Verification and validation of OpenFOAM for high-lift aircraft flows
This paper presents a detailed investigation into the performance of the open-source finite volume computational fluid dynamics (CFD) code OpenFOAM for complex high-lift aircraft flows. A range of cases are investigated, including a zero-pressure gradient flat plate, a NACA0012 airfoil at varying an...
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics (AIAA)
2019
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