The goal of this research is to develop a new aerodynamics design algorithm for the HAWT (Horizontal Axis Wind Turbine) to provide best power output at a rated wind speed. Traditional blade design method, which is based on the 2D airfoil’s blade element theory, and Prandtl’s blade tip loss correction formulation is applied to modify the span-wise geometry of the blade. This method inevitably introduced some inaccuracy in predicting the power coefficient of the blade. In this work, two blades are designed separated, a traditional one and a new designed based on a 3-dimensional aerodynamics wing theory. Both are by the blade element theory and momentum theory. Computational fluid dynamics (CFD) method is then used to calculate the performance of both blades. NACA4412 airfoil is adopted for both blades’ sectional profiles.