The paper presents three benchmark cases for verification of Reynolds-averaged Navier-Stokes solvers. The verification studies focus on a one-equation Spalart-Allmaras model, SA-[neg]-QCR2000, that uses a version of quadratic constitutive relations.The benchmark cases are a two-dimensional subsonic flow around a Joukowski airfoil, a three-dimensional supersonic flow through a square duct, and a three-dimensional flow over a wing-fuselage configuration. The turbulence-model formulation, geometry, flow conditions, grids, and the expected output are described in detail. Reference solutions computed by several established codes are shown


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model


    Contributors:

    Conference:

    2021 AIAA SciTech Forum ; 2021 ; online, US


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model

    Diskin, Boris / Ahmad, Nashat N. / Anderson, William K. et al. | AIAA | 2021


    Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model

    Boris Diskin / Yi Liu / Hiroaki Nishikawa et al. | NTRS


    Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model

    Boris Diskin / Nash'at Ahmad / William K. Anderson et al. | NTRS


    VERIFICATION TEST SUITE FOR SPALART-ALLMARAS QCR2000 TURBULENCE MODEL

    Diskin, Boris / Ahmad, Nashat N. / Anderson, William K. et al. | TIBKAT | 2021


    VERIFICATION TEST SUITE FOR SPALART-ALLMARAS QCR2000 TURBULENCE MODEL

    Diskin, Boris / Ahmad, Nashat N. / Anderson, William K. et al. | TIBKAT | 2021