Lingkong Technology’s R&D team strikes again! A detailed analysis of the impact of propeller slipstream on the aerodynamic characteristics of twin-tail‑boom UAVs.
The R&D team of Lingkong Technology (including Zhao Caixia, Dong Wenhui, Fan Kejing, and others), based on the aerodynamic configuration of the GHQ-600 fixed-wing UAV, published the academic paper “A Comparative Analysis of the Influence of Propeller Slipstream on the Aerodynamic Characteristics of UAVs with Different Tail Configurations” in Advances in Aerospace Engineering (Vol. 17, No. 2, 2026).
2026.06.26