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轴流风扇/压气机管道周向声模态的测量

王良锋 乔渭阳 纪 良 余索远

王良锋, 乔渭阳, 纪 良, 余索远. 轴流风扇/压气机管道周向声模态的测量[J]. 航空动力学报, 2014, 29(4): 917-926. doi: 10.13224/j.cnki.jasp.2014.04.024
引用本文: 王良锋, 乔渭阳, 纪 良, 余索远. 轴流风扇/压气机管道周向声模态的测量[J]. 航空动力学报, 2014, 29(4): 917-926. doi: 10.13224/j.cnki.jasp.2014.04.024
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

轴流风扇/压气机管道周向声模态的测量

doi: 10.13224/j.cnki.jasp.2014.04.024
基金项目: 

国家自然科学基金(51276149)

详细信息
    作者简介:

    王良锋(1986-),男,河南洛阳人,博士生,主要从事叶轮机械气动声学研究. E-mail:wlfzxlgnl@126.com

  • 中图分类号: V232.4

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

  • 摘要: 利用管道内部周向均匀分布的麦克风阵列对某单级风扇在高背景噪声和较大硬壁反射条件下的管道周向声模态进行了实验测量.利用与参考信号互相关(CC)模态分解技术和传统的方均根(RMS)模态分解技术得到了主要的周向声模态振幅.通过与Tyler和Sofrin的理论分析对比,发现在高背景噪声和较大硬壁反射条件下,两种模态分解技术都能获得较为理想的模态分解结果;并且发现CC模态分解技术获得的模态振幅较低,初步分析这是由于和RMS模态分解技术相比,CC模态分解技术可以降低随机噪声对模态振幅分解结果的影响.此外,周向麦克风个数大于所要分解周向声模态阶数的4倍时,使用CC模态分解技术获得的模态振幅误差可以控制在1dB之内.

     

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出版历程
  • 收稿日期:  2013-01-24
  • 刊出日期:  2014-04-28

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