数字农科院2.0

Construction of a CFD Simulation and Prediction Model for Pesticide Droplet Drift in Agricultural UAV Spraying

文献类型： 外文期刊

作者： Zhou, Qingqing;Zhang, Songchao;Huang, Meng;Cai, Chen;Zhang, Haidong;Jiao, Yuxuan;Xue, Xinyu

作者机构：

关键词： agricultural UAV;droplet drift;CFD numerical simulation;wind tunnel test;drift prediction model;centrifugal nozzle;flat-fan nozzle

期刊名称： AGRONOMY-BASEL

ISSN：

年卷期： 2026 年 16 卷 1 期

页码：

收录情况： SCIE（2025版）

摘要： This study employed a combined approach of computational fluid dynamics (CFD), numerical simulations, and wind tunnel tests to investigate droplet drift characteristics and develop prediction models in order to address the issues of low pesticide utilization rates and high drift risk, associated with droplet drift during agricultural unmanned aerial vehicle (UAV) spraying, as well as the unreliable results of field experiments. Firstly, a numerical model of the rotor wind field was established using the multiple reference frame (MRF) method, while the realizable k-epsilon turbulence model was employed to analyze the flow field. The model's reliability was verified through wind field tests. Next, the Euler-Lagrange method was used to couple the wind field with droplet movement. The drift characteristics of two flat-fan nozzles (FP90-02 and F80-02) were then compared and analyzed. The results showed that the relative error between the simulated and wind tunnel test values was within 20%. Centrifugal nozzle experiments were carried out using single-factor and orthogonal designs to analyze the effects of flight height, rotor wind speed, flight speed, and droplet size on drift. The priority order of influence was found to be rotor wind speed > flight height > flight speed, while droplet size (D-V50 = 100-300 mu m) was found to have no significant effect. Based on the simulation data, a multiple linear regression drift prediction model was constructed with a goodness of fit R-2 value of 0.9704. Under the verification condition, the relative error between the predicted and simulated values was approximately 10%. These results can provide a theoretical basis and practical guidance for assessing drift risk and optimizing operational parameters for agricultural UAVs.

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