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Adaptive mesh solutions from several flow solvers, error estimates and adaptive meshing packages are compared on a 2d high-lift airfoil application. All methods show mesh convergence to very similar results. Differences in convergence efficiency are examined to provide recommendations for future adaptive mesh applications.
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This page is a summary of: Comparing Unstructured Adaptive Mesh Solutions for the High Lift Common Research Airfoil, AIAA Journal, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060088.
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