Abstract
This paper provides a study of the dynamic stall of a pitching NACA 0012 airfoil at 106 Reynolds number by means of numerical simulation. A 2D study is carried out comparing three OES and URANS turbulence models (URANS, URANS k-ω SST and k-ε OES). Then a 3D computation is performed using DES Spalart modelling. URANS k-ω SST is providing the best results for 2D computations.
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© 2008 Springer-Verlag Berlin Heidelberg
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Martinat, G., Hoarau, Y., Braza, M., Vos, J., Harran, G. (2008). Numerical Simulation of the Dynamic Stall of a NACA 0012 Airfoil Using DES and Advanced OES/URANS Modelling. In: Peng, SH., Haase, W. (eds) Advances in Hybrid RANS-LES Modelling. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 97. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-77815-8_28
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DOI: https://doi.org/10.1007/978-3-540-77815-8_28
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-77813-4
Online ISBN: 978-3-540-77815-8
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