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Volume 24 Issue 2
Feb.  1998
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Journal of Beijing University of Aeronautics and Astronautics  > 1998  >  24(2): 174-177.
CHEN Tiantian, ZHAO Gang. Tool path generation for Loop subdivision surface based finish machining[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 663-668. doi: 10.13700/j.bh.1001-5965.2014.0308(in Chinese)
Citation: Cao Renjing, Zhou Sheng. Effects of 3D Flow on Aerodynamic Stability of Axial Flow Compressor[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(2): 174-177. (in Chinese)
shu

Effects of 3D Flow on Aerodynamic Stability of Axial Flow Compressor

  • Beijing University of Aeronautics and Astronautics,Dept. of Jet Propulsion

  • Received Date: 02 Sep 1996
  • Publish Date: 28 Feb 1998
    Abstract
  • Concerning the models for discribing aerodynamic stability of axial flow compressor,the original model is onedimensional,and it is reasonable for the onset of surge only.For the onset of rotating stall,there are just some twodimensional models at published literatures.A threedimensional aerodynamic of compressor has been presented in this paper.An aerodynamic stability model concerning radial disturbance of compressor is presented.The calculated results show that the occurrence of radial disturbance is related to the axial velocity disturbance,which has important effect on aerodynamic stability of compressor.The position of onset of stall,in blade tip or hub,is dependent upon the characteristics of blade element.The comparisons of calculated results predicted by 2D and 3D aerodynamic stability model have also been made in this paper.

     

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    • References(1)
  • 1.Day I J,Cumpsty N A.The measurement and interpretation of flow within rotating stall cells in axial compressors.Journal of Mechanics Engineering Sciences,1978,20:101~114 2. Day I J.Stall inception in axial flow compressors.ASME 91GT86,1991 3. Greitzer E M,Moore F K.A Theory of poststall transients in axial compression system.Prat　ⅡApplication.Transaction of the ASME Journal of Engineering for Gas Turbine and Power,1986.108 4. Lonley J P.A review of nonsteady flow models for compressor stability.ASME 93GT17,1993 5. Zhou S,Li X D,Cao R J.From flow fields in turblomachinery to their mathematical models.In:Mei Z Y,Wu Y L,eds.Proceedings of 2nd International Conference of Pump and Fan.Beijing:Petroleum Industry,1995.1~16
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