The motion of a single and multiple neutrally buoyant elliptical cylinders in plane Poiseuille flow Shih-Di Chen, Tsorng-Whay Pan, and Chien-Cheng Chang Citation: Phys. Fluids 24, 103302 (2012); doi: 10.1063/1.4757387 View online: http://dx.doi.org/10.1063/1.4757387 View Table of Contents: http://pof.aip.org/resource/1/PHFLE6/v24/i10 Published by the American Institute of Physics. Additional information on Phys. Fluids Journal Homepage: http://pof.aip.org/ Journal Information: http://pof.aip.org/about/about_the_journal Top downloads: http://pof.aip.org/features/most_downloaded Information for Authors: http://pof.aip.org/authors Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions PHYSICS OF FLUIDS 24, 103302 (2012) The motion of a single and multiple neutrally buoyant elliptical cylinders in plane Poiseuille flow Shih-Di Chen,1 Tsorng-Whay Pan,2,a) and Chien-Cheng Chang1,3,a) 1 Institute of Applied Mechanics, National Taiwan University, Taipei 106, Taiwan Department of Mathematics, University of Houston, Houston, Texas 77204, USA 3 Center for Advanced Studies in Theoretical Sciences, National Taiwan University, Taipei 106, Taiwan 2 (Received 16 January 2012; accepted 10 September 2012; published online 12 October 2012) In this article, we investigate the motion of neutrally buoyant elliptical cylinders in plane Poiseuille flow of a Newtonian fluid. The method of distributed Lagrange multiplier/fictitious domain was used to solve the Navier-Stokes equations as well as for the motion of elliptical cylinders. The motion of a single elliptical cylinder is shown to be dependent on the channel Reynolds number Re, the particle size ratio K = a* /H* , and the aspect ratio A = a* /b* of the cylinder, where H* is the half height of the channel, a* and b* are the lengths of the semi-major axis and semi-minor axis of the cylinder, respectively. It is found that there is a critical Reynolds number, Rec ∼ 3, which distinguishes the lateral migration of a single elliptical cylinder below and above it. As Re is increased, the equilibrium position of the elliptical cylinder shifts towards the wall when Re ≤ Rec or shifts closer to the central axis when Re ≥ Rec . Moreover, there are interesting correlations between the center-of-mass trajectories and the orientation dynamics, which depend on the ranges of K and Re. The motion of multiple elliptical cylinders is also affected by the total solid area fraction φ T , which is defined to be the proportion of the area occupied by the cylinders in the domain of computation. For a few elliptical cylinders (the number of cylinders ND = 16 and the corresponding φ T = 3.77%), the cylinders may scatter into several groups at lower Re (≤ 100), and each group fluctuates about an averaged position. At the higher Re (= 1000), the cylinders may converge to an equilibrium position on each side of the channel center. For a larger number of cylinders (ND = 36, 54, 72, 108, and the corresponding φ T = 8.48%–25.45%), we observed a significant rheological behavior in the velocity profiles. In addition, there exists a particle-free layer next to each wall, and the thickness of the particle-free layers is increased as A (or K) or Re is increased. C 2012 American Institute of Physics. [http://dx.doi.org/10.1063/1.4757387] I. INTRODUCTION A flow with rigid neutrally buoyant particles in a simple shear or Poiseuille flow between parallel plates can be simulated to investigate issues such as the fibres in a pulp (ellipse),1 the glutaraldehyde-fixed (rigid) red blood cells in the blood flow (biconcave),2, 3 and other particles of moderate aspect ratios in a similar flow. Understanding the motion of rigid particles in neutrally buoyant flow is important for fundamental developments in suspension rheology. The orientation dynamics of a single particle have been studied widely, from the Stokes limit to finite Reynolds number ranges for a simple shear flow. Jeffery4 considered a single ellipsoid in an unbounded shear flow, neglecting the inertia effect (the particle Reynolds number Rep = Re · K 1), and obtained a set of differential equations for the rotation of the ellipsoid depending on a) Authors to whom correspondence should be addressed. Electronic addresses: [email protected] and [email protected]. 1070-6631/2012/24(10)/103302/25/$30.00 24, 103302-1 C 2012 American Institute of Physics Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-2 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) the initial conditions. The rotation of an ellipsoid is indeterminate, so he hypothesized that “the particle will tend to adopt that motion which, of all the possible motions under the approximated equations, corresponds to ‘the least dissipation of energy.’” However, several later studies by other authors reported cases of maximum dissipation. Karnis, Goldsmith, and Mason5 demonstrated in experiments that the orbits of disks and rods assume maximum dissipation in the Couette flow at small particle Reynolds numbers (3 × 10−4 ≤ Rep ≤ 7 × 10−3 ). Harper and Chang6 demonstrated that even with the restricted class of flows considered by Jeffery, the minimum dissipation hypothesis does not hold. These authors considered the motion of a dumb-bell shape particle in an unbounded shear flow by including the inertia effects at low particle Reynolds numbers (Rep 1). The particle was shown to have a preferred periodic orbit that corresponds to maximum dissipation. Ding and Aidun7 studied numerically the dynamics of an elliptical cylinder suspended in a Couette flow at various particle Reynolds numbers (0.08 ≤ Rep ≤ 40), and showed a transient behavior from being rotary to stationary as the particle Reynolds number is increased. Their numerical findings were also demonstrated experimentally by Zettner and Yoda,8 who studied the motion of an elliptical cylinder in a plane Couette flow apparatus. Subramanian et al.9, 10 investigated the effect of fluid inertia on the orientation of a fibre in a simple shear flow, and also found that above a critical Reynolds number, the fibre ceases to rotate and inclines at a stable orientation. The orientation dynamics of an elliptical cylinder or ellipsoid in the Stokes limit have been studied for not only the Couette flow but also the Poiseuille flow. Chwang and Wu11, 12 solved the Stokes equations by assuming small particle Reynolds numbers (Rep 1) to determine the motion of an ellipsoid in unbounded quadratic flows. They showed that the ellipsoid moves in a straight line parallel to the flow direction, without any side drift, at a variable speed that is governed by a trajectory equation. Sugihara-Seki13 studied numerically the motion of a neutrally buoyant elliptical cylinder in a two-dimensional (2D) Poiseuille flow at small Reynolds numbers (Re 1, Rep 1), and found that an elliptical cylinder is either rotary or oscillatory depending on the particle-to-channel size ratio K, the aspect ratio A of the elliptical cylinder, and the initial condition. On the other hand, the center-of-mass trajectories of a single particle at finite Reynolds number ranges have been investigated more extensively for the Poiseuille flow. Segre and Silberberg14, 15 experimentally studied the lateral migration of dilute suspensions of neutrally buoyant spheres in Poiseuille flow through a tube. The spheres migrate away from the wall and the centerline to accumulate at about 0.6 of the tube radius from the centerline at small but finite Reynolds numbers (Re < 30). Ho and Leal16 examined the motion of a rigid circular cylinder in a 2D Poiseuille flow with inclusion of the inertia effects at small Reynolds numbers (Rep 1) by a regular perturbation method. The circular cylinder reaches a stable lateral equilibrium position independent of the initial location of release, and the position is the Segre–Silberberg position − 0.6 of the channel half-width from the centerline for the Poiseuille flow. Schonberg and Hinch17 studied the inertial migration of a sphere in a Poiseuille flow at the Reynolds numbers of