Open Submitted: 30 October 2007 Accepted: 23 July 2008 Published Online: 02 September 2008
Physics of Fluids 20, 093602 (2008); https://doi.org/10.1063/1.2973900
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  • M. M. Weislogel
  • Y. Chen
  • D. Bolleddula

A scaling of the two-dimensional Laplacian operator is demonstrated for certain solutions (at least) to Poisson’s equation. It succeeds by treating the operator as a single geometric scale entity. The belated and rather subtle method provides an efficient assessment of the geometrical dependence of the problem and is preferred when practicable to the hydraulic diameter or term-by-term scaling for slender fully developed laminar flows. The improved accuracy further reduces the reliance of problems on widely varying numerical data or cumbersome theoretical forms and improves the prospects of exact or approximate theoretical analysis. Simple example problems are briefly described that demonstrate the application and potential of the method.
Considering the Cartesian velocity field u=(u,v,w), the equation governing low-inertia, weakly time-dependent, and predominantly z-directional flows is a Poisson equation derived from the z-component momentum equation:
k=Δw=(2x2+2y2+2z2)w,(1)
subject to boundary conditions. As is often helpful, assuming acceptable scales for x, y, z and k can be identified for the problem, scale analysis may be performed on Eq. (1) to determine the velocity scale for w with which Eq. (1) can in turn be nondimensionalized. In situations where the “cross-flow coordinates” x and y can be parametrized and scaled in terms of z and t, it is proposed that such spatially and temporally dependent length scales xx¯s and yy¯s with zzs=L may be employed to compute a spatially and temporally dependent velocity scale ww¯s. Provided the flow is slender, (x¯s/L)21, treating Δ as a single scalable quantity such that ΔΔ¯s, “scale analysis” on Eq. (1) is performed to determine
ww¯s=kΔ¯sk1x¯s2+1y¯s2kx¯s21+T¯sxy2,(2)
where T¯sxy=x¯s/y¯s. The overbar for x¯s and y¯s denotes local, potentially z- and/or t-dependent x- and y-coordinate length scales such that, in general x¯s=x¯s(z,t), y¯s=y¯s(z,t), L=L(t), k=k(z,t), and thus w¯s=w¯s(z,t). The method introduces a notation Δ¯s for the local z- and t-dependent Laplacian operator scale which is treated as its own term—a minor twist on the more common and intuitive term-by-term scaling method.11. W. B. Krantz, Scaling Analysis in Modeling Transport and Reaction Processes (Wiley, Hoboken, NJ, 2007). The “Laplacian scale” Δ¯s obeys commutative laws (e.g., Δ¯sw¯s=w¯sΔ¯s)—it is not an operator but the scale of an operator. Using velocity scale (2) and spatially dependent length scales, Eq. (1) when nondimensionalized becomes
1=1(1+T¯sxy2)2w¯x¯2+T¯sxy2(1+T¯sxy2)2w¯y¯2,(3)
where x¯=x/x¯s, y¯=y/y¯s, and w¯=wΔ¯s/k=w(1+T¯sxy2)/kx¯s2. The result of Eq. (3) is forwarded as a modified two-dimensional (2D) Poisson equation that, despite having z- and t-dependent variables and coefficients, can lead to narrower bounds for numerical coefficients for the area-averaged velocity,
w¯=x¯sy¯sAw¯dx¯dy¯Fi,(4)
where A is the dimensional section area. We do not make any significant effort to examine (or prove) the generality of this claim. Instead we demonstrate the usefulness of the approach with several basic example problems where Δ¯s=const, Δ¯s=Δ¯s(z), and Δ¯s=Δ¯s(z,t).
