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高位垂直进气径向出流旋转盘腔风阻效应的实验 被引量:1

Experimental investigation on frictional loss in shrouded rotating disk with high-positioned air inflow
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摘要 用实验的方法对高位垂直进气转静系旋转盘的风阻效应进行了研究,研究结果表明:转盘无量纲力矩系数随着旋转雷诺数的增加而减小;转盘无量纲力矩系数随着流量系数的增加而增加;且与冷却的具体结构有关;在高旋转雷诺数时,转盘无量纲力矩系数小于自由盘无量纲力矩系数;当流量为0时,无量纲力矩系数的数值全部小于自由盘之值。 The experimental results of the friction effect on shrouded rotating disk with high positioned air flow are presented. The result shows that the dimensionless moment coefficient (NMC) of the rotor decreases with the increase of rotational Reynolds number, but the extent decreases with the increase of rotational Reynolds number. The NMC of the rotor increases with the increase of dimensionless cooling flow rate and differs with different structure of the cooling system. When the rotational Reynolds number reaches a certain value or the dimensionless cooling flow rate is zero, the NMC of the rotor is less than that of the free disk.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2006年第6期1008-1011,共4页 Journal of Aerospace Power
关键词 航空、航天推进系统 旋转盘 流动 摩擦阻力 实验 aerospace propulsion system; rotating disk; flow; friction loss; experi ments
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参考文献4

  • 1曹玉章,陶智,徐国强,等.航空发动机传热学[M].北京:北京航空航天大学出版社,2005.
  • 2徐国强,陶智,丁水汀,朱谷君.高位垂直进气旋转盘流动与换热的实验研究[J].航空动力学报,2000,15(2):164-168. 被引量:12
  • 3Dorfamn L A.Hydrodynamic resistance and the heat loss of rotating solids[M].Oliver and Boyd Ltd,1963.
  • 4Owen J M,Rogers R H.Flow and heat transfer in rotating disk system[M].UK:Research Studies Press,1989.

二级参考文献3

  • 1Phadke U P,Owen J M.Areodynamic Aspects of the Sealing of Gas-Turbine Rotor-Stator Systems: Part Ⅰ-The Behavior of Simple Shrouded Rotating-Disk Systems in a Quiescent Environment[].International Journal of Heat and Fluid Flow.1988
  • 2Ko S H,Rhode D L.Thermal Details in a Rotor-Stator Cavity at Engine Conditions with a Mainstream[].Journal of Turbomachinery.1992
  • 3Bunker R S,Metzger D E,Wittig S.Local Heat Transfer in Turbine Disk Cavities: Part Ⅱ-Rotor Cooling With Radial Location Injection of Coolant[]..

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