order unity (Re = 1–75, Rep 1), and found that the Segre–Silberberg position moves towards the wall as Reynolds number is increased. In general, it is believed that the migration away from the centerline of the channel is due to an effect of the curvature of velocity profile.18 If we make the approximation that a particle set in the Poiseuille flow has a zero mean velocity relative to the fluid, then owing to the curvature of the velocity field, the fluid velocity will be (absolutely) higher on the wall side than on the centerline. This dissymmetry will cause an excess lower pressure on the side where the velocity of the fluid is higher, leading the particle to migrate away from the axis. For a particle moving parallel to a wall, the pressure field around the particle will be greater on the wall side, so the wall tends to repel the particle. The particle will therefore reach the equilibrium position when the forces due to the curvature effect and the wall repulsion strike a balance in the Poiseuille flow.19 Feng et al.18 investigated the motion of neutrally buoyant and non-neutrally buoyant 2D circular cylinders in plane Poiseuille flows using a finite-element method and obtained qualitative agreements with the results of perturbation theories and experiments. The center-of-mass trajectories of an elliptical cylinder or ellipsoid have been investigated less than that of a circular one or sphere in previous studies. Zhao and Sharp20 investigated the rotational stability of an elliptical cylinder in 2D Poiseuille flow for different aspect ratios, transverse locations, and Reynolds numbers (Re = 1.5–30) by calculating the lift and torque. They found that stationary orientations could be reached for a higher aspect ratio, and Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-3 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) also suggested that increased Re may result in more stationary orientations. Pan et al.21 simulated the motion of an ellipsoid in neutrally buoyant 3D Poiseuille flows and found that its rotation exhibits distinctive states depending on the Reynolds number ranges and the shape of the ellipsoid. In spite of these previous studies, the relationship between the orientation dynamics and the center-of-mass trajectory is not clear. When the number of the particles is increased, the particle-particle interactions can cause a rheological effect. Leighton and Acrivos22 reported on the particle-particle interaction in a concentrated suspension of neutrally buoyant spheres, and provided the first evidence for the existence of a nonuniform equilibrium concentration distribution in a Couette flow at zero particle Reynolds number (Rep < 10−4 ). Nott and Brady23 simulated the pressure-driven flow in a channel for the suspensions of neutrally buoyant spheres at zero particle Reynolds number (Rep 1). They observed that even if one starts from a random distribution of sphere locations, the spheres gradually migrate towards the center of the channel, resulting in an inhomogeneous distribution and a blunting of the particle velocity profile. Han and Kim24 investigated the motion of spheres in the tube flow of suspensions for a wide range of solid volume fractions and particle Reynolds numbers (Rep = 0.05–0.376) experimentally. They found that as the total solid volume fraction is increased, the flow velocity profile and the particle velocity profile are more blunted than the initial parabolic profiles at higher solid volume fraction conditions, and the spheres concentrate round the center of the tube. Cohen et al.25 studied particle interactions of the hard-sphere colloidal particles in a highly confined geometry by confocal microscopy, and showed that geometric confinement leads to the ordered but highly non-equilibrium structure. Humphry et al.26 also studied the effects of particle concentration and channel geometry on inertial focusing, and showed that both the location and the number of focusing positions depend on the number of particles per unit length along the channel. Matas et al.27 studied the migration of dilute suspensions of spheres (φ T < 1%) in a tube flow at Reynolds numbers Re = 76–1700. They observed other inner equilibrium positions closer to the center, and found that most of the spheres cluster round either the Segre–Silberberg equilibrium positions or the inner equilibrium position. However, they were unable to determine whether this inner equilibrium position is a real equilibrium position in a steady state or simply a transient feature. Recent advances in computational sciences allow direct simulations of complicated solid-fluid interactions. Direct numerical simulations have been used to study the motion of particles in shear flows. Pan and Glowinski28 simulated the motion of circular cylinders in neutrally buoyant 2D flows, and confirmed that collisions between cylinders play a key role in driving cylinders to the central region of plane Poiseuille flow. For a multiple array of particles, the interactions between the particles in the rear and front are more complicated, but mainly because a rear particle in the wake of a front one may experience less drag29 and touch the front particle at later times.28 This study is aimed to investigate the motion of a single and multiple neutrally buoyant elliptical cylinders via mutual interactions. In this article, we consider the effects of the aspect ratio (A) and the cylinder-to-channel size ratio (K) on the equilibrium position, translational velocity and angular velocity of a single cylinder under various Reynolds numbers (Re). The present interest also extends to multi-elliptical cylinders under various conditions: the number of cylinders ND varying from 4 to 108 (the total solid area fraction φ T = 0.94%–25.45%) with A from 1 to 3.333, K from 0.11 to 0.2, and Re from 10 to 1000. The rest of the article is structured as follows. In Sec. II, we introduce the governing equations of the model problem concerning a single or multiple rigid neutrally buoyant elliptical cylinders moving freely in a two-dimensional Poiseuille flow. Then in Sec. III, we briefly describe the method used in this study – the distributed Lagrange multiplier/fictitious domain method (DLM/FD) developed by Glowinski et al.28, 30–32 In Sec. IV, we present and discuss the numerical results of the cases of a single and multiple elliptical cylinders in five parts. Section IV A provides the validation of a single elliptical cylinder in plane Couette flow. In Sec. IV B, we focus on the motion of a single elliptical cylinder in plane Poiseuille flow and its dependence on the effects of the aspect ratio A, the size ratio K of the cylinder, and the Reynolds number Re. The motion of a few elliptical cylinders (the number of cylinders ND = 16, and the total solid area fraction φ T = 3.77%) in plane Poiseuille flow and its dependence on the effects of the Reynolds number Re are investigated in Sec. IV C. We examine, in Sec. IV D, the motion of many elliptical cylinders (ND = 72, φ T = 16.96%) in plane Poiseuille flow and its dependence on the effects of the aspect Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-4 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) FIG. 1. (a) Model for validation: Schematic of single rigid elliptical cylinder in plane Couette flow. (b) Focus problem of this study: Schematic of multiple rigid elliptical cylinders in plane Poiseuille flow with the domain of computation D* = (L* × 2H* ). ratio A and the Reynolds number Re with particular emphasis on the rheological behaviors, and in Sec. IV E, the thickness of the particle-free layer yf on the effects of the total solid area fraction φ T (= 0.94%–25.45% and ND = 4–108), the aspect ratio A, and the Reynolds number Re. The main results are summarized in the Concluding Remarks. II. DESCRIPTION OF THE PROBLEM Figures 1(a) and 1(b) show the validation model of a single rigid neutrally buoyant elliptical cylinder in a Couette flow (as shown in Fig. 1(a)) and the focus problem of multiple