Abstract We consider the adjoint-based error estimation and goal-oriented mesh refinement for single and multiple aerodynamic force coefficients as well as residual-based mesh refinement applied to various three-dimensional laminar and turbulent aerodynamic test cases defined in the ADIGMA project.


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    GOAL-ORIENTED ERROR ESTIMATION AND HP-ADAPTIVE MESH REFINEMENT FOR AERODYNAMIC FLOWS

    Leicht, T. / Hartmann, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011



    Output Error Estimates and Mesh Refinement in Aerodynamic Shape Optimization

    Nemec, M. / Aftosmis, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013