Abstract This chapter presents high-order DG solutions of the RANS and k-ω turbulence model equations for transonic flows around aeronautical configurations. A directional shock-capturing term, proportional to the inviscid residual, is employed to control oscillations around shocks. Implicit time integration is applied to the fully coupled RANS and k-ω equations. Several high-order DG results of 2D and 3D transonic turbulent test cases proposed within the ADIGMA project demonstrate the capability of the method.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    High-Order Discontinuous Galerkin Discretization of Transonic Turbulent Flows

    Bassi, Francesco / Crivellini, Andrea / Ghidoni, Antonio et al. | AIAA | 2009


    High-Order Discontinuous Galerkin Discretization of Transonic Turbulent Flows

    Bassi, F. / Crivellini, A. / Ghidoni, A. et al. | British Library Conference Proceedings | 2009



    High-Order Discontinuous Galerkin Method for Computation of Turbulent Flows

    Wang, Li / Kyle Anderson, W. / Erwin, Taylor et al. | AIAA | 2015