Volume 29 Issue 5
May  2014
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HU Ying-jiao, WANG Song-tao. An aerodynamic design method and verification for counter-rotating compressor[J]. Journal of Aerospace Power, 2014, (5): 1135-1144.
Citation: HU Ying-jiao, WANG Song-tao. An aerodynamic design method and verification for counter-rotating compressor[J]. Journal of Aerospace Power, 2014, (5): 1135-1144.

An aerodynamic design method and verification for counter-rotating compressor

  • Received Date: 2013-03-07
  • Publish Date: 2014-05-28
  • An aerodynamic design method combined with boundary layer suction was proposed for counter-rotating compressor. For high-loaded compressor, because of the problems (such as strength problem) caused by boundary layer suction used in the rotating parts, the boundary layer suction was used only in the stator, while the rotor was designed by the low reaction design principle to ensure its efficiency based on the increasing rotor exit axial velocity. A counter-rotating compressor was designed to demonstrate the method above. The three dimensional viscous numerical simulation results show that, two-stage counter-rotating compressor with total pressure ratio of 5.85 and efficiency of 88% is attained at tip tangential speed 370m/s of the first rotor and 350m/s of the second rotor.

     

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