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高旋转数下不同通道转角梯形带肋回转通道的换热特性

王晓增 阚瑞 田淑青 邓宏武

王晓增, 阚瑞, 田淑青, 邓宏武. 高旋转数下不同通道转角梯形带肋回转通道的换热特性[J]. 航空动力学报, 2017, 32(12): 2947-2954. doi: 10.13224/j.cnki.jasp.2017.12.018
引用本文: 王晓增, 阚瑞, 田淑青, 邓宏武. 高旋转数下不同通道转角梯形带肋回转通道的换热特性[J]. 航空动力学报, 2017, 32(12): 2947-2954. doi: 10.13224/j.cnki.jasp.2017.12.018
Heat transfer characteristics in twopass ribroughened trapezoidal channel at high rotation number with different model orientation angles[J]. Journal of Aerospace Power, 2017, 32(12): 2947-2954. doi: 10.13224/j.cnki.jasp.2017.12.018
Citation: Heat transfer characteristics in twopass ribroughened trapezoidal channel at high rotation number with different model orientation angles[J]. Journal of Aerospace Power, 2017, 32(12): 2947-2954. doi: 10.13224/j.cnki.jasp.2017.12.018

高旋转数下不同通道转角梯形带肋回转通道的换热特性

doi: 10.13224/j.cnki.jasp.2017.12.018
基金项目: 上海市科学技术委员会资助项目(14DZ1104600)

Heat transfer characteristics in twopass ribroughened trapezoidal channel at high rotation number with different model orientation angles

  • 摘要: 为研究截面形状和旋转效应对高压涡轮动叶内部冷却通道换热的影响,对雷诺数为10000~50000,旋转数为0~209,通道转角为0°、225°、45°的带直肋双流程梯形截面通道换热特性进行了实验研究。结果表明:静止状态下,在第一通道,梯形通道后缘换热强于前缘;在第二通道,前、后缘换热区别不大,后缘的换热略强于前缘。旋转状态下,对0°通道转角,随旋转数的增大,第一通道的后缘面换热仍强于前缘面和外侧面,且差异更明显;第二通道前缘换热相对后缘增强。在较高旋转数(旋转数大于1)时,0°通道转角工况的换热最强,45°转角最弱。

     

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出版历程
  • 收稿日期:  2016-10-02
  • 刊出日期:  2017-12-28

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