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旋转矩形截面弯管内流动特性的研究 被引量:9

Research on the characteristics of the fluid flow in rotating curved rectangular duct
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摘要 本文利用数值计算方法研究了三种旋转矩形截面 ( η =1,η >1,η <1)弯管内的粘性流动 ,分析了在离心力和科氏力共同作用下二次流动、轴向主流、摩擦系数比随各参数的变化情况 ,所得的结果与已有文献的结果 (数值结果和实验结果 )非常吻合。计算结果表明 :对于宽高比 η 1的矩形截面 ,截面上最多可以存在 8个涡 ;若 η >1,截面上最多可以出现 6个涡 ;摩擦系数比和二次流函数最大值在F≈ - 1时取得最小值 ;计算结果还表明 ,η对高速旋转弯管内的摩擦系数比的影响程度要明显高于对静止的弯管内的摩擦系数比的影响程度 ,最后本文给出 η An incompressible viscous steady flow through a rotating curved rectangular duct is studied numerically employing the control volume integral method. The combine effects of the Coriolis force (due to rotation) and the centrifugal force (due to curvature) on the flow structure and the fraction factor ratio are examined in detail for three type rectangular duct: η>1,η=1,η<1 , where η is the aspect ratio. The structures of the flow are studied during the range -2.0F1.0 , where F represents the ratio of the Coriolis force to the centrifugal force, De =400 and 100 for η=1 , only De =400 for η ≠1. In this range, The complicated secondary flow vortices are obtained. For η 1, the most number of the secondary cell is eight and for η>1 , this number is six. The maximum of axial velocity is pushed either outside or inside, which depends on the value of F . The fraction factor ratio reaches its minimum value that is almost 1 at F ≈-1 and the effects of η on the fraction factor ratio depend on R o . It is also shown when R o is small, the fraction factor ratio decreases rapidly against R o and the contours of axial velocity are almost uniform along the y axis and has a shape like dumbbell.
机构地区 浙江大学力学系
出处 《空气动力学学报》 CSCD 北大核心 2001年第2期135-147,共13页 Acta Aerodynamica Sinica
关键词 旋转管道 曲线管道 二次流动 旋转矩形 截面弯管 流动特性 流体力学 secondary flow rotating pipe curved pipe
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参考文献10

  • 1张金锁,章本照.旋转弯管内粘性流动特性的研究[J].空气动力学学报,2000,18(3):336-344. 被引量:4
  • 2Yang W J,Appl Mech Rev,1994年,47卷,367页
  • 3THANGA M S,J Fluid Mech,1990年,217卷,421页
  • 4牟乃让,流体力学与传热学基础,1984年
  • 5Ghia K N,Trans ASMEJ Fluids Engineering,1977年,99卷,640页
  • 6Cheng K C,Trans ASMEJ Fluids Engineering,1976年,98卷,41页
  • 7Mori Y,Int J Heat Mass Transfer,1971年,14卷,1787页
  • 8Cheng K C,Int J Heat Mass Transfer,1970年,13卷,471页
  • 9Ludwieg H,Ingenieur Archiv,1951年,19卷,296页
  • 10Zhang J S,Int J Heat Fluid Flow

二级参考文献1

  • 1Dr. H. Ludwieg. Die ausgebildete Kanalstr?mung in einem rotierenden System[J] 1951,Ingenieur - Archiv(4-5):296~308

共引文献3

同被引文献68

  • 1郭治民,张会强,王希麟,郭印城,林文漪.用简化的联合PDF模型计算CH_4扩散燃烧[J].工程热物理学报,2002,23(S1):213-216. 被引量:3
  • 2HUANG Yi1, ZHANG JianHui1, HU XiaoQi1, XIA QiXiao2, HUANG WeiQing1 & ZHAO ChunSheng1 1 Department of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China,2 Department of Mechanical and Electrical Engineering, Beijing Union University, Beijing 100020, China.Dynamics analysis and experiment on the fishtailing type of valveless piezoelectric pump with rectangular vibrator[J].Science China(Technological Sciences),2010,53(12):3241-3247. 被引量:10
  • 3彭拾义.燃烧效率的研究[J].燃气轮机技术,1994,7(4):50-53. 被引量:1
  • 4李志强.燃烧过程辐射换热离散坐标模型的应用[J].航空动力学报,2006,21(2):320-325. 被引量:8
  • 5SPALDING D,MATHEMATICAL B.Models of turbulent flames[J].Combustion Science and Technology,1976,13:3-25.
  • 6TAGAWA M,MATSUBARA F,OHTA Y.Heat transfer characteristics of a non-premixed turbulent flame formed in a currved rectangular duct[J].Combustion and Flame,2002,129:151-163.
  • 7TAGAWA M,FUKATSU M.NABATA Y,et al.Thermal-field structure of a non-premixed turbulent flame formed in a strong pressure-gradient flow[J].Int J Heat and Fluid Flow,2005,26:905-913.
  • 8YAKHOT V,ORZAG S A.Renormalization group analysis of turbulence:basic theory[J].J Scient Comput,1986,1(1):3-11.
  • 9POPE S B.PDF methods for turbulent reactive flows[J].Prog Energy Combust Sci,1985,11(2):119-192.
  • 10POPE S B.New developments in PDF modeling of nonreactive and reactive turbulent flows[C] // Proceeding of the Second International Symposium on Turbulent,Heat and Transfer.Delft,Netherlands:Delft University Press,1997:35-45.

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