rigid neutrally buoyant elliptical cylinders in plane Poiseuille flow (as shown in Fig. 1(b)). In these plots, a* and b* are the lengths of the semi-major axis and semi-minor axis of the cylinder; A = a* /b* is the aspect ∗ is ratio of the cylinder; H* is the half height of the channel; L* is the length of the channel; Umax the maximum velocity of Couette flow or plane Poiseuille flow (without the existence of cylinders); (X ∗p , y ∗p ) is the center location of each cylinder; θ denotes the orientation of the major axis, or the angle of inclination (i.e., the angle the semi-major axis makes with the x-axis); and ∗p is the angular velocity of the elliptical cylinder. The fluid-particle system is governed by the Navier-Stokes equations for the fluid and (the ∗ ∗ , 2H* /Umax , and Euler-)Newton’s equations for rigid body motions. In this study, we take 2H* , Umax ∗ ∗ * μ f Umax /2H to be the characteristic length, translational speed, time, and pressure, respectively, where μ∗f is the dynamic viscosity of the fluid. A normalized physical quantity or variable is denoted by the same letter for the dimensional quantity or variable but without an asterisk. The dimensionless governing equations are given by30 ∂u + (u · ∇) u = −∇ p + ∇ 2 u, Re (1) ∂t dU p 6 = Geg + α Re (2) [− pl + τ ] · nd, dt πK3 60 dω = x − X p × ([− pl + τ ] · n) d, (3) α Re 5 dt πK Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-5 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) where denotes the boundary of the solid cylinder. In these equations, u is the fluid velocity; Up is the particle velocity; ω(= p ) is the speed of rotation of the cylinder; τ is the shear stress; p is the pressure; α = ρ ∗p /ρ ∗f is the mass density ratio, where ρ ∗p and ρ ∗f are the mass densities of the cylinder and fluid, respectively; eg is the unit vector in the direction of gravitation; and K = a* /H* is the size ratio. In addition, we defined two dimensionless parameters as follows: Re = and G= ∗ (2H ∗ ) ρ ∗f Umax μ∗f , the Reynolds number, ρ ∗p − ρ ∗f g ∗ (2H ∗ )2 ∗ μ∗f Umax , the gravity number, (4) (5) where g* is the gravitation acceleration. Since the cylinders are neutrally buoyant in plane Couette and Poiseuille flow in this study, G is zero. The flow is periodic in the x-direction, and the no-slip condition is applied on the top and bottom walls. Equations (2) and (3) are described for a single elliptical cylinder; their generalization to multiple cylinders is straightforward. III. NUMERICAL METHOD In this section, we briefly describe the numerical method used in this study for simulating particulate flows, and refer the readers to the cited references for details. The method of solution is actually a combination of a distributed Lagrange-multiplier-based fictitious domain method (DLM) and the operator splitting methods. The basic idea is to imagine that the fluid fills the entire space inside as well as outside the particle boundaries. The fluid-flow problem is then posed on a larger domain (the “fictitious domain”). This larger domain is simpler, allowing a simple regular mesh to be used, which in turn renders use of some specialized fast solution techniques. The larger domain is also time-independent, so the same mesh can be used for the entire simulation, eliminating the need for repeated re-meshing and projection. The fluid inside the particle boundary must exhibit a rigid-body motion. This constraint is enforced using the distributed Lagrange multiplier, which represents the additional body force per unit volume needed to maintain the rigid-body motion inside the particle boundary, much like the pressure in incompressible fluid flow, whose gradient is the force required to maintain the constraint of incompressibility. For space discretization, we use P1 -iso-P2 and P1 finite elements for the velocity field and pressure, respectively (like in Bristeau et al.33 ). In time advancing, many operator splitting schemes can be applied to the problem based on the Lagrange multiplier/fictitious domain method. We apply the Lie scheme to obtain a sequence of sub-problems for each time step (see Ref. 28 for details). The computational method has been validated in our previous study28 for the motion of neutrally buoyant disks in Poiseuille flow. In this paper, we extend the method to the case of elliptical cylinders moving in Poiseuille flow. IV. RESULTS AND DISCUSSION A. Validation of an elliptical cylinder in plane Couette flow We consider the motion of a neutrally buoyant elliptical cylinder in plane Couette flow, which was considered by Ding and Aidun.7 Their results were obtained by the lattice Boltzmann equation. The domain of computation is D = (5 × 1), the aspect ratio A = 2, and the size ratio K = 0.2 for this study (note that K = 0.1 for Ding’s work). The flow is periodic in the x-direction, and the top and bottom boundaries are the no-slip u(x,0) = 1 and u(x,1) = 0. The mesh size is h = 1/320, and the time step is t = 0.001. The definition of the particle Reynolds number in the Couette flow is the same as Ding and Aidun,7 Rep = Re · K. In Fig. 2, we can see that the computational results are in good agreement with Jeffery’s solution4 for Rep = 0 and the ones obtained by Ding and Aidun for Rep = 0.08 and 1.0, respectively. Figure 3 shows the normalized minimum angular velocity ωmin /π and the period of rotation T versus Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-6 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) FIG. 2. Validation of the computational results: The figure shows comparisons in both angle of inclination and angular velocity of an elliptical cylinder. Orientation θ /π versus time t: (a) our result (solid line) at Rep = 0.08; (b) Ding’s result (dashed line) at Rep = 0.08; (c) our result at Rep = 1; (d) Ding’s result at Rep = 1. Angular velocity ω/π versus time t: (e) our result at Rep = 0.08; (f) Ding’s result at Rep = 0.08; (g) our result at Rep = 1; (h) Ding’s result at Rep = 1. Jeffery’s solutions for θ p versus t: Jθ = θ /π , and for ω versus t: Jω = ω/π at Rep = 0 are also plotted for comparisons. The domain of computation is D = (5 × 1); the size ratio K = 0.2 for this study and K = 0.1 for Ding’s work; the aspect ratio A = 2. FIG. 3. Normalized minimum angular velocity ωmin /π (straight line) and period of rotation T (curve) versus Rep of an elliptical cylinder. It is noted that T increases to infinity as Rep approaches the critical value Rep,c ∼ 29. The domain of computation is D = (5 × 1); the size ratio K = 0.2 for this study and K = 0.1 for Ding’s work; the aspect ratio A = 2. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-7 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) Rep . The normalized minimum angular velocity ωmin /π decreases as Rep is increased with a nearly straight line relationship, where Rep,c = 29 is the critical particle Reynolds number, above which the rotational motion is stopped. It is also noted that the period of rotation T of the elliptical cylinder with the larger size ratio (K = 0.2) is shorter than that of the smaller one (K = 0.1) at Rep = 28; the cross of the two curves of K = 0.1 and 0.2 shows that a larger size ratio promotes rotation beyond a certain Re ∼ 25. B. The motion of a single elliptical cylinder in plane Poiseuille flow We consider the motion of a single neutrally buoyant elliptical cylinder in a pressure-driven plane Poiseuille flow. The domain of computation is D = (L × 1); A = 1.875, and K = 0.15 of the cylinder. The flow is periodic in the x-direction, and the pressure gradient is 8, which gives a driving force to the flow field. The fluid and cylinder are initially at rest. The initial y-coordinate of the center of the elliptical cylinder is 0.4. The mesh size is h = 1/256, and the time step is t = 0.01. We calculate the lateral migration of the elliptical cylinder by changing the length of the channel (L = 1, 2, 4, 6) at the Reynolds numbers Re = 10, 100, 1000, respectively. The results show that in the shorter channels (L = 1, 2), the