The aerodynamic analysis of iced and clean NACA 4410 and 0012 airfoils
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DOI: 10.1556/606.2023.00770
Abstract: The aims of the work is to develop a numerical iced airfoil; quarter round forward ice was tested on NACA 4410 and NACA 0012 airfoils at zero and non-zero angles of attack, and Reynolds numbers… read more here.
Keywords: airfoil; naca 4410; aerodynamic analysis; 0012 airfoils ... See more keywords