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.
Error Estimation and Adaptive Mesh Refinement for Aerodynamic Flows
ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications ; 2 ; 339-353
01.01.2010
15 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Mach Number , Coarse Mesh , Discontinuous Galerkin , Adaptive Mesh , Discontinuous Galerkin Method Engineering , Engineering Fluid Dynamics , Astronomy, Astrophysics and Cosmology , Classical Continuum Physics , Aerospace Technology and Astronautics , Appl.Mathematics/Computational Methods of Engineering , Numerical and Computational Physics
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