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Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

TIAN Xiao-pei SHAN Peng

TIAN Xiao-pei, SHAN Peng. Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors[J]. 航空动力学报, 2013, 28(7): 1526-1538.
引用本文: TIAN Xiao-pei, SHAN Peng. Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors[J]. 航空动力学报, 2013, 28(7): 1526-1538.
TIAN Xiao-pei, SHAN Peng. Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors[J]. Journal of Aerospace Power, 2013, 28(7): 1526-1538.
Citation: TIAN Xiao-pei, SHAN Peng. Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors[J]. Journal of Aerospace Power, 2013, 28(7): 1526-1538.

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

基金项目: Programme of Introducing Talents of Discipline to Universities(B08009)

Two 3-D multi-cascade co-design inverse methods based on streamline curvature approach and Clebsch formulation for single-stage centrifugal compressors

Funds: Programme of Introducing Talents of Discipline to Universities(B08009)
  • 摘要: Two strategies extended the single-cascade methods from a compressible three-dimensional inverse method for radial and mixed flow turbomachines to two three-dimensional multi-cascade co-design methods for single-stage centrifugal compressors.These two three-dimensional methods and a typical quasi-three-dimensional streamline curvature through-flow inverse method were employed to design the same subsonic high-speed single-stage centrifugal compressors.The compressor performances were simulated by a commercial Reynolds averaged Navier-Stokes (RANS) equations solver.The studies show that two three-dimensional co-design methods are reasonable and feasible.It was found that:firstly the blade camber angle designed by the three-dimensional methods was larger than that designed by the quasi-three-dimensional method;and secondly with regard to two three-dimensional methods with different boundary conditions,the co-design result differences between the diffusers were small,but those between the deswirlers were relatively large.

     

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出版历程
  • 收稿日期:  2012-10-07
  • 刊出日期:  2013-07-28

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