M. Lahooti, G. Vivarelli, F. Montomoli, S. Sherwin
In this work a high-order spectral-h/p element solver is employed to efficiently but accurately resolve the flow field around the NACA0012 aerofoil.
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Published on 22/11/22
Volume Computational Applied Mathematics, 2022DOI: 10.23967/eccomas.2022.281Licence: CC BY-NC-SA license
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