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压气机转子叶片所受激励的相关性

方立成 李舜酩 杜建建 陈茉莉

方立成, 李舜酩, 杜建建, 陈茉莉. 压气机转子叶片所受激励的相关性[J]. 航空动力学报, 2011, 26(6): 1289-1294.
引用本文: 方立成, 李舜酩, 杜建建, 陈茉莉. 压气机转子叶片所受激励的相关性[J]. 航空动力学报, 2011, 26(6): 1289-1294.
FANG Li-cheng, LI Shun-ming, DU Jian-jian, CHEN Mo-li. Study on the correlative property of excitation on compressor rotor blades[J]. Journal of Aerospace Power, 2011, 26(6): 1289-1294.
Citation: FANG Li-cheng, LI Shun-ming, DU Jian-jian, CHEN Mo-li. Study on the correlative property of excitation on compressor rotor blades[J]. Journal of Aerospace Power, 2011, 26(6): 1289-1294.

压气机转子叶片所受激励的相关性

基金项目: 国家自然科学基金(50675099)

Study on the correlative property of excitation on compressor rotor blades

  • 摘要: 为了分析复杂流场对叶片的作用,研究了压气机内三种非定常气动激振形式:上游叶片排尾迹、进气畸变和旋转失速的相关性.通过在单级低速轴流压气机试验台上获得的数据,采用自相关和互相关方法,研究三种激励的特性,分析激振信号的相关性机理.结果表明:多次自相关可以清晰地显示出信号的特征频率,有效地抑制干扰噪声;激励信号之间具有很强的相关性,且相关程度主要由偶数阶激励信号产生;两两激励信号之间的互相关频率成分幅值较低,低于各信号的自谱图在该处的幅值;而三个激励信号之间的相关程度较低,其相关性主要存在于偶数阶激励信号的前两阶.

     

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出版历程
  • 收稿日期:  2010-05-26
  • 修回日期:  2011-01-12
  • 刊出日期:  2011-06-28

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