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流动参数对合成射流控制叶栅流动分离的影响

谢永慧 屈焕成 何海宇

谢永慧, 屈焕成, 何海宇. 流动参数对合成射流控制叶栅流动分离的影响[J]. 航空动力学报, 2013, 28(3): 636-645.
引用本文: 谢永慧, 屈焕成, 何海宇. 流动参数对合成射流控制叶栅流动分离的影响[J]. 航空动力学报, 2013, 28(3): 636-645.
XIE Yong-hui, QU Huan-cheng, HE Hai-yu. Influence of flow parameters on flow separation control of cascade with synthetic jet[J]. Journal of Aerospace Power, 2013, 28(3): 636-645.
Citation: XIE Yong-hui, QU Huan-cheng, HE Hai-yu. Influence of flow parameters on flow separation control of cascade with synthetic jet[J]. Journal of Aerospace Power, 2013, 28(3): 636-645.

流动参数对合成射流控制叶栅流动分离的影响

基金项目: 国家高技术研究发展计划(2009AA04Z102);西安交通大学基本科研业务费(xjj20100127);“教育部新世纪优秀人才”支持计划(NCET-07-0682)

Influence of flow parameters on flow separation control of cascade with synthetic jet

  • 摘要: 采用大涡模拟方法、结构化网格建立了低压高负荷透平Pak B叶栅的非稳态数值分析模型,研究了不同流动参数对合成射流控制叶栅流动分离的影响.控制前随着雷诺数的减小和气流攻角的增大,叶栅流动分离区域变大,在气流攻角为5°下发生分离未在尾缘前再附的情况.合成射流控制后,不同流动参数下的流动分离都得到了有效的控制,并且在射流偏角为30°时,合成射流控制效果最好.合成射流使叶栅吸力面的流动分离位置推迟,再附位置前移,分离泡尺寸减小,叶栅吸力面的逆压梯度段缩短,吸力面边界层表面的剪切层在向下游迁移的过程中,没有发生充分的抬升,避免了大尺度涡旋的形成,并且很快地黏附于壁面,进而有效地控制了流动分离.

     

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出版历程
  • 收稿日期:  2012-04-04
  • 刊出日期:  2013-03-28

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