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| + | ==Summary== | ||
| + | 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. | ||
| + | |||
| + | == Abstract == | ||
| + | <pdf>Media:Draft_Sanchez Pinedo_5535503162128_abstract.pdf</pdf> | ||
| + | |||
| + | == Full Paper == | ||
| + | <pdf>Media:Draft_Sanchez Pinedo_5535503162128_paper.pdf</pdf> | ||
Latest revision as of 13:43, 22 November 2022
Summary
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.
Abstract
Full Paper
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Published on 22/11/22
Volume Computational Applied Mathematics, 2022
DOI: 10.23967/eccomas.2022.281
Licence: CC BY-NC-SA license
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