A. Steady fully developed laminar flow in a rectangular duct: Δ¯s=const=Δs
A schematic of this historic flow is provided in Fig. 1 with coordinates and characteristic lengths identified. It is frequently desirable to quickly determine the average velocity of the flow through the duct. Applying the present scaling approach, noting that the length scales for the duct are simply constants, x¯s=a, y¯s=b, and z¯s=L, where (a/L)21, the local dimensional velocity scale from Eq. (2) may be written directly,
w¯s=kΔ¯s=Pzμ1(1a2+1b2)=Pzμx¯s2(1+T¯sxy2)=Pzμa2(1+a2/b2),(5)
where k=Pz/μ, with Pz the pressure gradient along z and μ the dynamic viscosity of the fluid. (Subscript notation for partial differentiation is only implied herein for z and t.) The negative sign in Eq. (5) assures w¯s>0 when Pz<0. As reviewed by Shah and London (Ref. 22. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978)., Chap. 7A), when the hydraulic diameter scaling is applied to this problem, xs=ysab/(a+b), and term-by-term similar scaling of Eq. (1) produces
w¯hyd=Pzμa2(1+a/b)2.(6)
The exact analytic solution for the average velocity,22. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978).
w=Pzμx¯s23[1192π5T¯sxyi=1,3,5,tanh(iπ/2T¯sxy)i5]Fiw¯sFihydw¯hyd,(7)
is normalized by both the Laplacian [Eq. (5)] and hydraulic diameter [Eq. (6)] velocity scales and plotted against duct aspect ratio a/b in Fig. 2. Both approaches capture the order of magnitude of the exact average velocity for all a and b. However, the Laplacian scaling delivers at most a significant fourfold reduction in the variance of Fi versus Fihyd.
The result of Eq. (5) is similar in form to that presented by Bejan [Ref. 33. A. Bejan, Convection Heat Transfer, 3rd ed. (Wiley, New York, 2004)., Eq. (3.33)] following integration of assumed parabolic velocity fields expressed in terms of the cross-flow coordinates. However, Eq. (5) is here determined directly and simply by Δ¯s and provides a quick, concise, and more geometrically representative approximation of w for use in subsequent analytical solutions that are consequently only weakly dependent on further cumbersome solution forms or numerical data. The difference between Eqs. (5) and (6) is subtle for this problem, but disparities can increase dramatically in favor of the Laplacian scaling method for problems of increased geometric complexity.44. Y. Chen, M. M. Weislogel, and C. Nardin, “Capillary-driven flows along rounded interior corners,” J. Fluid Mech. https://doi.org/10.1017/S0022112006001996 566, 235 (2006). Equality between w and w¯s is established in Eq. (7) by introducing the narrowly varying function Fi, also defined in Eq. (4); for the rectangular section, 0.281Fi(a/b)1/3. The fact that Fi1/3 with at worst a 15.6% shortfall opens up further possibilities for approximate analytical solutions.
Defined in this manner, the function Fi is inversely proportional to previously determined friction factors.2,5,62. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978).5. P. S. Ayyaswamy, I. Catton, and D. K. Edwards, “Capillary flow in triangular groves,” J. Appl. Mech. 41, 332 (1974).6. T. C. Ransohoff and C. J. Radke, “Laminar flow of a wetting liquid along corners of a predominately gas-occupied noncircular pore,” J. Colloid Interface Sci. https://doi.org/10.1016/0021-9797(88)90442-0 121, 392 (1988). For the rectangular section22. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978). also reviewed by White,77. F. M. White, Viscous Fluid Flow, 3rd ed. (McGraw-Hill, New York, 2006), p. 117, Fig. 3-13. it can be shown that the Poiseuille number is confined such that 14.2PofRe=8(1+a2/b2)/Fi(1+a/b)224, where f is the Fanning friction factor with hydraulic diameter Reynolds number Re=ρUDhyd/μ, where Dhyd=4As/P, with As and P as the total section area and wetted perimeter, respectively. Not only is Fi or its inverse four times more confined than Po but it is O(1). Last, using the Δ¯s scaling it can be shown that if a single viscous length rμ was computed, characterizing the average velocity for this flow, it would be rμ=(2Fi/Δ¯s)1/2(2/3)1/2ab/(a2+b2)1/2. For such laminar flows this “viscous length” is accurate, satisfying wPzrμ2/2μ, and is more akin to a section area divided by a section diagonal as opposed to a section area divided by a section perimeter (i.e., the hydraulic diameter approach). Note that Po may be converted to Fi using Fi=Dhyd2Δ¯s/2Po .
