在所述蓄冰槽箱体中，过冷水滴撞击金属丝网进行解冷。
In the ice storage tank, the supercooled water drop impacts a metal mesh for de-cold.
研究表明飞机表面材料和过冷水滴，与机翼表面结冰之间存在一定联系。
It proves that super-cooled large droplets impingement onto airfoil and aircraft materials have a great effect on aircraft icing.
局部收集系数反映了空气中过冷水滴的撞击特性，对其进行计算是防、除冰研究的重要方面。
It is a significant aspect for research of local collection efficiencies that reflect the impingement properties of the super cooling water droplets in the air.
通过对空气流场、过冷水滴运动轨迹的计算和能量方程的求解，得到了多种状态下的风速管表面温度。
Based on the calculation of aerodynamic flow field, overcooled water droplets trajectories and energy equation, surface temperatures of the anemometer under various conditions were obtained.
通过对空气流场、过冷水滴运动轨迹的计算和能量方程的求解，得到了多种状态下的风速管表面温度。
Based on the calculation of aerodynamic flow field, overcooled water droplets trajectories and energy equation, surface temperatures of the anemometer under various conditions were obtained.
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