期刊文献+

双旋转盘腔压力特性实验 被引量:2

Experiment on pressure characteristics of dual rotating cavities
原文传递
导出
摘要 将压力传感器安装在测点测量几何结构复杂的双旋转盘腔转盘表面的压力分布及盘腔进出口的总压损失.实验结果表明:当湍流参数由0.1变化到0.4时,转盘表面的压力先随旋转雷诺数的增大而减小,之后随旋转雷诺数的增大而增大,并且转变的湍流参数对于两个转盘是不同的.在相同湍流参数下,旋转雷诺数决定了转盘表面的压力分布曲线形状;两个旋转腔的总压损失随湍流参数的增大而增大,随旋转雷诺数的变化规律不同,右旋转腔两个入口到出口的总压损失随旋转雷诺数的变化规律也有差异. Pressure distribution and total pressure loss were measured by fixed transduc ers on proper positions of dual rotating cavities. The results show that with turbulent flow parameter varying from 0.1 to 0.4, the pressure on rotating disk decrease with the increas ing rotational Reynolds number at first, and then increases with the increasing rotational Reynolds number. The critical turbulent flow parameters for these two cavities are different. Under the same turbulent flow parameter, rotational Reynolds number dominates the shape of pressure distribution curves on the rotating disk surfaces. When turbulent flow parameter increases, total pressure losses of two cavities become larger. But when rotational Reynolds number increases under the same turbulent flow parameter, total pressure losses of these two cavities are different.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2013年第10期2267-2275,共9页 Journal of Aerospace Power
关键词 旋转盘腔 压力分布 总压损失 压力传感器 旋转系 rotating cavity pressure distribution total pressure losspressure transducer rotating system
  • 相关文献

参考文献15

  • 1Owen J M,Pincombe J R. Velocity measurements inside a rotating cylindrical cavity with a radial outflow of fluid[J]. Journal of Fluid Mechanics,1980,99(1) :111-127.
  • 2Owen J M, Rogers R H. Flow and heat transfer in rota- ting-disc systems: Volume 2 rotating cavities [M]. New York: Research Studies Press, 1995 : 65-106.
  • 3Ong C L,Owen J M. Prediction of heat transfer in a rota- ting cavity with a radial outflow[J]. Journal of Turboma- chinery, 1991,113(1) : 115-122.
  • 4Karabay H,Chen J X, Pilbrow R, et al. Flow in a "cover- plate" preswirl rotor-stator system[J]. Journal of Turbo- machinery, 1999,121(1) :160-166.
  • 5Karabay H, Pilbrow R, Wilson M, et al. Performance of pre-swirl rotating-disc systems[J]. Journal of Engineering for Gas Turbines and Power,2000,122(3):442-450.
  • 6Karabay H,Wilson M,Owen J M. Predicitons of effect of swirl on flow and heat transfer in a rotating cavity[J]. In- ternational Journal of Heat and Fluid Flow, 2001,22 (2) 143-155.
  • 7Pilbrow R,Karabay H,Wilson M,et al. Heat transfer in a "cover-plate" preswirl rotating-disk system[J]. Journal of Turbomachinery, 1999,121(4) : 249-255.
  • 8Peter R N C. Rotating flowEM]. New York.. Research Studies Press, 2011 : 281-285.
  • 9Flow in rotating components: discs, cylinders and cavities [R]. Sussex, UK: The Institution of Mechanical Engi- neers, ESDU 07004,2010.
  • 10张东,丁水汀,陶智,徐国强,宁磊.旋转系下的实时压力测量方法研究[J].航空动力学报,2003,18(2):244-247. 被引量:6

二级参考文献12

共引文献20

同被引文献12

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