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一种用于飞机结冰的海绵冰模型及应用

李鑫 白俊强 王昆

李鑫, 白俊强, 王昆. 一种用于飞机结冰的海绵冰模型及应用[J]. 航空动力学报, 2013, 28(11): 2419-2429.
引用本文: 李鑫, 白俊强, 王昆. 一种用于飞机结冰的海绵冰模型及应用[J]. 航空动力学报, 2013, 28(11): 2419-2429.
LI Xin, BAI Jun-qiang, WANG Kun. A spongy icing model for aircraft icing and application[J]. Journal of Aerospace Power, 2013, 28(11): 2419-2429.
Citation: LI Xin, BAI Jun-qiang, WANG Kun. A spongy icing model for aircraft icing and application[J]. Journal of Aerospace Power, 2013, 28(11): 2419-2429.

一种用于飞机结冰的海绵冰模型及应用

A spongy icing model for aircraft icing and application

  • 摘要: 基于两相流理论,采用欧拉法对飞机结冰进行数值模拟,在空气流场速度分布的基础上,求解水滴流场,得到水滴收集率和撞击极限.结果表明:欧拉法比拉格朗日法在计算水滴收集效率和撞击极限方面有优势,尤其是在较大的水滴平均等效直径情况下.对翼型的冰形和圆柱表面的温度预测数据和实验数据进行对比,圆柱冰形厚度误差在15.0%之内,计算结果与实验结果吻合较好,同时表明结冰模型是有效可行的.

     

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出版历程
  • 收稿日期:  2013-01-14
  • 刊出日期:  2013-11-28

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