南京航空航天大学学报（自然科学版）2026，Vol.58Issue(3)：655-665,11.DOI:10.16356/j.2097-6771.2026.03.019
考虑非稳态耦合传热的多周期电热除冰过程数值模拟研究
Numerical Simulation Investigation of Multi-cycle Electrothermal Deicing with Transient Conjugate Heat Transfer
摘要
Abstract
Electrothermal deicing is recognized as a reliable method for aircraft ice protection.To systematically investigate the internal temperature variation and the ice-shedding process of the airfoil during multi-cycle deicing operations,this study establishes a coupled numerical simulation framework that integrates water film flow and transient heat transfer.The proposed model incorporates distinct conjugate heat transfer configurations for"water film/ice layer/wing"and"water film/wing"systems,explicitly accounting for the dynamic effects of ice accretionand shedding.The validity of the proposed model is verified through comparison with experimental data.Comparative analysis of the computational results from multi-cycle electrothermal deicing reveals that the continuously energized heated zone,functioning as a thermal knife,leads to an expansion in the coverage of both overflow water and ice accretion,accompanied by increased ice accretion in downstream heated zones.The results demonstrate that the proposed numerical model achieves a maximum deviation of less than 3 K in temperature profiles compared to experimental data throughout multiple electrothermal deicing cycles.Furthermore,it accurately predicts the evolution of both the runback water and ice accretion.关键词
多周期电热除冰/水膜流动/耦合传热/数值模拟Key words
multi-cycle electrothermal deicing/water film flow/coupled heat transfer/numerical simulation分类
航空航天引用本文复制引用
向冬,邱岳,朱春玲..考虑非稳态耦合传热的多周期电热除冰过程数值模拟研究[J].南京航空航天大学学报（自然科学版）,2026,58(3):655-665,11.基金项目
国家重点研发计划(2024YFB4205600). （2024YFB4205600）
