This paper's goal is to determine the best material for propeller cutting edges. The method used for this study is to design the NACA 4412 propeller model is analyzed using numerical methods and validated by theoretical methods in order to find maximum stress and distortion area. It shows that the centrifugal stress for titanium is increased 100% than fiber reinforced plastic composites. In the present study static analysis of structure is analyzed using different materials and its stress and deformation values are obtained. This novel concept is used for the entire turbo prop and piston engine propeller to enhance the life time by introducing the new material. Also this concept will be used for existing and upcoming aircrafts.