A three-dimensional mathematical model for simulating ice accretion on helicopter rotors

被引:20
|
作者
Chen, Ningli [1 ,2 ]
Ji, Honghu [2 ]
Cao, Guangzhou [3 ]
Hu, Yaping [2 ]
机构
[1] Southwest Petr Univ, Sch Mechatron Engn, Chengdu 610500, Sichuan, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing 210016, Jiangsu, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Res Inst Unmanned Aircraft, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
PERFORMANCE DEGRADATION; ICING MODEL; FENSAP-ICE; AIRCRAFT; SURFACE; FLIGHT; FLOW; FILM;
D O I
10.1063/1.5041896
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A new three-dimensional mathematical model is proposed to predict the shape of accreted ice on helicopter rotors. The model assumes that ice accretion on a rotor's surface occurs by flow and solidification of a thin water film on its surface. The model is developed by analyzing conservation of mass, momentum, and energy in the thin water film on a rotating curved surface. The model is expressed in rotating body-fitted nonorthogonal curvilinear coordinates, and the Coriolis-force term in the momentum equations is neglected because its effect is relatively small compared with that of the centrifugal force. The computational method is presented to solve the model, and the model is validated by comparing its results with published experimental data. The results show that the proposed model accurately predicts both the water-film thickness and the ice-layer thickness on a rotating surface. Additionally, the model has been used to study how the rotor angular speed and MVD (Median Volumetric Diameter) of the droplets affect ice accretion. The results show that an increase in both angular speed and MVD can lead to a thicker layer of ice, while the effect of MVD on ice accretion near the stagnation point becomes unobvious when MVD is larger enough. Published by AIP Publishing.
引用
收藏
页数:12
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