
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.
CASE, adjoint-based error estimation, mesh refinement, turbulent flows
CASE, adjoint-based error estimation, mesh refinement, turbulent flows
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