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旋转状态下S型带肋通道流动特性数值研究

王顺斌 张丽 赵曙 朱惠人 孙瑞嘉

王顺斌, 张丽, 赵曙, 朱惠人, 孙瑞嘉. 旋转状态下S型带肋通道流动特性数值研究[J]. 航空动力学报, 2015, 30(7): 1583-1591. doi: 10.13224/j.cnki.jasp.2015.07.007
引用本文: 王顺斌, 张丽, 赵曙, 朱惠人, 孙瑞嘉. 旋转状态下S型带肋通道流动特性数值研究[J]. 航空动力学报, 2015, 30(7): 1583-1591. doi: 10.13224/j.cnki.jasp.2015.07.007
WANG Shun-bin, ZHANG Li, ZHAO Shu, ZHU Hui-ren, SUN Rui-jia. Numerical study of flow characteristics in rotating S-shaped passage with ribs[J]. Journal of Aerospace Power, 2015, 30(7): 1583-1591. doi: 10.13224/j.cnki.jasp.2015.07.007
Citation: WANG Shun-bin, ZHANG Li, ZHAO Shu, ZHU Hui-ren, SUN Rui-jia. Numerical study of flow characteristics in rotating S-shaped passage with ribs[J]. Journal of Aerospace Power, 2015, 30(7): 1583-1591. doi: 10.13224/j.cnki.jasp.2015.07.007

旋转状态下S型带肋通道流动特性数值研究

doi: 10.13224/j.cnki.jasp.2015.07.007
基金项目: 

国家重点基础研究发展计划(2013CB035702)

详细信息
    作者简介:

    王顺斌(1990-),男,浙江温州人,硕士生,主要从事航空发动机高温部件传热与冷却技术研究.

  • 中图分类号: V231.1

Numerical study of flow characteristics in rotating S-shaped passage with ribs

  • 摘要: 为了更好地了解涡轮叶片内冷完整通道中流体的流动特性,数值研究了肋、转弯以及旋转对完整S型带肋通道流动特性的影响.雷诺数为17000,3个出口的出流比分别为27%,49%,24%,旋转数取0,0.03,0.06,0.09.结果表明:通道1靠近前缘侧阻塞比高,肋的扰流作用强,流体速度较低.转弯引起流体流动分离,使转弯下游通道中的主流发生偏移,通道3靠近分隔板侧存在较大范围低速区.旋转产生的切向哥氏力使流体向哥氏力指向面偏移,通道2与通道3主流分别偏向吸力面与压力面.旋转影响通道中二次流的分布,增强转弯下游低速回流涡区域流体的流动.

     

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出版历程
  • 收稿日期:  2014-01-21
  • 刊出日期:  2015-07-28

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