Volume 47 Issue 9
Sep.  2026
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Yang Hui, Yan Bo, Gao Yingbo, Zhang Bo, Lü Zhongbin, Liu Guanghui, Wu Xingwang, Deng Huachao. A Multi-Fidelity Surrogate Model for Aerodynamic Coefficients of Iced Bundle Conductors[J]. Applied Mathematics and Mechanics, 2026, 47(9): 1159-1178. doi: 10.21656/1000-0887.460131
Citation: Yang Hui, Yan Bo, Gao Yingbo, Zhang Bo, Lü Zhongbin, Liu Guanghui, Wu Xingwang, Deng Huachao. A Multi-Fidelity Surrogate Model for Aerodynamic Coefficients of Iced Bundle Conductors[J]. Applied Mathematics and Mechanics, 2026, 47(9): 1159-1178. doi: 10.21656/1000-0887.460131

A Multi-Fidelity Surrogate Model for Aerodynamic Coefficients of Iced Bundle Conductors

doi: 10.21656/1000-0887.460131
  • Received Date: 2025-06-27
  • Rev Recd Date: 2025-07-30
  • Publish Date: 2026-09-01
  • For quad-, six-, and eight-bundle conductors with crescent-shaped ice, the air flow fields around the iced conductors under different icing and wind conditions were numerically simulated with the computational fluid dynamics, and the variations of drag, lift, and torque coefficients of each iced sub-conductor vs. the wind attack angle were obtained. With the high-fidelity data of aerodynamic coefficients measured by wind tunnel tests and the low-fidelity data by numerical simulations, a multi-fidelity surrogate model was built by means of the BP neural networks, the random forest algorithm and the feature enhancement technique, with the sub-conductor position, the ice thickness, the ice accretion angle, the wind speed, the turbulence intensity and the wind attack angle as the input, and the aerodynamic coefficients of each sub-conductor as the output. The efficiency of the surrogate model was verified through the analysis of aerodynamic stability regions based on the Den Hartog and Nigol coefficients, and through the galloping simulations of typical iced bundle conductors. By this multi-fidelity surrogate model, a software with the bundle number of conductor lines, the ice thickness, the ice accretion angle, the wind speed and the turbulence intensity as the input, and the aerodynamic coefficient vs. the wind attack angle for each iced sub-conductor as the output, was developed. This work lays a foundation for the investigation of galloping of iced transmission lines and its prevention technologies.
  • (Contributed by Yan Bo, Member of the Editorial Board of AMM)
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