In this paper, an analysis of basic airfoils profile for micro and small-scale horizontal axis wind turbine (HAWT) has been studied for different angle-of-attack and fixed Reynolds number. For turbine blade modeling, the data used is from National advisory committee of aeronautics (NACA) of five digit airfoil series. The comprehensive relationship between optimal angle-of-attack and Reynolds number has been analyzed. A low or high lift-to-drag ratio ( / ) can be identified at different angle-of-attack . The computational fluid dynamics analysis of NACA 63-415 airfoil is carried out at different angle-of-attack at wind speed 5 m/s using ANSYS/Fluent software. The pressure, turbulence and velocity distribution plots have been observed.Index Terms-Angle-of-attack ( ), coefficient of power ( ), horizontal axis wind turbine (HAWT), lift-to-drag ( / ) ratio, national advisory committee of aeronautics (NACA) series, reynolds number (Re) and tip speed ratio (TSR).