equilibrium position of the elliptical cylinder is much lower than in other cases (L = 4, 6). Since we assume the periodic boundary in the x-direction, the mutual interactions between cylinders in neighboring periods are not negligible for the short channels (L = 1, 2), which is insufficient to recover the flow condition for a single cylinder.34 The cases of L = 4 and L = 6 have about the same equilibrium position at each Re, which means that the hydrodynamic interactions across the periodic boundary do not affect the cylinder motion much. In the following simulations, we choose the length of channel L = 4 to achieve good accuracy and reduce the computational cost. 1. The effect of the shape of the cylinder (A, K) In this section, we vary the shape of a neutrally buoyant elliptical cylinder in a pressure-driven Poiseuille flow. We keep the cross section constant and vary the aspect ratio A, and therefore the size ratio K of the elliptical cylinder. We chose A = 3.333, 2.5, 1.875, 1.2, 1.0, and the corresponding K = 0.2, 0.17, 0.15, 0.12, 0.11 at Re = 10. Figure 4 shows the temporal development of the dimensionless height Yp of the elliptical cylinder for different aspect ratios. Considering the long-time behavior, we observe that the cylinder is eventually fluctuating about an averaged height, denoted by Yeq = Yp . Correspondingly, we define the radial equilibrium position, req = 1/2 − Yeq , in the lower half channel, which measures the average distances of the mass center to the central line of the channel. The relation of the averaged equilibrium position and the aspect ratio of the elliptical cylinder fitted by the least-squares gives req = 0.4801 − 0.002(A − 1) − 0.0025(A − 1)2 , which shows that the equilibrium position of the cylinder with a higher A is closer to the central axis. The mechanism of this lateral migration is related to the balance among the wall repulsion due to lubrication, inertial lift related to shear slip, and lift due to the curvature of the velocity profile in the Poiseuille flow.16, 18, 19, 35 Figures 5(a) and 5(b) show the translational velocities for cylinders of different shapes. The translational velocity of an elliptical cylinder Up in one rotation period reaches the maximum when its major axis is aligned with the direction of flow, and reaches the minimum when its major axis is perpendicular to the direction of flow. We also found that the time-averaged translational velocity Up,avg between 2400 ≤ t ≤ 2500 and the amplitude of oscillation in the translational velocity Up,osc increase with increases in the aspect ratio A as shown in Fig. 6. Figures 7(a) and 7(b) show the normalized angular velocity ω/π of an elliptical cylinder between 2490 ≤ t ≤ 2500, and its averaged value ωs /π over this period for different aspect ratios. The elliptical cylinder is subject to a large torque when it is at a large angle of inclination to the flow direction.36 The higher A corresponds to a lower ωs /π , because the higher A increases the moment arm associated with the pressure force, which produces a relatively larger torque; therefore, ωs /π Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-8 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 0.4 A=3.333, K=0.20 A=2.500, K=0.17 A=1.875, K=0.15 A=1.200, K=0.12 A=1.000, K=0.11 0.38 0.36 Y p 0.34 0.32 0.3 0.28 A 0.26 0.24 0 500 1000 1500 2000 2500 t FIG. 4. Temporal development of lateral migration of an elliptical cylinder with different A and K at Re = 10. is decreased.29 By the least-squares fitting, we obtain the relation of the averaged angular velocity ωs /π and the aspect ratio of cylinder A as ωs /π = 0.3051 − 0.0355(A − 1) − 0.033(A − 1)2 , which shows that the elliptical cylinder with a higher aspect ratio rotates more slowly on average; this tendency is similar to the results of Chwang12 obtained for an ellipsoid in an unbounded quadratic flow. From Jeffery’s orbit, we can obtain the maximum angular velocity ωmax = γ a2 /(a2 +b2 ) at the angles of inclination θ = (n+1/2)π (when the major axis is perpendicular to the flow direction), and the minimum angular velocity ωmin = γ b2 /(a2 +b2 ) at the angles of inclination θ = nπ (when the major axis is aligned with the flow direction), where γ is the shear rate, and n is an integer. We also examine an elliptical cylinder of aspect ratio A = 3 at Re = 10 for different size ratios K = 0.2, 0.4, 0.5, 0.6. In our results, the maximum and minimum angular velocities do occur at angles of inclination close to θ = (n+1/2)π and θ = nπ , respectively; however the values of ωmax and ωmin are somewhat different from Jeffery’s orbits when the size ratio K is greater than 0.4, as shown in Fig. 8. 2. The effect of Reynolds number (Re) In this section, we consider the motion of an elliptical cylinder with A = 1.875 and K = 0.15 at different Reynolds numbers from Re = 0.5 to 1000. Figures 9(a) and 9(b) show the equilibrium position versus Reynolds number with different aspect ratios, and the present results are compared to other studies of 2D and 3D particles. Figure 9(a) shows the equilibrium positions of an elliptical cylinder with the aspect ratio A = 3.333, 1.875, 1 and the size ratio K = 0.2, 0.15, 0.11 at low Re; they all have the same trend. For these three cases, the transition is observed to occur at about Rec = 3, below which the Segre–Silberberg position shifts away from the centerline with increasing Re, and above which the trend is the opposite. Figure 9(b) shows the equilibrium position versus Re with the present result and the other studies of 2D and 3D particle for comparison. The tendency of the equilibrium position versus Reynolds number is different for a circular cylinder (2D) and a sphere (3D). The main features are summarized as follows: (1) The sphere moves towards the wall as Re is increased (i.e., the results () obtained by Schonberg and Hinch17 ). (2) Figures 9(a) and 9(b) show the present results of a circular cylinder with K = 0.11 (●) at Re = 1–1000. The equilibrium position Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-9 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 A=3.333, K =0.20 A=2.500, K =0.17 A=1.875, K =0.15 A=1.200, K =0.12 A=1.000, K =0.11 0.95 U p 0.9 0.85 0.8 0.75 0.7 0 500 1000 1500 2000 2500 2440 2450 t (a) 0.8 A=3.333 0.795 A=2.500 0.79 A=1.875 0.785 U p 0.78 0.775 0.77 0.765 0.76 A=1.200 A=1.000 0.755 0.75 2400 2410 2420 2430 t (b) FIG. 5. (a) Translational velocity Up versus time t of an elliptical cylinder for different A and K at Re = 10. (b) The local plot at 2400 ≤ t ≤ 2450. moves towards the wall with increasing Re when Re ≤ Rec (∼3), and then the equilibrium position moves closer to the central axis with increasing Re when Re ≥ Rec . (3) Yang et al.37 simulated the motion of a circular cylinder with K = 0.1 (◦) at Re = 12.5–1000. The equilibrium position moves closer to the channel center with increasing Re, as shown in Fig. 9(b). (4) Feng et al.36 simulated the motion of a circular cylinder with K = 0.25 () at Re = 40–200. The equilibrium position moves Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-10 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 0.8 0.795 6.7e−3 0.79 0.785 Up,avg 0.78 4.4e−3 0.775 2.9e−3 0.77 9e−4 0.765 0.76 U =1e−4 p,osc 0.755 0.75 0.5 1 1.5 2 2.5 3 3.5 4 A FIG. 6. Average translational velocity Up,avg and its amplitude of oscillation Up,osc versus the aspect ratio A at Re = 10 when it fluctuates about the averaged equilibrium position. Amplitude of oscillation is marked as the error bar. towards the wall with increasing Re, as shown in Fig. 9(b). These results indicate that the relation of the equilibrium position and the Reynolds number may significantly depend on the size ratio K. We also consider the motion of an elliptical cylinder at a higher Re; Figure 10 shows the temporal development of lateral migration of the cylinder. The equilibrium position becomes closer to the central axis of the channel as Re is increased, which is similar to the case for the circular cylinder.38 We further examine the effects of the presence of walls. In our study, we do observe that the center of the elliptical cylinder undergoing the Poiseuille flow oscillates about its mean equilibrium position. The amplitude of oscillation Yosc versus Re and versus K are presented in Fig. 11. It is shown that Yosc becomes smaller with decreasing Re or K; this long-term dynamic is consistent with the results of Chwang12 for an ellipsoid. Then, we examine the effect of the size ratio K and the 0.32 0.6 A=3.333 A=2.5 A=1.875 0.5 0.3 0.28 A=1.2 0.4 0.26 ωs /π ω /π A=1 0.3 0.24 0.22 0.2 0.2 0.1 0.18 0 2490 0.16 2492 2494 2496 t (a) 2498 2500 1 1.5 2 2.5 3 3.5 A (b) FIG. 7. (a) Angular velocity ω/π versus time t between 2490 < t < 2500; (b) averaged angular velocity ωs /π versus time t of an elliptical cylinders for different aspect ratios A at Re = 10. