“…The following airfoils are used: NACA 4415, 4418, 4421, 4424, 4430 and 4436 (Fuglsang et al, 2004;Khaled et al, 2017;Mamadaminov, 2013;Manwell et al, 2009). These are located in the blade according to defined considerations used by (Mohammadi et al, 2016) and (Adaramola, 2014). Using the XFOIL software the lift and drag coefficients are evaluated (Manwell et al, 2009; Massachusetts Institute of Technology, 2013).…”