Volume 23 Issue 1
Jan.  2008
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XIONG Jin-song, HOU An-ping, YUAN Wei, ZHOU Sheng. Some discuss on technology trend and aerodynamics problem of adjustable blade[J]. Journal of Aerospace Power, 2008, 23(1): 112-116.
Citation: XIONG Jin-song, HOU An-ping, YUAN Wei, ZHOU Sheng. Some discuss on technology trend and aerodynamics problem of adjustable blade[J]. Journal of Aerospace Power, 2008, 23(1): 112-116.
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Some discuss on technology trend and aerodynamics problem of adjustable blade

  • National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 2006-12-28
  • Rev Recd Date: 2007-05-22
  • Publish Date: 2008-01-28
    Abstract
  • Current adjustable blade application in military aero-engine was discussed and the further development trend was predicted.High load,high mach number,broad flow angle range,and low flow loss level will be pursued.Aerodynamic analysis was carried out on a flectional cascade.It indicates that flectional cascade is an excellent solution for turning angle control in compressors.But still more work is needed on advanced adjustable cascade with higher turning angle and higher mach number.

     

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    • References(4)
  • [1]
    Louis M L,Jerry R W,Adam J M,et al.Aerodynamic design study of advanced multistage axial compressor[R].NASA-TP 2002-211568,ARL-TR-2859.
    [2]
    Baligand B,Garnier B,Mathioudakis K,et al.Gas turbine health monitoring demonstrator[R].Proc.2nd Int.Conf.on Acoustical and Vibratory Surveillance Methods and Diagnostic Techniques,SFM/IMEKO/SFA-SEMLIS,Oct.10-12,1995:521-531.
    [3]
    Tsalavoutas A,Mathioudakis K,Stamatis A,et al.Identifying faults in the variable geometry system of a gas turbine compressor[J].Journal of Turbomachinery,2006,128(4):786-797.
    [4]
    Wennerstrom A L,Hearsey R M.The design of an axial compressor stage for a total pressure ration of 3 to 1[R].ARL-71-TR-0061,1971.
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