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-11 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) Our ωmax 0.9 Jeffery’s ω max 0.8 Our ω 0.7 Jeffery’s ωmin ω max /π , ω min /π min [θ/π]=0.5167 0.6 0.5131 0.5092 0.4918 0.5 0.4 0.3 0.2 [θ/π]=0.9982 0.9961 0.9973 0.1 0.9979 0 −0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 K FIG. 8. Maximum angular velocity ωmax /π and minimum angular velocity ωmin /π for an elliptical cylinder of A = 3 at Re = 10 for different K = 0.2, 0.4, 0.5, 0.6. Jeffery’s solutions are also plotted for comparisons. The notation [θ /π ] denotes the decimal part of θ /π calculated in the present method. particle Reynolds number Rep on the rotation of an elliptical cylinder for (a) K = 0.4, A = 3 and (b) K = 0.76, A = 2. It is found that the oscillatory orientation does occur at a sufficiently high Rep , in particular when K is large. Figure 12(a) shows that the elliptical cylinder with K = 0.4 is always rotary at Rep = 4, 16, 40, and becomes oscillatory in orientation at Rep = 80. Figure 12(b) shows that the elliptical cylinder with the larger K = 0.76 exhibits an oscillatory orientation at Rep = 30, 152, 380, but becomes stationary at the largest Rep = 418. Figure 13 shows the maximum and minimum normalized angles of inclination θ max /π , θ min /π versus Re for the elliptical cylinders with K = 0.4, A = 3 and K = 0.76, A = 2, respectively. We have the following observations. (1) 0.28 A=3.333, K=0.2 A=1.875, K=0.15 A=1, K=0.11 0.275 A=3.333, K=0.2 A=1.875, K=0.15 A=1, K=0.11 0.4 Yang 0.35 0.27 (2D), K=0.1 Feng (2D), K=0.25 Yang (3D), K=0.1 Schonberg (3D) Yeq Yeq 0.3 0.265 0.25 0.26 0.2 0.255 0.25 0.15 0 5 10 Re (a) 15 20 0.1 0 50 100 150 200 Re (b) FIG. 9. (a) Equilibrium position Yeq versus Reynolds number Re for the elliptical cylinder with A = 3.333, K = 0.2 (), and A = 1.875, K = 0.15 (); and the circular cylinder with K = 0.11 (●). (b) The present results compared to a sphere by Schonberg and Hinch17 (), a circular cylinder with K = 0.1 (◦) and a sphere with K = 0.1 () by Yang et al.,32, 37 and a lager circular cylinder with K = 0.25 () by Feng et al.36 Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-12 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 0.42 Re=1000 0.4 0.38 0.36 Re=200 Y p 0.34 0.32 0.3 Re=100 0.28 Re=40 0.26 0.24 Re=20 Re=10 0 500 1000 1500 2000 2500 t FIG. 10. Temporal development of lateral migration Yp of an elliptical cylinder with A = 1.875, K = 0.15 at different Re. The curves at t = 2500 from the bottom to the top correspond to Re = 10, 20, 40, 100, 200, 1000, respectively. In a range of lower Reynolds numbers (Re < 200 for K = 0.4), the elliptical cylinder is rotary all the time. (2) In a range of moderate Reynolds numbers (Re ≥ 200 for K = 0.4, Re < 550 for K = 0.76), the elliptical cylinder exhibits an oscillatory orientation dynamics; the maximum and minimum normalized angles of inclination θ max /π and θ min /π approach 0.9 and 0.1, respectively, as Re is increased. This behavior is independent of the size ratio K. (3) In a range of higher Reynolds 0.012 K=0.15, A=1.875 K=0.2, A=3.333 K=0.4, A=3 0.01 Y osc 0.008 0.006 0.004 0.002 0 0 20 40 60 80 100 Re FIG. 11. The amplitude of oscillation Yosc versus Re of an elliptical cylinder when it fluctuates about the averaged equilibrium position for (1) K = 0.15 and A = 1.875 (◦), (2) K = 0.2 and A = 3.333 (), and (3) K = 0.4 and A = 3 (). Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-13 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 0.5 Re=10, Re =4 p 0.4 Re=40, Re =16 p Re=100, Re =40 0.3 p Re=200, Re =80 p 0.2 ω /π 0.1 0 −0.1 −0.2 −0.3 −0.4 −0.5 150 200 250 300 350 t (a) 0.3 Re=40, Re =30 p 0.25 Re=200, Rep=152 0.2 Re=500, Re =380 0.15 Re=550, Rep=418 p ω /π 0.1 0.05 0 −0.05 −0.1 −0.15 −0.2 0 50 100 150 200 250 300 t (b) FIG. 12. Angular velocity ω/π versus time t of an elliptical cylinder with (a) small size ratio K = 0.4 and aspect ratio A = 3, (b) large size ratio K = 0.76 and aspect ratio A = 2 at different Rep . Note that for the smaller K = 0.4, the elliptical cylinder keeps rotating at Rep = 4–40, but oscillates in orientation at Rep = 80. For the larger K = 0.76, the elliptical cylinder oscillates in orientation at Rep = 30–380, but becomes stationary in orientation with θ = 0 at Rep = 418. numbers (Re ≥ 550 for K = 0.76), the elliptical cylinder becomes stationary, and the angle θ is approaching zero. In order to examine the correlations between the center-of-mass trajectory and the orientation dynamics of an elliptical cylinder, we present in Figs. 14(a) and 14(b) the height of the elliptical cylinder corresponding to Figs. 12(a) and 12(b). Figure 14(a) shows that the center-of-mass for Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-14 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 θ max /π , θ min /π K =0.4, A=3 K =0.76, A=2 0.1 0 0 200 400 600 800 1000 Re FIG. 13. The maximum and minimum normalized angles of inclination θ max /π , θ min /π versus Re for the elliptical cylinders with K = 0.4, A = 3 and K = 0.76, A = 2, respectively. K = 0.4 oscillates mildly about an averaged equilibrium position for Rep = 4–40, but it oscillates about the channel center at the higher Rep = 80. Figure 14(b) shows that the elliptical cylinder with the larger K = 0.76 oscillates about the channel center for Rep = 30–380, but it moves to the channel center at the higher Rep = 418. It is of great interest to observe the following correlations between the center-of-mass trajectory and the orientation dynamics. (1) In the cases where the center-of-mass trajectory moves to the channel center, the elliptical cylinder is stationary in orientation with the angle of inclination θ = 0. (2) In the cases where the center-of-mass trajectory oscillates about the channel center, the elliptical cylinder also exhibits oscillatory orientation dynamics. (3) In the 0.8 Re=10, Re =4 Re=40, Re =30 0.7 p p Re=40, Re =16 Re=200, Re =152 p 0.7 p Re=100, Re =40 Re=500, Re =380 0.65 p p Re=200, Re =80 Re=550, Re =418 p p 0.6 Yp Y p 0.6 0.5 0.55 0.5 0.4 0.45 0.3 0.4 0.2 0 100 200 300 t (a) 400 500 0 50 100 150 200 250 300 t (b) FIG. 14. Lateral migration of an elliptical cylinder with (a) small size ratio K = 0.4 and aspect ratio A = 3, (b) large size ratio K = 0.76 and aspect ratio A = 2 at different Rep . Note that for the smaller K = 0.4, the center-of-mass is oscillating mildly about an equilibrium position for Rep = 4–40, but will eventually oscillate about the channel center at the higher Rep = 80. For the larger K = 0.76, the elliptical cylinder oscillates about the channel center for Rep = 30–380, and eventually moves to the channel center at the higher Rep = 418. