Numerical Simulation of the Dynamic Stall of a NACA 0012 Airfoil Using DES and Advanced OES/URANS Modelling.

Autor: Kacprzyk, J., Shia-Hui Peng, Haase, Werner, Martinat, G., Hoarau, Y., Braza, M., Vos, J., Harran, G.
Zdroj: Advances in Hybrid RANS-LES Modelling; 2008, p271-278, 8p
Abstrakt: 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. [ABSTRACT FROM AUTHOR]
Databáze: Supplemental Index