitations of the transition prediction method in an industrial computational environment are presented.


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    Title :

    Industrialization of the Automatic Transition Prediction in the DLR TAU Code


    Additional title:

    Notes Numerical Fluid Mech.


    Contributors:


    Publication date :

    2013-01-01


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English