Stagnation-saddle points and flow patterns in Stokes flow between contra-rotating cylinders

被引:20
作者
Gaskell, PH [1 ]
Savage, MD
Thompson, HM
机构
[1] Univ Leeds, Sch Mech Engn, Leeds LS2 9JT, W Yorkshire, England
[2] Univ Leeds, Dept Phys & Astron, Leeds LS2 9JT, W Yorkshire, England
关键词
D O I
10.1017/S0022112098002031
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The steady flow is considered of a Newtonian fluid, of viscosity mu, between contra-rotating cylinders with peripheral speeds U-1 and U-2 The two-dimensional velocity field is determined correct to O(H-0/2R)(1/2), where 2H(0) is the minimum separation of the cylinders and R an 'averaged' cylinder radius. For flooded/moderately starved inlets there are two stagnation-saddle points, located symmetrically about the nip, and separated by quasi-unidirectional flow. These stagnation-saddle points are shown to divide the gap in the ratio U-1 : U-2 and arise at \X\ = A where the semi-gap thickness is H(A) and the streamwise pressure gradient is given by dP/dX = mu(Ulf U-2)/H-2(A). Several additional results then follow. (i) The effect of non-dimensional flow rate, lambda: A(2) = 2RH(0)(3 lambda - 1) and so the stagnation-saddle points are absent for lambda < 1/3, coincident for lambda = 1/3 and separated for lambda > 1/3. (ii) The effect of speed ratio, S = U-1/U-2: stagnation-saddle points are located on the boundary of recirculating flow and are coincident with its leading edge only for symmetric flows (S = i). The effect of unequal cylinder speeds is to introduce a displacement that increases to a maximum of O(RH0)(1/2) as S --> 0. Five distinct flow patterns are identified between the nip and the downstream meniscus. Three are asymmetric flows with a transfer jet conveying fluid across the recirculation region and arising due to unequal cylinder speeds, unequal cylinder radii, gravity or a combination of these. Two others exhibit no transfer jet and correspond to symmetric (S = 1) or asymmetric (S not equal 1) flow with two asymmetric effects in balance. Film splitting at the downstream stagnation-saddle point produces uniform films, attached to the cylinders, of thickness H-1 and H-2, where H-1/H-2 = S(S + 3)/3S + 1, provided the flux in the transfer jet is assumed to be negligible. (iii) The effect of capillary number, Ca: as Ca is increased the downstream meniscus advances towards the nip and the stagnation-saddle point either attaches itself to the meniscus or disappears via a saddle-node annihilation according to the flow topology. Theoretical predictions are supported by experimental data and finite element computations.
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页码:221 / 247
页数:27
相关论文
共 23 条
  • [1] [Anonymous], COMPUTATIONAL ANAL P
  • [2] BALLAL BY, 1976, ARCH RATION MECH AN, V62, P237, DOI 10.1007/BF00280016
  • [3] ROLL COATING OF PURELY VISCOUS-LIQUIDS
    BENKREIRA, H
    EDWARDS, MF
    WILKINSON, WL
    [J]. CHEMICAL ENGINEERING SCIENCE, 1981, 36 (02) : 429 - 434
  • [4] FILM-SPLITTING FLOWS IN FORWARD ROLL COATING
    COYLE, DJ
    MACOSKO, CW
    SCRIVEN, LE
    [J]. JOURNAL OF FLUID MECHANICS, 1986, 171 : 183 - 207
  • [5] COYNE JC, 1970, ASME, V92, P451
  • [6] MENISCUS SHAPE EXPERIMENTS IN FORWARD ROLL COATING
    DECRE, M
    GAILLY, E
    BUCHLIN, JM
    [J]. PHYSICS OF FLUIDS, 1995, 7 (03) : 458 - 467
  • [7] MODELING AND ANALYSIS OF MENISCUS ROLL COATING
    GASKELL, PH
    SAVAGE, MD
    SUMMERS, JL
    THOMPSON, HM
    [J]. JOURNAL OF FLUID MECHANICS, 1995, 298 : 113 - 137
  • [8] GASKELL PH, 1998, UNPUB PHYS FLUIDS
  • [9] THEORETICAL AND EXPERIMENTAL STUDIES OF THE FLUID-DYNAMICS OF A 2-ROLL COATER
    GREENER, J
    MIDDLEMAN, S
    [J]. INDUSTRIAL & ENGINEERING CHEMISTRY FUNDAMENTALS, 1979, 18 (01): : 35 - 41
  • [10] GREENER J, 1975, POLYM ENG SCI, V15, P1