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燃气轮机压气机涡量动力学理论及分析方法

吴宏 蒋洪德

吴宏, 蒋洪德. 燃气轮机压气机涡量动力学理论及分析方法[J]. 航空动力学报, 2013, 28(4): 903-910.
引用本文: 吴宏, 蒋洪德. 燃气轮机压气机涡量动力学理论及分析方法[J]. 航空动力学报, 2013, 28(4): 903-910.
WU Hong, JIANG Hong-de. Theory and analysis method based on vorticity dynamics for gas turbine compressor[J]. Journal of Aerospace Power, 2013, 28(4): 903-910.
Citation: WU Hong, JIANG Hong-de. Theory and analysis method based on vorticity dynamics for gas turbine compressor[J]. Journal of Aerospace Power, 2013, 28(4): 903-910.

燃气轮机压气机涡量动力学理论及分析方法

Theory and analysis method based on vorticity dynamics for gas turbine compressor

  • 摘要: 阐述了压气机涡量动力学理论及分析方法,建立了压气机总性能参数与两个重要的涡量参数(边界涡量流(BVF)和周向涡量)的直接数学物理关系,研究了基于BVF和周向涡量的分析优化方法.将该方法应用于燃气轮机多级轴流压气机中进行涡量动力学分析,从涡量角度指出了改进的方向.结果表明:周向涡量能反映近壁面的高损失区,使周向涡量峰值束缚在近壁区有利于降低端区损失,在通流设计中可通过优化环量分布控制周向涡量分布,算例中基于周向涡量优化可使跨声压气机转子效率提高1.13%;边界涡量流BVF能反映旋涡的壁面根源,通过优化BVF的分布可控制涡量壁面根源,有利于抑制旋涡和流动分离,基于BVF优化可使转子效率提高1.12%.

     

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出版历程
  • 收稿日期:  2012-04-27
  • 刊出日期:  2013-04-28

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