B. Constant rate laminar flow in a slender constant area rectangular duct of varying aspect ratio: Δ¯s=Δ¯s(z)
The accommodation of spatially varying scales can be demonstrated with the pedagogical problem sketched in Fig. 3. For this duct, w=const=wo and A=const=4ab. As sketched, for a linearly tapering duct in the y-z plane, the duct boundaries are defined by xw=±ab/(bmz) and yw=±(bmz), where m=(ba)/L.
One may want to quickly compute Pz or P(z) for this flow in instances where wo is known. Using the Eq. (7) definition wFiw¯s, Eq. (2) is employed again but now with z-dependent length scales. For example, when (a/L)21, substituting the z-dependent length scales x¯s=xw and y¯s=yw into Eq. (2) and noting T¯sxy=ab/(bmz)2, solving for Pz yields
Pz=μwoFi(bmzab)2(a2b2(bmz)4+1).(8)
However, Fi1/3 and is a weak function of z. Treating Fi=1/3 and applying the boundary condition P(L)=PL, Eq. (8) may be integrated to find
PsPLμwo[3a2b2+(a33ab2)(bmz)(bmz)4a2b2m(bmz)],(9)
which is more accessible than the exact solution
Pe=3μwo(bmza2b2){1192π5ab(bmz)2i=1,3,5,tanh[iπ(bmz)/2ab]i5}1dz,(10)
subject also to P(L)=PL, which must be integrated numerically. [Subscripts s and e denote “scale” and “exact” forms for pressure P(z).] Choosing PL=0, from Eq. (9) the upstream pressure is
Ps(0)=μwoL(a2+4ab+b2a2b2).(11)
Using this pressure to nondimensionalize Eqs. (9) and (10) yields the respective dimensionless pressure distributions
Ps(z)=[b(ba)z]4(a33ab2)[b(ba)z]3a2b2(ba)(a2+4ab+b2)[b(ba)z](12)
and
Pe(z)=3[b(ba)z]2(a2+4ab+b2){1192π5ab[b(ba)z]2i=1,3,5,tanh{iπ[b(ba)z]2/2ab}i5}1dz,(13)
where z=z/L. Lengths a and b are nondimensionalized by A1/2/2, such that in dimensionless form b=a1. The functions of Eqs. (12) and (13) are compared in Fig. 4(a) for a selection of values for a. The agreement is complete for a1 and a1 and worsens to at most 15% as a approaches 1. Any discrepancy at all is due to Fi being treated as a constant in Eq. (9). As will be presented in connection with Figs. 7 and 9, it can be shown that a simple correlation for Fi(a) is Fi(116sin2α)/3, where α for the rectangular section is defined as α=tan1(a/b)=tan1a2. Exploiting this relationship in Eq. (8) leads to
Pc(z)=Ps(z)(116sin2α),(14)
where subscript c denotes a “correlated” scale value. Pc(z) is also compared to Pe(z) in Fig. 4(b), where conditions a1, a=1, and a1 agree completely with intermediate discrepancies <5%.
The simple Δ¯s scale solutions (12) and (14) do well in capturing the z dependence of the flow with errors typically less than 15% and 5%, respectively. Exact theoretical or numerical solutions are preferable, but in many cases such solutions mask the largely simple geometric dependence of the flow typified by such examples, i.e., Eq. (5) versus Eq. (7) and Eq. (9) versus Eq. (10). The compact forms resulting from the Laplacian scale approach further encourages the notion that the method might be exploited to greater effect in theoretical analyses where, say, w or P become variables in subsequent derivations or models. A sample problem of this kind is highlighted below in three steps.
C. Laminar gravity-driven flow along a slender channel: Δ¯s=Δ¯s(z,t)
This contrived example flow illustrates how z- and t-dependent scales within the Laplacian scale Δ¯s assist in the formulation of governing evolution equations.
