期刊文献+

柔性管与紊流耦合的减阻特性 被引量:4

BEHAVIOR ON DRAG REDUCING BY COUPLING FLEXIBLE TUBES WITH TURBULENT FLOW
下载PDF
导出
摘要 为探讨柔性管与紊流耦合的减阻特性和初步机理,使用双重管结构,对柔性管的减阻特性进行试验研究,采用激光传感测位仪对柔性管外壁的位移脉动特性及其与柔性管减阻率之间的相关性进行研究。结果表明,壁厚越小,雷诺数越大,柔性管减阻率越大;在双重管结构及雷诺数约为3×10^4时,壁厚为2mm、3mm及4mm柔性管的减阻率依次约为16%、11%、9%;管外壁位移脉动的低频方均根值与减阻率存在正相关关系;在高雷诺数下,由于使用理论模型计算的管径膨胀引起的减阻率偏低,单重管的减阻率比实际值偏高。 In order to probe into the mechanism and behavior of drag reducing by coupling flexible tubes with turbulent flow, experimental investigation is performed on behavior of turbulent drag reduction using flexible tubes with sleeve-structure, and the fluctuating displacement characters of tubes at the outer wall and their relations with the drag reduction rates are studied by using laser displacement sensor. The results are found as follows. The thinner the flexible tubes are or the bigger the Reynolds number is, the bigger the drag reduction rates by coupling flexible tubes with turbulent flow are. At the Reynolds number of about 3×10^4 , the rates of drag reduction of the sleeve-structured flexible tubes with thickness of 2, 3, 4 mm are about 16%, 11%, 9% respectively. A positive correlation exists between the drag reduction rates and the root mean square of fluctuating displacement in low frequency band at the outer wall of simple tubes. With simple tubes and at the big Reynolds number, the rates of drag reduction of the flexible tubes are bigger than their true values, as the drag reduction rates, which are caused by the inside expansion of the tubes and obtained by using the theoretical formula, are much lower.
出处 《机械工程学报》 EI CAS CSCD 北大核心 2007年第10期41-45,共5页 Journal of Mechanical Engineering
基金 国家自然科学基金(50374087) 湖南省教育厅(06C265)资助项目。
关键词 柔性管 双重管 耦合 脉动位移 紊流减阻 Flexible tubes Tubes with sleeve-structure Coupling Fluctuating displacement Turbulent drag-reduction
  • 相关文献

参考文献11

  • 1KRAMER M O. Boundary layer stabilization by distributed damping[J]. Am. Soc. Nav. Engrs., 1960, 6(72):25-33.
  • 2STEIN P D, WALBURM F J. Damping effect of distensible tubes on turbulent flow[J]. Biorheology, 1980, 17 (3):275-280.
  • 3BTLICK E F, WALTERS R R. Turbulent boundary layer characteristics of compliant surfaces[J]. Aircraft, 1988,4 (5):11-17.
  • 4LEE T, FISHER M, SCHWARZ W H. Investigation of stable interaction of a passive compliant surface with a turbulent boundary layer[J]. Fluid Mech., 1993, 36(257): 373-401.
  • 5BUSHNELL D M. Effect of compliant wall motion on turbulent boundary layers[J]. Phys. Fluids, 1977, 20 (10): 31-47.
  • 6赵汉中.柔性壁对湍流边界层速度型的变形影响[J].水动力学研究与进展(A辑),2002,17(4):391-399. 被引量:8
  • 7王玉春,姜楠,周兴华,舒玮.柔性壁面湍流边界层相干结构控制的实验研究[J].实验力学,2004,19(1):45-50. 被引量:4
  • 8NAKAO S A, SUZUKI M. Numerical study of drag reduction by compliant walls[J]. Trans. Jpn. Soc. Aero. Space Sci., 1985, 27 (78): 195-201.
  • 9福原岩坪.弹性管による摩擦抵抗軽減に関する実驗研究[J].日本機械学会論文集,1993,59(568):104-108.
  • 10ARAKAWA M. Critical Reynolds numbers for the flow in flexible tubes[J]. Transaction Japanese Society Biorheology, 1982, 48 (5): 226-232.

二级参考文献15

  • 1CHO1 K S X.Turblent drag reduction using compliant[J]. Proc R Soc Lond, 1997,453:2229-2240.
  • 2方義.長谷川.希薄高分子水溶液の冈管内流れにぉける摩擦損失と压力变動特性[J].日本機械学會論文集B,1996,62(598):59-63.
  • 3伊藤ら.界面活性剂水溶液の乱流境界层れにぉける速度埸計测[J].日本機械学會論文集B,2004,70(693):22—29.
  • 4FUKUHARA M. Experiment study on drag reduction using flexible[ J ]. JSME International Journal Series B, 1998,41 ( 1 ) : 77-85.
  • 5中林,伊藤.流体力学(粘性編)[M].東京:株式会社コロナ,1993:70—79.
  • 6[1]LEE T, FISHER M & SCHWARZ W H. Investigation of stable interaction of a passive compliant surface with a turbulent boundary layer[J]. J. Fluid Mech. , 1993, 257: 373-401.
  • 7[2]GAD-EL-HAK M. The response of elastic and viscoelastic surfaces to a turbulent boundary[J]. Trans.ASME, Ser. E: J. Appl. Mech. , 1986, 53: 206-212.
  • 8[3]GAD-EL-HAK M, BLACKWELDER R F & RILEY. J J. On the interaction of compliant coatings with boundary-layer flow[J]. J. Fluid Mech. , 1984, 140: 257-280.
  • 9[4]CHOI K S, YANG X, CLAYTON B R, et al. Turbulent drag reduction using compliant surfaces[J].Proc. Roy. Soc. London, Ser. A,1997, 453: 2229-2241.
  • 10[1]Kline S J, Reynolds W C, Schraub F A, Runstadlter P W. The structure of turbulent boundary layer [J]. J. Fluid Mech., 1967,30:741~774

共引文献11

同被引文献132

引证文献4

二级引证文献33

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