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改进的多级涡轮噪声经验预测模型

纪良 乔渭阳 王良峰 英基勇

纪良, 乔渭阳, 王良峰, 英基勇. 改进的多级涡轮噪声经验预测模型[J]. 航空动力学报, 2015, 30(5): 1210-1218. doi: 10.13224/j.cnki.jasp.2015.05.024
引用本文: 纪良, 乔渭阳, 王良峰, 英基勇. 改进的多级涡轮噪声经验预测模型[J]. 航空动力学报, 2015, 30(5): 1210-1218. doi: 10.13224/j.cnki.jasp.2015.05.024
JI Liang, QIAO Wei-yang, WANG Liang-feng, YING Ji-yong. Improved empirical prediction model for multi-stage turbine noise[J]. Journal of Aerospace Power, 2015, 30(5): 1210-1218. doi: 10.13224/j.cnki.jasp.2015.05.024
Citation: JI Liang, QIAO Wei-yang, WANG Liang-feng, YING Ji-yong. Improved empirical prediction model for multi-stage turbine noise[J]. Journal of Aerospace Power, 2015, 30(5): 1210-1218. doi: 10.13224/j.cnki.jasp.2015.05.024

改进的多级涡轮噪声经验预测模型

doi: 10.13224/j.cnki.jasp.2015.05.024
基金项目: 

国家自然科学基金(51276149)

详细信息
    作者简介:

    纪良(1985-),男,江苏宜兴人,博士生,研究领域为叶轮机气动声学.E-mail:cainiaojl@sina.com

  • 中图分类号: V231

Improved empirical prediction model for multi-stage turbine noise

  • 摘要: 基于早期的涡轮噪声经验预测模型和涡轮噪声试验数据,对影响涡轮噪声的关键涡轮参数进行了分析,发展了改进的多级涡轮噪声经验预测模型.该模型由单级涡轮噪声计算、涡轮噪声在下游涡轮级中传播的衰减量计算和各级涡轮噪声叠加3个部分组成.采用涡轮噪声试验数据对单级涡轮噪声计算方法进行了验证.结果表明:该单级涡轮噪声计算方法的计算结果误差小于1.5dB.由试验数据拟合得到的涡轮噪声叶片排衰减经验预测模型也被应用于该改进的多级涡轮噪声经验预测模型中.与早期经验预测模型相比,改进模型的计算方法更合理,噪声预测结果更可靠.

     

  • [1] Batard H.Aircraft noise reduction:airbus industrial needs in terms of new materials for nacelle liners[EB/OL].[2003-03-16].Http://hathor.onera.fr/congres/jso2003matbruit/pdfs/AIRBUS-HBatard.pdf.
    [2] Nesbitt E.Towards a quieter low pressure turbine:design characteristics and prediction needs[J].Aeroacoustics, 2011, 10(1):1-16.
    [3] 赵磊.涡轮气动-声学一体化设计理论及方法研究[D].西安:西北工业大学, 2012. ZHAO Lei.Theory and method investigation of the aerodynamic-acoustics integration design in turbine[D].Xi'an:Northwestern Polytechnical University, 2012.(in Chinese)
    [4] Smith M J T, Bushell K W.Turbine noise:its significance in the civil aircraft noise problem[R].ASME Paper 69-WA/GT-12, 1969.
    [5] Dunn D G, Peart N A.Aircraft noise source and contour estimation[R].NASA CR-114649, 1973.
    [6] Krejsa E A, Valerino M F.Interim prediction method for turbine noise[R].NASA TM X-73566, 1976.
    [7] Kazin S B.Core engine noise control program:Vol Ⅰ identification of component noise sources[R].Federal Aviation Administration, FAA Report DOT-FA72WA-3023, 1974.
    [8] Kazin S B.Core engine noise control program:Vol Ⅱ identification of noise generation and suppression mechanisms[R].Federal Aviation Administration, FAA Report DOT-FA72WA-3023, 1974.
    [9] Kazin S B.Core engine noise control program:Vol Ⅲ prediction methods[R].Federal Aviation Administration, FAA Report DOT-FA72WA-3023, 1974.
    [10] Matta R K, Sandusky G T, Doyle V L.GE core engine noise investigation:low emission engines[R].Federal Aviation Administration, FAA-RD-77-4, 1977.
    [11] Mathews D C, Peracchio A A.Progress in core engine and turbine noise technology[R].AIAA 74-948, 1974.
    [12] Mathews D C, Nagel R T.Review of theory and methods for turbine noise prediction[R].AIAA 75-540, 1975.
    [13] Morin B, Atassi O.An empirical model for turbine noise prediction[R].Columbia:Aero Acoustics Research Consortium, AARC Turbine Noise Workshop, 2008.
    [14] Tyler J M, Sofrin T G.Axial flow compressor noise studies[R].Society of Automotive Engineers, SAE Technical Paper 620532, 1962.
    [15] Heidmann M F.Interim prediction method for fan and compressor source noise[R].NASA TM-75-25948, 1975.
    [16] Fisk W S.Supersonic transport noise reduction technology summary:Phase Ⅰ[R].Federal Aviation Administration, DOT/FAA Report FAA-SS-72-43, 1972.
    [17] Tibbetts J G.Near-field noise prediction for aircraft in cruising flight[R].NASA CR-159105, 1977.
    [18] JI Liang, QIAO Weiyang, ZHAO Lei.An investigation of the inlet and exhaust noise sources of turbofan using linear microphone array[R].AIAA-2013-2296, 2013.
    [19] Burdsall E A, Brochu F P, Scaramella V M.Results of acoustic testing of the JT8D-109 refan engines[R].NASA CR-134875, 1975.
    [20] Grande E.Core engine noise[R].AIAA 73-1026, 1973.
    [21] Doyle V L, Matta R K.Attenuation of upstream generated low frequency noise by gas turbines[R].NASA CR-135219, 1977.
    [22] Cherry D G, Gay C H, Lenahan D T.Energy efficient engine:low pressure turbine test hardware detailed design report[R].NASA CR-167956, 1982.
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出版历程
  • 收稿日期:  2013-12-09
  • 刊出日期:  2015-05-28

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