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低速轴流压气机转子叶片三维优化的数值研究

张晨凯 胡骏 王志强 尹超 严伟

张晨凯, 胡骏, 王志强, 尹超, 严伟. 低速轴流压气机转子叶片三维优化的数值研究[J]. 航空动力学报, 2015, 30(2): 483-490. doi: 10.13224/j.cnki.jasp.2015.02.028
引用本文: 张晨凯, 胡骏, 王志强, 尹超, 严伟. 低速轴流压气机转子叶片三维优化的数值研究[J]. 航空动力学报, 2015, 30(2): 483-490. doi: 10.13224/j.cnki.jasp.2015.02.028
ZHANG Chen-kai, HU Jun, WANG Zhi-qiang, YIN Chao, YAN Wei. Numerical study on three-dimensional optimization of low-speed axial compressor rotor blade[J]. Journal of Aerospace Power, 2015, 30(2): 483-490. doi: 10.13224/j.cnki.jasp.2015.02.028
Citation: ZHANG Chen-kai, HU Jun, WANG Zhi-qiang, YIN Chao, YAN Wei. Numerical study on three-dimensional optimization of low-speed axial compressor rotor blade[J]. Journal of Aerospace Power, 2015, 30(2): 483-490. doi: 10.13224/j.cnki.jasp.2015.02.028

低速轴流压气机转子叶片三维优化的数值研究

doi: 10.13224/j.cnki.jasp.2015.02.028
基金项目: 

高等学校博士学科点专项科研基金(20123218120009)

详细信息
    作者简介:

    张晨凯(1987-),男,江苏丹阳人,博士生,研究方向为叶轮机械气动热力学.

  • 中图分类号: V231.3

Numerical study on three-dimensional optimization of low-speed axial compressor rotor blade

  • 摘要: 为了深入认识低速大尺度轴流压气机端壁区的流动,减小流动损失,提高其气动性能,采用数值模拟和优化相结合的手段,针对用于低速模拟的某低速大尺度轴流压气机原型转子的三维积叠线进行了优化,提高了其设计工况下的气动性能.结果表明:优化转子轮毂附近无法承受过大的负荷;相比于原型转子,优化转子主要的性能提升位于轮毂附近,一定程度的正弯有效减小了轮毂区的流动损失,具有“前加载”的效果,抑制了叶根尾缘的流动分离,转子总压损失减小约19.4%.

     

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出版历程
  • 收稿日期:  2013-09-18
  • 刊出日期:  2015-02-28

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