Propeller shaft and blade structure is widely used in aviation, ships, vehicles and energy technologies. It is an important research area for the development of the vehicle and Energy Technology. In order to explore the reaction force, reaction moment, relative displacement of connector, relative angular displacement of connector, von Mises stress of propeller blades and the effect of material properties to reaction force. This study will utilize the nonlinear finite element code ABAQUS to establish the nonlinear dynamic analysis procedure of rotating rectangular propeller. Then, the study results could be the reference for ship structure designer.