The Wilcox 2006 stress- ω model, a Reynolds stress model, implemented in both the NASA Langley codes FUN3D and CFL3D, has been used to study a number of 2-D and 3-D cases. This study continues the assessments of the stress- ω model by simulating the flow over two wings: the DPW-W1 and the DLR-F11 wings. Using FUN3D, which uses unstructured grids, and CFL3D, which uses structured grids, the results were compared to solvers employing one- and two-equation turbulence models and experimental data. In general, in situations where experimental data is available, the stress- ω model performs as well or better than one- and two-equation models.


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    Title :

    Simulation of a Variety of Wings Using a Reynolds Stress Model


    Contributors:

    Published in:

    Journal of Aircraft ; 52 , 5 ; 1668-1680


    Publication date :

    2015-09-01




    Type of media :

    Conference paper , Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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