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An overset-mesh approach for large-Eddy simulation of high-Reynolds number aerofoil flow |
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| Authors: | D P Rizzetta M R Visbal |
| Institution: | 1. Air Force Research Laboratory, Dayton, OH, USAdonald.rizzetta@us.af.mil;3. Air Force Research Laboratory, Dayton, OH, USA |
| Abstract: | |
| Keywords: | Large-eddy simulation high-Reynolds number aerofoil high-order numerical method nested-grid approach high-order interpolation |