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-15 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 0.8 0.7 1 p Y Y 0.6 0.5 0.5 0.4 0 0 0.5 1 1.5 2 2.5 3 3.5 4 0.3 X 0.2 (a) 0.1 0 0 100 200 300 400 500 600 700 800 900 1000 120 140 160 180 200 t 0.9 0.9 0.8 0.8 0.7 0.7 0.6 0.6 p 1 0.5 Y Y p (b) 1 0.5 0.4 0.4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 100 200 300 400 500 600 700 800 900 1000 0 0 20 40 60 80 100 t t (c) (d) FIG. 15. (a) The initial positions of ND = 16 (φ T = 3.77%) cylinders with A = 1.875 and K = 0.15, the initial setup is sx = 0.25, sy = 0.25, and random θ 0 . Temporal development of lateral migration Yp of ND = 16 cylinders at (b) Re = 10, (c) Re = 100, and (d) Re = 1000. cases where the center-of-mass trajectory oscillates mildly about the Segre–Silberberg equilibrium position, the elliptical cylinder is rotary all the time. C. The cases of a few elliptical cylinders (ND = 16, φ T = 3.77%) In this section, we consider the motion of 16 (the corresponding φ T = 3.77%) neutrally buoyant elliptical cylinders with A = 1.875 and K = 0.15 in a pressure-driven plane Poiseuille flow at Re = 10, 100, 1000. The domain of computation is D = (4 × 1). The initial setups are similar to those in Fig. 15(a): the initial distance between two cylinder centers is sx = 0.25 in the x-direction, and sy = 0.25 in y-direction, and the initial angles of inclination of the particles θ 0 are chosen randomly. The other parameters are the same as in Sec. IV B. 1. The effect of the Reynolds number (Re) Figures 15(b)–15(d) show the temporal developments of lateral migrations at Re = 10, 100, and 1000. At the lower Re = 10, the collisions between cylinders repel them off each other (Fig. 15(b)). The cylinders exhibit a bifurcation behavior by scattering into eight groups, with each group fluctuating about a time-averaged position Yavg . At the higher Re = 100, the cylinders tend to cluster near the equilibrium positions (Fig. 15(c)). At the even higher Re = 1000, the cylinders move to the equilibrium position on each side of the central axis (Fig. 15(d)). Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-16 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 0.8 0.7 1 p Y y 0.6 0.5 0.5 0.4 0 0 0.5 1 1.5 2 2.5 3 3.5 4 x 0.3 (a) 0.2 0.1 0 0 500 1000 1500 2000 2500 t (b) FIG. 16. (a) The initial positions of ND = 16 (φ T = 3.77%) cylinders with A = 1.875 and K = 0.15, the initial setup is sx = 0.5, sy = 0.2, and θ 0 = π /4. (b) Temporal development of lateral migration Yp of ND = 16 cylinders at Re = 10. 2. The effect of the initial distributions of cylinders We also consider the effect of the initial positions for 16 elliptical cylinders at Re = 10. Figure 16(a) shows the initial setup: the initial distance between two cylinder centers is sx = 0.5 in the x-direction, and sy = 0.2 in the y-direction, and initial angles of inclination θ 0 = π /4. Figure 16(b) shows the temporal development of lateral migration of 16 cylinders at Re = 10. The particle-particle collisions occur much later if the initial positions of the cylinders are farther away from each other (compared to Fig. 15(b), where sx = 0.25, sy = 0.25). Eventually, the cylinders are divided into eight groups, and fluctuate about a time-averaged position. The results show that the bifurcation behavior is independent of the initial positions of the cylinders. Then, we consider the effects of the initial orientations for 16 elliptical cylinders at Re = 10 and 1000. The initial orientations are either chosen randomly, or fixed at θ 0 = 0, π /4, or π /2. For the cases at Re = 10, the bifurcation in the averaged equilibrium positions remains almost the same for all the initial orientations. For the cases at Re = 1000, all the cases have the same equilibrium position at about req = 0.13. These results show that the bifurcation behaviors in the time-averaged equilibrium positions are independent of the initial positions and orientations of the elliptical cylinders. D. The cases for many cylinders (ND = 72, φ T = 16.9%) In this section, we consider the motion of 72 neutrally buoyant cylinders in a pressure-driven Poiseuille flow at Re = 1000; here the total solid area fraction φ T is increased to 16.9%. The initial distance between two cylinder centers is sx = 0.167 in the x-direction, sy = 0.167 in the y-direction with θ 0 = π /4 for the larger K = 0.2 (A = 3.333), and θ 0 randomly chosen for the smaller K = 0.15 (A = 1.875) and 0.11 (A = 1). The other parameters are the same as in Sec. IV B. 1. The effect of the aspect ratio (A) In the first three cases, there are ND = 72 (φ T = 16.9%) cylinders with aspect ratios of A = 3.333, 1.875, 1 and the corresponding K = 0.2, 0.15, 0.11, respectively. Figures 17(a)–17(c) and 18(a)–18(c), and 19(a)–19(c) show the cylinder positions at t = 1000, the distributions of the translational velocity of the fluid (u) and of the cylinders (Up ), and the time-averaged solid area distribution φ during t = 900 and 1000 for 72 cylinders. The elliptical cylinders with the higher A = 3.333 have faster Up ’s among the three cases, being more closely concentrated towards the central axis. The cylinders with the moderate A = 1.875 have slower Up ’s, and a relatively lower distribution φ can be observed in the middle channel. The cylinders with the smallest A = 1 have the slowest Up ’s, and the cylinders are more widely spread across the channel. The cylinders and flow velocity profiles are more blunted as A is increased, yet there is no velocity blunting near the wall due to the insignificant rheological effect there. We also observe a lower distribution φ in the middle channel; this situation is similar to the experimental result obtained for spheres with a small Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-17 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 0.9 0.8 0.8 0.7 0.7 0.6 0.6 y y (a) 1 0.5 0.5 0.4 0.4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 0 1 0 0.1 0.2 0.3 0.4 0.5 Up, u φ (b) (c) 0.6 0.7 0.8 0.9 1 FIG. 17. The behaviors of 72 cylinders (φ T = 16.9%) with A = 3.333, K = 0.2 at Re = 1000: (a) The cylinder positions at t = 1000; (b) the distribution of the translational velocities of cylinders Up (●), the averaged flow velocity profile u (solid line) and that of the Poiseuille flow (without cylinders) (dashed line); (c) the time-averaged solid area distribution φ during t = 900 and 1000. 1 0.9 0.9 0.8 0.8 0.7 0.7 0.6 0.6 0.5 y y (a) 1 0.5 0.4 0.4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 0.1 0.2 0.3 0.4 0.5 Up, u (b) 0.6 0.7 0.8 0.9 1 0 0 0.1 0.2 0.3 0.4 0.5 φ 0.6 0.7 0.8 0.9 1 (c) FIG. 18. The behaviors of 72 cylinders (φ T = 16.9%) with A = 1.875, K = 0.15 at Re = 1000: (a) The cylinder positions at t = 1000; (b) the distribution of the translational velocities of cylinders Up (●), the averaged flow velocity profile u (solid line) and that of the Poiseuille flow (without cylinders) (dashed line); (c) the time-averaged solid area distribution φ during t = 900 and 1000. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-18 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 0.9 0.8 0.8 0.7 0.7 0.6 0.6 0.5 0.5 y y (a) 1 0.4 0.4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 Up, u (b) 0 0 0.1 0.2 0.3 0.4 0.5 φ 0.6 0.7 0.8 0.9 1 (c) FIG. 19. The behaviors of 72 cylinders (φ T = 16.9%) with A = 1, K = 0.11 at Re = 1000: (a) The cylinder positions at t = 1000; (b) the distribution of the translational velocities of cylinders Up (●), the averaged flow velocity profile u (solid line) and that of the Poiseuille flow (without cylinders) (dashed line); (c) the time-averaged solid area distribution φ during t = 900 and 1000. solid volume fraction by Han and Kim.24 The cylinders with a lower A (1.875 and 1) tend to cluster about two peak positions. In contrast to the elliptical cylinders (A = 1.875), the circular cylinders interact against this converging tendency to scatter the cylinders more widely across the channel. For each cylinder, we consider its time-averaged angular velocity ωs /π during t = 900 and 1000. Figure 20 shows the distribution of ωs /π for the 72 cylinders. At these aspect ratios (A = 3.333, 1.875, 1), the cylinders near the walls have higher ωs /π , while the ones near the channel center have almost zero ωs /π . In other words, the cylinders are not rotating except those at the outer regions (near the walls), since the cylinders closer to the central axis of the channel are constrained by the neighboring cylinders. This constraint of rotation is more significant for the cylinders with a higher aspect ratio, since the cylinders are more concentrated near the channel center. 