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不同进口雷诺数下双旋流杯下游回流区特征

于博文 张弛 杨谦 许全宏 林宇震

于博文, 张弛, 杨谦, 许全宏, 林宇震. 不同进口雷诺数下双旋流杯下游回流区特征[J]. 航空动力学报, 2016, 31(4): 823-829. doi: 10.13224/j.cnki.jasp.2016.04.008
引用本文: 于博文, 张弛, 杨谦, 许全宏, 林宇震. 不同进口雷诺数下双旋流杯下游回流区特征[J]. 航空动力学报, 2016, 31(4): 823-829. doi: 10.13224/j.cnki.jasp.2016.04.008
YU Bo-wen, ZHANG Chi, YANG Qian, XU Quan-hong, LIN Yu-zhen. Characteristics of the recirculation zone downstream a dual-swirl cup at varied inlet Reynolds numbers[J]. Journal of Aerospace Power, 2016, 31(4): 823-829. doi: 10.13224/j.cnki.jasp.2016.04.008
Citation: YU Bo-wen, ZHANG Chi, YANG Qian, XU Quan-hong, LIN Yu-zhen. Characteristics of the recirculation zone downstream a dual-swirl cup at varied inlet Reynolds numbers[J]. Journal of Aerospace Power, 2016, 31(4): 823-829. doi: 10.13224/j.cnki.jasp.2016.04.008

不同进口雷诺数下双旋流杯下游回流区特征

doi: 10.13224/j.cnki.jasp.2016.04.008
详细信息
    作者简介:

    于博文(1990-),男,山东济宁人,硕士生,研究领域为燃气轮机燃烧及传热传质.E-mail:dtyubw90@163.com

  • 中图分类号: V231.2

Characteristics of the recirculation zone downstream a dual-swirl cup at varied inlet Reynolds numbers

  • 摘要: 为了分析旋流杯下游流场结构对航空燃气轮机燃烧室性能影响的作用,利用PIV(激光粒子测速仪)技术,在常温常压下对双旋流杯下游冷态流场进行测试,研究进口雷诺数对双旋流杯下游回流区的影响.试验结果表明:当进口雷诺数较低时,下游流场结构为收扩型;当进口雷诺数增大到25000后,流场结构变为扩张型;之后继续增加进口雷诺数,回流区流场结构不再改变,但回流区内的无量纲回流速度会随之增加.

     

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出版历程
  • 收稿日期:  2014-07-24
  • 刊出日期:  2016-04-28

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