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旋转整流罩积冰过程中水膜流动和脱离的数值研究

菅锦锦 吉洪湖 曹广州 胡娅萍 陈宁立

菅锦锦, 吉洪湖, 曹广州, 胡娅萍, 陈宁立. 旋转整流罩积冰过程中水膜流动和脱离的数值研究[J]. 航空动力学报, 2018, 33(11): 2725-2736. doi: 10.13224/j.cnki.jasp.2018.11.019
引用本文: 菅锦锦, 吉洪湖, 曹广州, 胡娅萍, 陈宁立. 旋转整流罩积冰过程中水膜流动和脱离的数值研究[J]. 航空动力学报, 2018, 33(11): 2725-2736. doi: 10.13224/j.cnki.jasp.2018.11.019
Numerical study on water film flow and sheddingin ice accretion of rotating spinner[J]. Journal of Aerospace Power, 2018, 33(11): 2725-2736. doi: 10.13224/j.cnki.jasp.2018.11.019
Citation: Numerical study on water film flow and sheddingin ice accretion of rotating spinner[J]. Journal of Aerospace Power, 2018, 33(11): 2725-2736. doi: 10.13224/j.cnki.jasp.2018.11.019

旋转整流罩积冰过程中水膜流动和脱离的数值研究

doi: 10.13224/j.cnki.jasp.2018.11.019
基金项目: 国家自然科学基金(51506084);江苏省自然科学基金(BK20150740)

Numerical study on water film flow and sheddingin ice accretion of rotating spinner

  • 摘要: 为了更准确地模拟旋转整流罩积冰过程,在现有三维积冰与冰层表面薄水膜流动耦合模型基础上,基于功平衡分析的方法引入了旋转部件表面水膜脱离模型,并发展了相应的计算方法,给出了水膜脱离的判定依据:当气流曳力做的功和由于离心力使水膜增加的潜能之和大于黏附功时整流罩表面的水膜会发生脱离。对旋转整流罩积冰进行数值模拟,计算结果与实验结果吻合得较好,验证了该模型的合理性和计算方法的可行性。之后分析了转速和来流速度对整流罩表面水膜脱离和积冰的影响,结果表明:转速和来流速度越大,水膜发生脱离的比例越大。在研究范围内,转速为3000r/min和6000r/min时,因水膜脱离导致积冰总量分别减少13.4%和15.8%;来流速度为40、50m/s和60m/s时,因水膜脱离导致积冰总量分别减少为12.2%、13.4%、14.2%。

     

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出版历程
  • 收稿日期:  2018-01-03
  • 刊出日期:  2018-11-28

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