The invention relates to the technical field of experimental fluid mechanics and aerodynamics and discloses an active rotation type airflow field test system. The system comprises a flow equalizing acceleration duct and a rotation mechanism, in the flow equalizing acceleration duct, the cross section area of a contraction section is gradually reduced along the air inlet direction; the test section is of a cylindrical ventilation structure and is used for placing a test object; the sectional area of the diffusion section is gradually increased in the air inlet direction; the contraction section, the test section and the diffusion section are symmetrical structures taking the first reference surface as a symmetrical central surface; in the contraction section, a distance from the midpoint of the air inlet inner side edge to the second reference surface is the maximum value a of the distance from any point in the air inlet inner side edge to the second reference surface, a distance from the midpoint of the air inlet outer side edge to the second reference surface is the maximum value b of the distance from any point in the air inlet outer side edge to the second reference surface, and b is smaller than a. In the active rotary airflow field test system, the flow field homogeneity in the test section is ensured through the flow-equalizing acceleration duct (and the asymmetric honeycomb device) with a specific structure.