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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: 2006Downloads: 7016
NACA0012 Gurney flap Static extended trailing edge CFD low Reynolds number
Abstract Full Text PDF (1045 KB) Full Text HTML Full Text ePUB (940 KB)
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