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To simulate the flow around aerodynamic configurations, we have developed a higher-order finite volume solver, which reduces both memory consumption and solution time.

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This page is a summary of: Efficient Convergence for a Higher-Order Unstructured Finite Volume Solver for Compressible Flows, AIAA Journal, April 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058537.
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