Composites are well-known for its characters of lightweight and high strength, but because of the various manufacturing methods of composite members, it is often not easy to perform the finite element method analysis. Therefore, if the equivalent material mechanical properties of composites could be first calculated, the composite materials could be considered as quasi-isotropic materials, then the analysis of finite element method will be significantly simplified and speed up the composite products time to the market. This study focuses on the carbon fiber prepreg member(chassis strut bar) to calculate its equivalent material mechanical properties, and then to perform the finite element method analysis. The experimental values are to compare those of the ANSYS simulation to verify this approach’s feasibility. Finally, the ANSYS simulations of the traditional aluminum alloy strut bar and carbon fiber strut bar of the same size have been carried out to compare the stiffness of the two strut bars.