摘要 : During the aircraft icing process caused by super-cooled droplet impingement, the surface temperature and heat flux distributions of the skin would vary due to the solid substrate heat conduction. An unsteady thermodynamic model o... 展开
作者 | Shen~ Xiaobin Zeng~ Yu Lin~ Guiping Mu~ Zuodong Wen~ Dongsheng |
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作者单位 | |
期刊名称 | 《Proceedings of the Institution of Mechanical Engineers》 |
页码/总页数 | 1306-1317 / 12 |
语种/中图分类号 | 英语 / TH |
关键词 | Aircraft icing icing thermodynamic model effect of heat conductivity ice accretion rate numerical simulation |
DOI | 10.1177/0954410020972577 |
馆藏号 | TH-038 |