2. The effect of the Reynolds number (Re) We consider the motion of ND = 72 (φ T = 16.9%) cylinders with A = 1.875 and K = 0.15 in a pressure-driven Poiseuille flow at Re = 500, 1000, and 2000, respectively. The domain of computation is D = (4 × 1), and the pressure gradient is 8. The fluid and particles are at rest initially. The initial setup is sx = 0.167, and sy = 0.167, with θ 0 chosen randomly. The mesh size is h = 1/256, and the time step is t = 0.01. In order to see the scaling relationships with respect to Re, we normalize the translational velocity by Reα . Figure 21 shows good overlaps of u/Reα and Up /Reα of 72 cylinders during t = 900 and 1000 for the different Reynolds numbers, with α = 1.068. The cylinders are more densely concentrated around the central axis of the channel as Re is increased. Figures 22(a)–22(c) show the time-averaged solid area distribution φ during t = 900 and 1000 of the 72 cylinders for the different Reynolds numbers. It is observed that there are no longer clearly defined averaged equilibrium positions. Instead, a particle-free layer exists near each wall. We define the thickness yf of the layer to be the distance between the wall and the clustering of cylinders (or the thickness Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-19 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 0.9 0.8 0.7 y 0.6 0.5 0.4 0.3 0.2 0.1 0 0 0.5 1 | ωs/π | 1.5 2 2.5 FIG. 20. The distribution of the time-averaged angular velocities ωs /π during t = 900 and 1000 for the 72 cylinders (φ T = 16.9%) with A = 3.333 and K = 0.2 (●), A = 1.875 and K = 0.15 (◦), A = 1 and K = 0.11 (×). of the time-averaged solid area distribution φ = 0 region next to the wall). As Re is increased, yf also increases, while the central axis of the channel has a relatively larger local minimum in φ. The cylinders at a higher Re are distributed closer to the central axis, while at low Re, the more frequent particle-particle interactions cause the cylinders to scatter more widely across the channel. It is noted 1 0.9 0.8 0.7 y 0.6 0.5 0.4 0.3 0.2 0.1 0 0 1 2 3 Up/Reα , u/Reα or u/Re 4 5 −4 x 10 FIG. 21. The normalized flow velocity profile u/Reα (solid line) and the normalized distributions of the translational velocities Up /Reα with α = 1.068 of 72 cylinders (φ T = 16.9%, A = 1.875, K = 0.15) at Re = 500 (●), 1000 (), 2000 () during t = 900 and 1000. The normalized Poiseuille flow velocity (without cylinders) u/Re is denoted by the dashed line for comparison. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-20 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) TABLE I. The number of equilibrium positions (if it is 2) or the averaged equilibrium positions (if it is greater than 2) and the thickness of the particle-free layers yf . A NDa (or φ T b ) 36 54 (8.48) (12.72) Re 4 (0.94) 8 (1.88) 16 (3.77) 10 4 4 8 8 100 2 2 4 500 2 2 2 1000 2 2 2–3 10 4 4 8 100 2 2 4 500 2 2 2 1000 2 2 2 10 100 500 4 2 2 4 2 2 8 4 2 1000 2 2 2 3.333 1.875 1 72 (16.96) 90 (21.21) 108 (25.45) No [0.0935] No [0.2336] No [0.2991] 8 Noc [0.0093]d No [0.0748] No [0.1963] No [0.2336] 8 No [0.0093] No [0.0561] No [0.1495] No [0.2150] 8 No [0.0654] No [0.1589] No [0.2430] 8 6–8 No [0.1121] No [0.1589] No [0.0374] No [0.1121] No [0.1776] 9 6–8 No [0.0564] No [0.1121] No [0.0187] No [0.0748] No [0.1215] 9 8–9 No [0.0374] No [0.0841] No [0.0093] No [0.0374] No [0.1028] No [0.1963] No [0] No [0.0093] No [0.0561] No [0.0841] 9 9 No [0.0187] No [0.0374] No [0.0093] No [0.0280] No [0.0748] No [0.1682] No [0] No [0] No [0.0280] No [0.0654] 9 9 No [0.0093] No [0.0187] a ND is the number of cylinders. is the total solid area fraction (%). c “No” means no averaged position identified. d [y ] represents the thickness of the particle-free layer. f T 1 1 0.9 0.9 0.9 0.8 0.8 0.8 0.7 0.7 0.7 0.6 0.6 0.6 0.5 0.5 0.5 y 1 y y bφ 0.4 0.4 0.4 0.3 0.3 0.3 0.2 0.2 0.2 0.1 0.1 0.1 0 0 0.1 0.2 φ (a) 0.3 0.4 0.5 0 0 0.1 0.2 φ 0.3 (b) 0.4 0.5 0 0 0.1 0.2 φ 0.3 0.4 0.5 (c) FIG. 22. The time-averaged solid area distribution φ for 72 cylinders (φ T = 16.9%) with A = 1.875, K = 0.15 at Re = (a) 500, (b) 1000, (c) 2000 during t = 900 and 1000. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-21 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) TABLE II. The relations between the thickness of the particle-free layer and the total solid area fraction of the cylinders, where 8.48% < φ T < 25.45%. 100 Re 500 1000 0.0002φ T 2 − 0.0100φ T + 0.1364 0.0001φ T 2 − 0.0065φ T + 0.1439 0.0003φ T − 0.0173φ T + 0.2335 0.0002φ T 2 − 0.0150φ T + 0.2691 0.0001φ T 2 − 0.0122φ T + 0.3346 0.0003φ T − 0.0204φ T + 0.3084 0.0004φ T 2 − 0.0223φ T + 0.3888 0.0003φ T 2 − 0.0147φ T + 0.4984 A 1 1.875 3.333 2 2 that the transition flow occurs when Re > 2300 for the channel flow in the absence of cylinders,39, 40 but the transition to turbulence could occur at lower Re in the presence of cylinders.41 However, our results are mainly for the cases at Re = 500, 1000, and only one case at Re = 2000. E. The effect of the total solid area fraction (φ T = 0.94%–25.45%, ND = 4–108) We consider a wide range in the number of elliptical cylinders with (1) A = 3.333 and K = 0.2, (2) A = 1.875 and K = 0.15, and (3) A = 1 and K = 0.11 in a pressure-driven Poiseuille flow. The numbers of cylinders are ND = 4, 8, 16, 36, 54, 72, 90, and 108, which correspond to the total solid area fractions φ T = 0.94, 1.88, 3.77, 8.48, 12.72, 16.96, 21.21, and 25.45 (%), respectively. The Reynolds numbers include Re = 10, 100, 500, and 1000. The initial distance between two cylinder centers in the x-direction and y-direction are sx = sy = 0.25 for ND = 4–36, and sx = sy = 0.167 for ND = 54–108. The initial angles of inclination are θ 0 = π /4 for the larger K = 0.2, and θ 0 is random for the smaller K = 0.15 and 0.11. The other parameters are the same as in Sec. IV B. Table I lists the number of time-averaged equilibrium positions of the cylinders for different aspect ratios A and the dimensionless thickness of the particle-free layers yf at various Reynolds numbers Re. The equilibrium positions can be clearly identified when ND is low. As ND is increased, 0.35 0.3 0.25 y f 0.2 0.15 0.1 0.05 0 8 10 12 14 16 18 φT (%) 20 22 24 26 FIG. 23. The thickness of the particle-free layer yf versus the total solid area fraction φ T of the cylinders with A = 3.333 and K = 0.2 (●), A = 1.875 and K = 0.15 (◦), A = 1 and K = 0.11 () at Re = 100 (dotted line), 500 (dashed line), 1000 (solid line). Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-22 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) 1 1 0.9 0.9 0.8 0.8 0.7 0.7 φT=0.12 φ =0.16 T φ =0.25 T 0.6 ND 0.5 y y 0.6 0.5 0.4 0.4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 0.2 0.4 0.6 0.8 1 0 0 0.2 0.4 p φ (a) (b) U or u 0.6 0.8 1 FIG. 24. (a) The time-averaged distribution of the translational velocities of cylinder Up for ND = 54 (●), 72 (), 108 () circular cylinders with K = 0.11 (φ T = 0.12, 0.16, 0.25, respectively), and averaged flow velocity profile u (solid line) during t = 100 and 200 at Re = 10 (Rep = 1.1). The flow velocity profiles without particles are denoted by dashed line. (b) The time-averaged solid area distribution φ. the rheological effect is also more significant, and the equilibrium positions can no longer be defined; instead, a particle-free layer is found near each wall of the channel. Figure 23 shows the dimensionless thickness of the particle-free layers yf versus the aspect ratio A (= 3.333, 1.875, 1) at three different Re (= 100, 500, 1000). As φ T is increased, the particle-particle interactions are intensified, causing deviation of the cylinders from the equilibrium positions and thus a decrease in yf . It is also found that yf increases as Re or A is increased, because the particle-free layers are easier to produce at higher Re or for cylinders with a larger A. At a lower Re (= 10, 100), the