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Detailed comparisons are made between CFD and DSMC predictions for laminar attached flow near the leading edge for three canonical geometries, to understand the role of slip near the wall.
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This page is a summary of: Velocity-Slip and Temperature-Jump Effects in Near-Continuum Hypersonic Flows, AIAA Journal, June 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059890.
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