In order to effectively support the simulation analysis of unmanned aerial vehicle（UAV） impact on aircraft and reduce the cost of experimental research， the test and finite element simulation method research of collision between UAV and windshield of a transport category aircraft were carried out. The modeling method of windshield and UAV was studied and established according to the actual size and curved surface configuration. Considering the unpredictability and complexity of crack initiation and propagation of windshield glass after impact， zero-thickness cohesive elements were embedded between glass elements and between glass layer and rubber layer in the windshield model through Python programming， and the finite element model of windshield based on intrinsic cohesion was presented. It is found that the simulation results of corresponding conditions are basically consistent with the experimental results， which validates the cohesive zone model in the simulation. And compared with the conventional element deletion method， the simulation results based on the cohesive zone model are closer to the experimental results， which demonstrates that the established method has higher accuracy.