期刊文献+

Modal Decomposition for the Analysis of the Rotor-stator Interactions in Multi-stage Compressors 被引量:2

Modal Decomposition for the Analysis of the Rotor-stator Interactions in Multi-stage Compressors
原文传递
导出
摘要 A modal analysis method of the rotor-stator interactions in multistage compressors has been developed by LMFA. This method, based on a double modal decomposition of the flow over space and time, has been applied to nu- merical and experimental results of the high-speed 3Y2-stage compressor CREATE based at LMFA, Lyon-France. It reveals the presence of a very strong rotor-stator interaction which completely drives the flow at casing behind all the rotors. This modal analysis method applied to an unsteady RANS simulation permits to calculate the en- ergy of the rotor-stator interactions and to plot energetic meridian maps to explain experimental results and to analyze the interaction in the whole machine.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第3期276-285,共10页 热科学学报(英文版)
基金 the CNRS and the company Snecma (SAFRAN) which support the compressor CREATE research program
关键词 rotor-stator interactions modal analysis multistage compressors numerical and experimental results 多级压缩机 模态分解 转子 定子 交互作用 模态分析 相互作用 雷诺平均
  • 相关文献

参考文献12

  • 1J.M.Tyler et T.G.Sofrin,Axial Flow Compressor Noise Studies,SAE International,620532,Warrendale,PA,1962.
  • 2R.Mailach et K.Vogeler,Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part I:Un-steady Profile Pressures and the Effect of Clocking,Journal of Turbomachinery,vol.126,No.4,p.507,2004.
  • 3R.Mailach,L.Mul ler,et K.Vogeler,Rotor-Stator In-teractions in a Four-Stage Low-Speed Axial Compres-sor—Part II:Unsteady Aerodynamic Forces of Rotor and Stator Blades,Journal of Turbomachinery,vol.126,No.4,p.519,2004.
  • 4X.Ottavy,I.Trébinjac,A.Vouillarmet,et D.Arnaud,Laser measurements in high speed compressors for ro-tor-stator interaction analysis,Journal of Thermal Sci-ence,vol.12,No.4,pp.310 317,2003.
  • 5M.Ernst,A.Michel,et P.Jeschke,Analysis of Ro-tor-Stator-Interaction and Blade-to-Blade Measurements in a Two Stage Axial Flow Compressor,Journal of Turbomachinery,vol.133,No.1,p.011027,2011.
  • 6D.Arnaud,X.Ottavy,et A.Vouillarmet,Experimental Investigation of the Rotor-Stator Interactions Within a High-Speed,Multi-Stage,Axial Compressor:Part 2 — Modal Analysis of the Interactions,presented at the ASME Turbo Expo 2004:Power for Land,Sea,and Air,Vienna,Austria,2004,pp.915 924.
  • 7N.Gourdain,X.Ottavy,et A.Vouillarmet,Experi-mental and numerical investigation of unsteady flows in a high speed three stages compressor,presented at the 8th European Turbomachinery Conference,Graz,Austria,2009.
  • 8J.J.Adamczyk,Model Equation for Simulating Flows in Multistage Turbomachinery,NASA,USA,1984.
  • 9A.Touyeras et M.Villain,Aerodynamic Design and Test Result Analysis of a Three Stage Research Com-pressor,presented at the ASME Turbo Expo 2004:Power for Land,Sea,and Air,Vienna,Austria,2004,pp.589 597.
  • 10M.Mersinligil,J.-F.Brouckaert,N.Courtiade,et X.Ot-tavy,A High Temperature High Bandwidth Fast Re-sponse Total Pressure Probe for Measurements in a Mul-tistage Axial Compressor,presented at the ASME Turbo Expo 2011:Power for Land,Sea,and Air,Van-couver,Canada,2011.

同被引文献14

引证文献2

二级引证文献1

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