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.


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    Title :

    Automatic Transition Prediction for Three-Dimensional Aircraft Configurations Using the DLR TAU Code


    Contributors:


    Publication date :

    2010


    Size :

    8 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Transition Prediction for Three-Dimensional Configurations

    Krimmelbein, N. / Radespiel, R. | British Library Conference Proceedings | 2009


    Transition Prediction for Three-Dimensional Configurations

    Krimmelbein, N. / Radespiel, R. | Springer Verlag | 2009



    Transition Prediction for Three-Dimensional Configurations

    Krimmelbein, N. / Radespiel, R. | Tema Archive | 2009