Direct Numerical Simulations on the three-dimensional wake transition of flows over NACA0012 airfoil at Re = 1000

نویسندگان

چکیده

For micro air vehicles (MAV), the precise prediction of aerodynamic force plays an important role. The a comparative low Reynold number (Re) vehicle tends to be affected by different flow modes. In this paper, performance three-dimensional NACA0012 airfoil is studied numerically. A range angles attack ( α) 0°−25° and Reynolds 1000 considered. Mean fluctuating coefficients forces around are analyzed for wake difference between two simulations compared. results show that remains steady two-dimensional lower attack. At α = 9°, Von Karman vortex pattern noticed. Flow transition as angle increases from 13°. 3D found stable with parallel shedding mode 14°-17°. However, these modes become finer gradual increase in incidence. While, loses its stability chaotic increment afterwards.

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ژورنال

عنوان ژورنال: International Journal of Micro Air Vehicles

سال: 2021

ISSN: ['1756-8307', '1756-8293']

DOI: https://doi.org/10.1177/17568293211055656