Volume 29 Issue 4
Apr.  2014
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WANG Liang-feng, QIAO Wei-yang, JI Liang, YU Suo-yuan. In-duct circumferential acoustic mode measurement of axial fan/compressor[J]. Journal of Aerospace Power, 2014, 29(4): 917-926. doi: 10.13224/j.cnki.jasp.2014.04.024
Citation: WANG Liang-feng, QIAO Wei-yang, JI Liang, YU Suo-yuan. In-duct circumferential acoustic mode measurement of axial fan/compressor[J]. Journal of Aerospace Power, 2014, 29(4): 917-926. doi: 10.13224/j.cnki.jasp.2014.04.024

In-duct circumferential acoustic mode measurement of axial fan/compressor

doi: 10.13224/j.cnki.jasp.2014.04.024
  • Received Date: 2013-01-24
  • Publish Date: 2014-04-28
  • In-duct circumferential acoustic mode of a single stage fan was measured using equidistant microphone array with high back ground noise and high rigid wall reflection. Primary circumferential acoustic mode amplitude was obtained by utilizing the cross-correlated(CC) reference channel mode detection technique and the conventional root mean square-averaging (RMS) mode detection technique. The results were compared with Tyler and Sofrins duct mode theory, finding that both CC mode detection technique and RMS mode detection technique can obtain the ideal mode detection results with high back ground noise and high rigid wall reflection, and the mode amplitude of the former was lower than that of the latter. This is because CC mode detection technique decreases the impact of random noise on the mode amplitude. It is also found that the error of mode amplitude from CC mode detection technique is lower than 1dB when the number of microphone in the circular microphone array is more than four times of the circumferential acoustic mode order.

     

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  • [1]
    乔渭阳.航空发动机气动声学[M].北京:北京航空航天大学出版社,2010.
    [2]
    Joppa P D.Acoustic mode measurements in the inlet of a turbofan engine[J].Journal of Aircraft,1987,24(9):557-593.
    [3]
    Meyer H D,Envia E.Aeroacoustic analysis of turbofan noise generation .NASA CR-4715,1996.
    [4]
    Pickett G F,Sofrin T G,Wells R A.Method of fan sound mode structure determination:final report .NASA CR-135293,1977.
    [5]
    Moore C J.Measurement of radial and circumferential modes in annular and circular fan ducts[J].Journal of Sound and Vibration,1979,62(2):235-256.
    [6]
    Sarin S L,Rademaker E R.In-flight acoustic mode measurements in the turbofan engine inlet of Fokker 100 aircraft .AIAA 93-4414,1993.
    [7]
    Rademaker E D,Sijtsma P,Tester B J.Mode detection with an optimized array in a model turbofan engine intake at varying shaft speeds .AIAA-2001-2181,2001.
    [8]
    Joppa P D.An acoustic mode measurement technique .AIAA 84-2337,1984.
    [9]
    Cicon D E,Sofrin T G,Mathews D C.Investigation of continuously traversing microphone system for mode measurement .NASA CR-168040,1982.
    [10]
    Hall D G,Heidelberg L J,Konno K.Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake:data collection/analysis techniques .AIAA 93-0599,1993.
    [11]
    Sutliff D L.Turbofan duct mode measurements using a continuously rotating microphone rake[J].Aeroacoustics,2007,6(2):147-170.
    [12]
    Sijtsma P,Zillmann J.In-duct and far-field mode detection techniques .AIAA-2007-3439,2007.
    [13]
    Morse P M,Ingard U K.Theoretical acoustics[M].New York:McGraw-Hill Book Company,1968.
    [14]
    Munjal M L.Acoustics of ducts and mufflers with application to exhaust and ventilation system design[M].Hoboken,US:John Wiley & Sons,1987.
    [15]
    Tyler J M,Sofrin T G.Axial flow compressor noise studies[J].Transactions of the Society of Automotive Engineers,1962,70:309-332.
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