cylinders fluctuate about several averaged equilibrium positions, and the particle-free layer cannot be formed. The relations between yf and φ T of the cylinders for A = 3.333, 1.875, 1 at Re = 100, 500, 1000 in the range of 8.48 < φ T < 25.45 (%) are shown in Table II. Basically, these relations are linear, but they are modified by a small quadratic term, which derives the linear relationships only at higher total solid area fraction φ T ’s. The decreasing rate of the linear term increases as Re is increased. Figures 24(a) and 24(b) show the translational velocity profiles (K = 0.11) at Re = 10 (Rep = 1.1) and the corresponding averaged flow velocity profiles for ND = 54, 72, 108 (φ T = 12.72%, 16.96%, 25.45%), respectively. The blunting of the velocity profile uaxial /u = 1.50 (uaxial and u are the space-averaged fluid velocities in the channel center and in the domain of computation, respectively) for φ T = 16.96%, which is close to uaxial /u = 1.46 for φ T = 15%, obtained by Nott and Brady.23 As φ T is increased, the Up and u profiles deviate more from the Poiseuille flow profile (without cylinders), especially at places near the channel center. Basically, the distribution of φ has a major maximum near each wall and a minor maximum in the channel center. This behavior is more pronounced as φ T is increased. V. CONCLUDING REMARKS This study provides a detailed investigation of the motion of a single and multiple neutrally buoyant elliptical cylinders in plane Poiseuille flow. As a validation, we consider a single elliptical cylinder in Couette flow, and obtained a critical particle Reynolds number Rep,c = 29, which is in good agreement with Ding and Aidun’s solution.7 We summarize the results for the motion of a single elliptical cylinder in two parts: (a) the smaller size ratio range K ≤ 0.2, and (b) the larger size ratio range K ≥ 0.4. (a) For the smaller size ratio range K ≤ 0.2, we consider the cases with K = 0.2, 0.17, 0.15, 0.12, 0.11 and corresponding aspect ratios A = 3.333, 2.5, 1.875, 1.2, 1 in the Poiseuille flow at Re = 10. It was found that the cylinder with a higher A moves closer to the central line, and has a higher translational velocity Up but a lower average angular velocity ω. By Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-23 (b) Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) least-squares fitting, we obtain the equilibrium position req and the time-averaged angular velocity ωs versus A as req = 0.4801 − 0.002(A − 1) − 0.0025(A − 1)2 and ωs /π = 0.3051 − 0.0355(A − 1) − 0.033(A − 1)2 , respectively. We also investigated the effect of Re (1–1000) on a single elliptical cylinder with A = 1.875 and K = 0.15, and found that there is a critical Reynolds number Rec ∼ 3, below which req shifts towards the wall with increasing Re, and above which the trend is the opposite. This trend and Rec are identical with a circular cylinder with the same size ratio. The center-of-mass of an elliptical cylinder (A = 1.875, 3.333) can oscillate about its averaged equilibrium position, and the amplitude of oscillation becomes larger with increasing Re or K. For the larger size ratio range K ≥ 0.4, we consider the cases with K = 0.4, 0.76 and corresponding A = 3, 2 in the range of Re = 10–550 (Rep = 4–418). For K = 0.4, the cylinder always is rotary at Re = 10, 40, 100 (Rep = 4, 16, 40), and becomes oscillatory in the angle of inclination in θ at Re = 200 (Rep = 80). For K = 0.76, the cylinder exhibits an oscillatory behavior in inclination at Re = 40, 200, 500 (Rep = 30, 152, 380), and becomes stationary in θ = 0 at the largest Re = 550 (Rep = 418). It is found that the center-of-mass trajectories and the orientation dynamics have the following correlations. (1) In the cases where the centerof-mass trajectory eventually moves to the channel center, the elliptical cylinder becomes stationary in orientation with the angle of inclination θ = 0. (2) In the cases where the center-of-mass trajectory oscillates about the channel center, the elliptical cylinder exhibits an oscillatory orientation dynamics. (3) In the cases where the center-of-mass trajectory is eventually oscillating mildly about the Segre–Silberberg equilibrium position, the elliptical cylinder is rotary all the time. We also summarize the results for the motion of multiple elliptical cylinders in two parts: (a) a few cylinders, ND = 16 (the corresponding total solid area fraction φ T = 3.77%) and (b) a larger number, ND = 36–108 (φ T = 8.48%–25.45%). (a) (b) For a smaller ND = 16 (φ T = 3.77%), we consider the cylinders with A = 1.875 and K = 0.15 at Re = 10, 100, 1000. It is shown that at the small Re = 10, the cylinders scatter into four groups on each side, with each group fluctuating about an averaged equilibrium position, and this bifurcation behavior is shown to be independent of the initial positions and orientations of the cylinders. The particle-particle interactions are less dominant as Re is increased, and there are fewer averaged equilibrium positions (four positions on each side of the channel center at Re = 10; two at Re = 100; one at Re = 1000). For the larger ND = 36, 54, 72, 90, and 108 (φ T = 8.48, 12.72, 16.96, 21.21, and 25.45 (%), respectively) in the range of Re = 10–1000, we observed the rheological effect due to the motion of cylinders in fluid, which affects the migration of the cylinders dramatically. There are no longer clear equilibrium positions, and the particle-free layers near the walls are formed instead. The cylinders and flow velocity profiles are more blunted as φ T is increased, yet there is no velocity blunting near the walls due to the insignificant rheological effect there. The number of cylinders ND = 36 (φ T = 8.48%) is a critical case in which the Reynolds number has a great impact. At lower Re (<100), the cylinders are widely spread over the entire channel, while at higher Re (>100), there are particle-free layers next to the walls. Interesting remarks are also available for more circular cylinders (ND = 54, 72, 108 with φ T = 12.72%, 16.96%, 25.45%. At the low Re = 10, the distribution of φ has a major maximum near each wall and a minor maximum in the channel center. At the high Re = 1000, the maximum-φ positions shift away from the walls. If we consider a smaller φ T (12.72% or 16.96%), the channel center becomes the location of a local minimum of φ. However, at the higher φ T = 25.45%, the φ-distribution in the middle channel is a high plateau with thinner particle-free layers next to the walls. The results for A = 3.333, 1.875, 1 on 72 cylinders (φ T = 16.96%) at Re = 1000 showed that the cylinders with higher A are more densely concentrated around the channel center. The general trend is that the thickness of the particle-free layer yf increases as A (or K) or Re is increased. In addition, an elliptical cylinder has a higher angular velocity when it is close to the particle-free layer than to the channel center. Downloaded 01 May 2013 to 140.112.50.48. This article is copyrighted as indicated in the abstract. Reuse of AIP content is subject to the terms at: http://pof.aip.org/about/rights_and_permissions 103302-24 Chen, Pan, and Chang Phys. Fluids 24, 103302 (2012) ACKNOWLEDGMENTS The work was supported in part by the National Science Council (Taiwan) under Contract Nos. NSC97-2221-E-002-223-MY3, NSC99-2628-M-002-003, and NSC100-2221-E-002-152-MY3. T.-W. Pan acknowledges the support of the US NSF (Grant No. DMS-0914788). 1 H. Xu and C. K. Aidun, “Characteristics of fiber suspension flow in a rectangular channel,” Int. J. Multiphase Flow 31, 318 (2005). 2 V. Yue, R. Kowal, L. Neargarder, L. Bond, A. Muetterties, and R. Parsons, “Miniature field-flow fractionation system for analysis of blood cells,” Clin. Chem. 40, 1810 (1994). 3 X. Tong and K. D. Caldwell, “Separation and characterization of red blood cells with different membrane deformability using steric field flow fractionation,” J. Chromatogr. 674, 39 (1995). 4 G. B. 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