• 结冰 - 引用次数：6

  The design of anti-icing system for aircraft engines has been conducted to small droplet icing condition. However,recent research shows that icing accretion due to supercooled large droplet(SLD)may result in extremely severe aircraft or engine performance degradation.

  目前航空发动机防冰系统通用设计方案是以过冷小水滴的撞击特性为依据,但最新的研究结果显示大尺寸水滴环境下的结冰会对飞行器带来更加恶劣的影响。

  参考来源 - 发动机整流支板的大尺寸过冷水滴撞击特性研究

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