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基于半无限引压管效应的动态压力测量方法

杨林 王偲臣 林峰 李继超 聂超群

杨林, 王偲臣, 林峰, 李继超, 聂超群. 基于半无限引压管效应的动态压力测量方法[J]. 航空动力学报, 2014, (10): 2457-2463. doi: 10.13224/j.cnki.jasp.2014.10.024
引用本文: 杨林, 王偲臣, 林峰, 李继超, 聂超群. 基于半无限引压管效应的动态压力测量方法[J]. 航空动力学报, 2014, (10): 2457-2463. doi: 10.13224/j.cnki.jasp.2014.10.024
YANG Lin, WANG Si-chen, LIN Feng, LI Ji-chao, NIE Chao-qun. Method of dynamic pressure measurement based on semi-infinite pressure tube effect[J]. Journal of Aerospace Power, 2014, (10): 2457-2463. doi: 10.13224/j.cnki.jasp.2014.10.024
Citation: YANG Lin, WANG Si-chen, LIN Feng, LI Ji-chao, NIE Chao-qun. Method of dynamic pressure measurement based on semi-infinite pressure tube effect[J]. Journal of Aerospace Power, 2014, (10): 2457-2463. doi: 10.13224/j.cnki.jasp.2014.10.024

基于半无限引压管效应的动态压力测量方法

doi: 10.13224/j.cnki.jasp.2014.10.024
基金项目: 

国家自然科学基金(51176188)

详细信息
    作者简介:

    杨林(1988- ),男,浙江台州人,硕士生,主要从事气动测量技术研究.

  • 中图分类号: V211.71

Method of dynamic pressure measurement based on semi-infinite pressure tube effect

  • 摘要: 实验研究了动态压力信号在有限和半无限引压管腔中传播的幅频特性及其与引压管结构变化的规律性关联.采用半无限引压管结构设计了头部为基尔整流罩的动态总压探针,测量大角度来流的气流总压,并对其动态传递函数进行标定.对一台轴流压气机转子尾迹的测量结果显示:动态总压探针可以测量到转子尾迹的总压流场特征,获得叶片端区流动等大梯度总压流场.对于采用引压管腔的动态探针设计中管径变化和弯曲造成信号能量的衰减作用,半无限引压管效应可有效减小动态压力信号的能量衰减,并减弱管腔的谐振效应.

     

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出版历程
  • 收稿日期:  2013-07-05
  • 刊出日期:  2014-10-28

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