期刊文献+

高频响气动探针研究综述 被引量:4

A Review of the Study on High Frequency Response Aerodynamic Probe
下载PDF
导出
摘要 为了应对高效发电趋势,提高汽轮机和燃气轮机的效率,必须对动叶流场气动性能进行准确的测量和分析。高频响气动探针可以有效的对涡轮机械中三维非定常流场进行时间分辨测量。而探针的研制主要涉及探头形状、大小,气动腔动态特性,标定以及数据后处理。文中对这几个方面的国内外研究现状和发展趋势进行了详细阐述,总结了它们各自的特点、适用范围和局限性,并指出了今后的研究方向以及难点所在,为相关科研人员进一步开展探针理论分析、数值模拟研究和应用设计提供参考。 In order to improve the efficiency of steam turbine and gas turbine,it is necessary to measure accurately the aerodynamic performance of the flow field,expecially the unsteady flow field.The high frequency response aerodynamic probe can effectively measure the three-dimensional unsteady flow field in turbomachinery.The development of high frequency response probe mainly involves the shape and size of probe,dynamic characteristics of pneumatic cavity,calibration and data post-processing.In this paper,the research status and development trend of the probe in these aspects were reviewed.The respective characteristics,scope of application and limitations of high frequency response probes were summarized,and the development directions and difficulties in the future were pointed out,which provides reference for relevant researchers to further carry out theoretical analysis,numerical research and application design.
作者 李新年 周骛 蔡小舒 LI Xinnian;ZHOU Wu;CAI Xiaoshu(University of Shanghai for Science and Technology,Yangpu District,Shanghai 200093,China)
机构地区 上海理工大学
出处 《中国电机工程学报》 EI CSCD 北大核心 2020年第19期6246-6256,共11页 Proceedings of the CSEE
基金 国家科技重大专项(2017-V-0016-0069)。
关键词 涡轮机械 非定常压力测量 探针设计 高频响应 动态特性分析 turbomachinery unsteady pressure measurement probe design high frequency response dynamic characteristic analysis
  • 相关文献

参考文献10

二级参考文献115

  • 1张训文,陈曦,朱琦,方继明.压力传感器管腔效应问题研究[J].测试技术学报,2002,16(z1):387-390. 被引量:8
  • 2郭勇,王效葵,王洪伟.高频压力探针动态性能的补偿方法[J].航空动力学报,2005,20(2):273-277. 被引量:9
  • 3Ligrani P, Singer B, Baun L. Miniature five-hole pressure probe for measurement of three mean velocity components in low-speed flows[J]. Journal of Physics E: Scientific Instruments, 1989,22 : 868- 876. 被引量:1
  • 4Morrison G, Schobeiri M, Pappu K. Five-hole pressure probe analysis technique[J]. Flow Measurement and In strumentation, 1998,9 : 153-158. 被引量:1
  • 5Johansen E,Rediniotis O,Jones G. The compressible calibration of miniature multi hole probes[J]. Journal of Fluids Engineering, 2001,123 : 128 -138. 被引量:1
  • 6Rediniotis O, Chrysanthakopoulos G. Application of neural networks and fuzzy logic to the calibration of the seven hole probe[J]. ASME Journal of Fluid Engineering, 1998, 120:95-101. 被引量:1
  • 7Rediniotis O,Viiayagopal R. Miniature multihole pressure probes and their neural network-based calibration [J]. AIAA Journal, 1999,37(6):666-674. 被引量:1
  • 8Fan H, Lu W, Xi G, et al. An improved neural-networkbased calibration method for aerodynamic pressure probes [J].Journal of Fluids Engineering, 2003,125:113-120. 被引量:1
  • 9Pisasale A, Ahmed N. Development of a functional relationship between port pressures and flow properties for the calibration and application of multihole probes to highly three-dimensional flows[J].Experiments in Fluids, 2004,36 : 422-436. 被引量:1
  • 10[1]Gyarmathy G.Grundlagen einer theorie der nassdampfturbine[D].Zurich,ETH,1962. 被引量:1

共引文献204

同被引文献36

引证文献4

二级引证文献3

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部