Assessment of several modeling strategies on the prediction of lift-drag coefficients of a NACA0012 airfoil at a moderate Reynold number
This paper investigates modelling strategies on the prediction of lift and drag coefficients of a NACA0012 airfoil at Reynolds number of 360,000. Two computational methods are employed; namely Navier-Stokes equation and panel method, by using different tools for computing lift and drag coefficients....
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| Format: | article |
| Langue: | EN |
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Elsevier
2022
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| Accès en ligne: | https://doaj.org/article/088a1f4595ed4f98a117d6646807e04e |
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