Abstract This chapter describes Dassault Aviation’s contribution to Workpackage 5 of the ADIGMA Project. The adjoint operator developed in the framework of optimum design is used to estimate the error in the solution with respect to a given target quantity. Local values of this error estimation are used as a criterion to refine the mesh. This yields significant improvement over traditional criteria based on the residual or on gradients of physical quantities. The method is carefully tested using inviscid, transonic, laminar, and high Reynolds number turbulent flows.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code

    Chalot, Frédéric / Normand, Pierre-Elie | Springer Verlag | 2010


    Three-Dimensional Stabilized Finite Elements for Compressible Navier–Stokes

    Erwin, J. Taylor / Anderson, W. Kyle / Kapadia, Sagar et al. | AIAA | 2013


    Three Dimensional Stabilized Finite Elements for Compressible Navier-Stokes

    Erwin, Jon / Anderson, W Kyle / Kapadia, Sagar et al. | AIAA | 2011


    GOAL-ORIENTED MESH ADAPTATION FOR FLOWS IN THERMOCHEMICAL NONEQUILIBRIUM

    Munguia, Brian C. / Maier, Walter T. / Needels, Jacob T. et al. | TIBKAT | 2020


    Goal-Oriented Mesh Adaptation for Flows in Thermochemical Nonequilibrium

    Munguía, Brian C. / Maier, Walter T. / Needels, Jacob T. et al. | AIAA | 2020