A novel method, a non-destructive test, is developed to obtain the dynamic elasticity modulus of composite wind turbine blades. The proposed method is based on the free vibration theory of cantilever beams, the sectional analysis of laminated composites, the laminated composite theory, and the area contribution method. In response, the static elasticity modulus and the area properties of a hollow cross-section are obtained. On the other hand, by employing an equivalent beam that integrates all the cross-sections of a wind turbine blade. The method is tested with an equivalent blade, and all incidences of nonlinearity are avoided to obtain linear vibration modes; it is demonstrated that the free vibration test is applicable. Finally, it is observed that the first three natural frequencies were related to the dynamic elasticity modulus, where the third frequency shows an error of less than 1.2 %. This study revealed that the method for dynamics elasticity modulus has good potential to be used in the design of wind turbine blades as a quality control and non-destructive test.