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.
引用
收藏
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 [J].
BENKREIRA, H ;
EDWARDS, MF ;
WILKINSON, WL .
CHEMICAL ENGINEERING SCIENCE, 1981, 36 (02) :429-434
[4]   FILM-SPLITTING FLOWS IN FORWARD ROLL COATING [J].
COYLE, DJ ;
MACOSKO, CW ;
SCRIVEN, LE .
JOURNAL OF FLUID MECHANICS, 1986, 171 :183-207
[5]  
COYNE JC, 1970, ASME, V92, P451
[6]   MENISCUS SHAPE EXPERIMENTS IN FORWARD ROLL COATING [J].
DECRE, M ;
GAILLY, E ;
BUCHLIN, JM .
PHYSICS OF FLUIDS, 1995, 7 (03) :458-467
[7]   MODELING AND ANALYSIS OF MENISCUS ROLL COATING [J].
GASKELL, PH ;
SAVAGE, MD ;
SUMMERS, JL ;
THOMPSON, HM .
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 [J].
GREENER, J ;
MIDDLEMAN, S .
INDUSTRIAL & ENGINEERING CHEMISTRY FUNDAMENTALS, 1979, 18 (01) :35-41
[10]  
GREENER J, 1975, POLYM ENG SCI, V15, P1