Investigation on the ice-type microstructure characteristics of aircraft icing based on the fractal theories
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Investigation on the ice-type microstructure characteristics of aircraft icing based on the fractal theories
Vol. 26, Issue 5, (2011)
作者机构:
1. 中国空气动力研究与发展中心 计算空气动力研究所,四川,绵阳,621000
2. 北京航空航天大学 交通科学与工程学院,北京,100191
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Published:2011
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DU Yan-xia, GUI Ye-wei, KE Peng, et al. Investigation on the ice-type microstructure characteristics of aircraft icing based on the fractal theories[J]. 2011, 26(5).
DOI:
DU Yan-xia, GUI Ye-wei, KE Peng, et al. Investigation on the ice-type microstructure characteristics of aircraft icing based on the fractal theories[J]. 2011, 26(5).DOI:
Investigation on the ice-type microstructure characteristics of aircraft icing based on the fractal theories
The ice-type microstructure characteristics of aircraft icing were investigated by combining icing tunnel and metallography tests based on the theories of fractal geometry.The fractal dimension of the ice-type microstructure was calculated by means of box-counting dimension method
and the relationship between the fractal dimension and the icing conditions was analyzed.The results indicate that the inflow temperature and velocity of the airflow have great influence on the fractal dimension of ice-type microstructure.The higher velocity or the lower the temperature means greater fractal dimension
and vice versa.Under the same icing conditions
the fractal dimension of runback icing is smaller than the leading edge icing.