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引射式结冰风洞内圆柱结冰试验

孟繁鑫 陈维建 梁青森 张大林

孟繁鑫, 陈维建, 梁青森, 张大林. 引射式结冰风洞内圆柱结冰试验[J]. 航空动力学报, 2013, 28(7): 1467-1474.
引用本文: 孟繁鑫, 陈维建, 梁青森, 张大林. 引射式结冰风洞内圆柱结冰试验[J]. 航空动力学报, 2013, 28(7): 1467-1474.
MENG Fan-xin, CHEN Wei-jian, LIANG Qing-sen, ZHANG Da-lin. Experiment on cylinder icing in injection driven icing wind tunnel[J]. Journal of Aerospace Power, 2013, 28(7): 1467-1474.
Citation: MENG Fan-xin, CHEN Wei-jian, LIANG Qing-sen, ZHANG Da-lin. Experiment on cylinder icing in injection driven icing wind tunnel[J]. Journal of Aerospace Power, 2013, 28(7): 1467-1474.

引射式结冰风洞内圆柱结冰试验

Experiment on cylinder icing in injection driven icing wind tunnel

  • 摘要: 设计并建造了用于结冰研究的小型引射式结冰风洞试验系统,对其结冰气象条件参数进行了标定,给出了试验段水雾均匀区范围,验证了试验冰形的可重复性.在霜状冰和瘤状冰条件下,对直径为25.4mm和50.8mm的圆柱在所建的结冰风洞内进行了结冰试验.试验结果表明:在所研究的结冰条件和结冰时间范围内,霜状冰与瘤状冰的结冰厚度均随时间推进而线性增长;在满足结冰相似准则的情况下,冰形相似性结果良好,无量纲厚度的最大偏差约为10%.

     

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出版历程
  • 收稿日期:  2012-07-11
  • 刊出日期:  2013-07-28

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