期刊文献+

EXPERIMENTAL INVESTIGATION FOR THE EFFECT OF ROTATION ON THREE-DIMENSIONAL FLOW FIELD IN FILM-COOLED TURBINE 被引量:2

EXPERIMENTAL INVESTIGATION FOR THE EFFECT OF ROTATION ON THREE-DIMENSIONAL FLOW FIELD IN FILM-COOLED TURBINE
下载PDF
导出
摘要 An experimental investigation of three-dimensional flow field in a film-cooled turbine model is carried out by using particle image velocimeter (PIV) in a low-speed wind tunnel. The effects of different blowing ratios (M=1.5, 2) on the flow field are studied. The experimental results reveal the classical phenomena of the formation of kidney vortex pair and secondary flow in wake region behind the jet hole. And the changes of the kidney vortex pair and the wake at different locations away from the hole on the suction and pressure sides are also studied. Compared with the flow field in stationary cascade, there are centrifugal force and Coriolis force existing in the flow field of rotating turbine, and these forces bring the radial velocity in the jet flow. The effect of rotatien on the flow field of the pressure side is more distinct than that on the suction side from the measured flow fields in Y-Z plane and radial velocity contours. The increase of blowing ratio makes the kidney vortex pair and the secondary flow in the wake region stronger and makes the range of the wake region enlarged. An experimental investigation of three-dimensional flow field in a film-cooled turbine model is carried out by using particle image velocimeter (PIV) in a low-speed wind tunnel. The effects of different blowing ratios (M=1.5, 2) on the flow field are studied. The experimental results reveal the classical phenomena of the formation of kidney vortex pair and secondary flow in wake region behind the jet hole. And the changes of the kidney vortex pair and the wake at different locations away from the hole on the suction and pressure sides are also studied. Compared with the flow field in stationary cascade, there are centrifugal force and Coriolis force existing in the flow field of rotating turbine, and these forces bring the radial velocity in the jet flow. The effect of rotatien on the flow field of the pressure side is more distinct than that on the suction side from the measured flow fields in Y-Z plane and radial velocity contours. The increase of blowing ratio makes the kidney vortex pair and the secondary flow in the wake region stronger and makes the range of the wake region enlarged.
出处 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2007年第1期10-15,共6页 中国机械工程学报(英文版)
基金 This project is supported by National Natural Science Foundation ofChina(No. 50406017)
关键词 Film-cooled turbine rotor PIV measurement Blowing ratio Three-dimensional flow field Film-cooled turbine rotor PIV measurement Blowing ratio Three-dimensional flow field
  • 相关文献

参考文献2

二级参考文献3

共引文献10

同被引文献18

  • 1DU H ,EKKAD S V ,HAN J C. Effect of unsteady wake with trailing edge coolant ejection on detailed heat transfer coefficient distributations for a gas turbine blade [ J ]. ASME Journal of Heat Transfer, 1997,119 : 242 - 248.
  • 2AZZI A, LAKEttAL D. Perspectives in modeling film cooling of turbine blades by transcending conventional two-equation turbulence models [ J ]. ASME Journal of Turbomachinery, 2002, 124 : 472 - 484.
  • 3蒋雪辉.非定常尾迹对气膜冷却的影响研究[D].北京:中国科学院工程热物理研究所,2004.
  • 4GARG V K. Heat transfer on a film-cooled rotating blade using different turbulence models [ J ]. International Journal of Heat Mass Transfer, 1999,42:789 - 802.
  • 5GARG V K, RIGBY D LHeat transfer on a film-cooled blade-effect of hole physics [ J ]. International Journal Heat and Fluid Flow, 1999,20 : 10 - 25.
  • 6GARG V K. Heat transfer on a film-cooled rotating blade [ J ]. International Journal of Heat and Fluid Flow,2000,21:134 - 145.
  • 7GARG V K. Modeling film-coolant flow characteristics at the exit of shower-head holes [ J ]. International Joornal of Heat and Fluid Flow ,2001,22 : 134 - 142.
  • 8GARG V K, AMERI A A. Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade [ J ]. Internationa[ J].rnal of Heat and Fluid Flow,2001,22:593 -602.
  • 9GARG V K. Adiabatic effectiveness and heat transfer coefficient on a film-cooled rotating blade [ J ]. International Journal of Heat and Fluid Flow, 1997,32:811 - 830.
  • 10HYLTON L D, MILHEC M S ,TURNER E R, et al. Analytical and experimental evaluation of the heat transfer distribution over the surface of turbine vanes[ R]. NASA - CR - 168015, 1983.

引证文献2

二级引证文献6

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