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Numerical Investigation of a NACA 0012 Airfoil with Static-Extended Trailing Edges and Gurney Flaps for Low-Reynolds-Number Wind Turbine Applications

by Tiberius S. Gikenyi, Churchill O. Saoke and Joseph N. Kamau

American Journal of Energy Research. 2025, 13(3), 86-95. DOI: 10.12691/ajer-13-3-2
Pub. Date: October 29, 2025Views: 2006 Downloads: 7003Like: 5

NACA0012 Gurney flap Static extended trailing edge CFD low Reynolds number

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