1. Rectangular channel section
A schematic with critical dimensions for this free surface flow with negligible surface tension and θ=π/2 contact angle is provided in Fig. 5. The driving hydrostatic pressure gradient is Pz=ρghz with ρ the density difference across the free surface and g the gravitation in the negative y direction, i.e., g=(0,g,0). It is desirable for this flow to determine the governing evolution equation using the Laplacian scaling method. From Fig. 5 x¯s=const=a, y¯s=hh(z,t), and zs=const=Lfcn(t). For a slender column (a/L)21. Employing Eq. (5) and the definition of Fi, Eq. (7) becomes
w=Fiw¯s=FiPzμx¯s2(1+T¯sxy2)=FiPzμa2[1+(a/h)2].(15)
Conservation of volume along the z axis for this flow requires
At=(Aw)z=(AFiw¯s)z.(16)
In this case, A=2ah and substitution of Eq. (15) into Eq. (16) yields the dimensional nonlinear governing equation,
ht=ρga2μ(Fihhz1+(a/h)2)z.(17)
This form is exact provided Fi from Eq. (7) is employed. However, as demonstrated in Fig. 2, since Fi1/3, a wieldy approximate solution form is obtained by absorbing Fi and ρga2/μ into the time scale should further theoretical analysis be pursued as will be momentarily.
It is noted that Eq. (17) is a dimensional evolution equation derived using local, weakly z- and t-dependent scales via Δ¯s through h=h(z,t). Because the local scales are unknown and variable, Eq. (17) must be normalized by global scales that are known and constant. For this simple flow the global scales are xa, hH, zL, and tL/ws, where ws follows from w¯s but incorporates the global scales in a global (note the absence of overbar) Laplacian scale Δs=1/a2+1/H2 such that
wsPzμΔsPzsμ1(1a2+1H2)ρgHa2μL(1+a2/H2),(18)
where PzsρgH/L. Nondimensionalizing Eq. (17) now by the global scales yields the dimensionless nonlinear evolution equation
ht=(Fi(1+λ2)1+λ2/h2hhz)z,(19)
where λa/H. This form of the equation is O(1) in all limits of the single parameter λ2 since Fi is approximately constant and O(1). Equation (19) reveals different evolutionary behavior in the primary limits. For narrow channel flow, λ2/h21 (Fi1/3),
ht=(Fihhz)z.(20)
For thin film flow, λ2/h21 (Fi1/3),
λ2ht=[Fi(1+λ2)h3hz]z.(21)
In essence, when λ2/h21 the flow geometry transitions from a narrow channel flow [Eq. (20)], to the full flow [Eq. (19)], and then to a thin film flow [Eq. (21)] as h0. This progression is qualitatively depicted by locations 1–3 in Fig. 5, respectively. The limiting equations (20) and (21) offer significantly improved opportunities to develop analytical solutions (exact, steady, similarity, etc.) to benchmark the governing equation (19), with the latter to be solved numerically in the majority. This result may be more appreciated for more geometrically complex flows as will be demonstrated.
2. Triangular channel section
This flow geometry is sketched in Fig. 6 for θ=π/2α and is addressed identically as the rectangular channel flow only, x¯s=htanα, y¯s=h, zs=L, and A=h2tanα. Again, taking (htanα/L)21 and substitution of the z-dependent scales into Eq. (15) for w and then into Eq. (16), the governing equation for 0απ/2 becomes
(h2)t=ρgsin2αμ(Fih4hz)z.(22)
An exact solution is not available for Fi for all α for this section. However, numerical results in various forms2,5–82. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978).5. P. S. Ayyaswamy, I. Catton, and D. K. Edwards, “Capillary flow in triangular groves,” J. Appl. Mech. 41, 332 (1974).6. T. C. Ransohoff and C. J. Radke, “Laminar flow of a wetting liquid along corners of a predominately gas-occupied noncircular pore,” J. Colloid Interface Sci. https://doi.org/10.1016/0021-9797(88)90442-0 121, 392 (1988).7. F. M. White, Viscous Fluid Flow, 3rd ed. (McGraw-Hill, New York, 2006), p. 117, Fig. 3-13.8. D. Bolleddula, “Capillary flow analysis and computation of dewetting and wetting resistances in angular geometries,” M.S.M.E. thesis, Portland State University, 2007. are (in Ref. 22. R. K. Shah and A. L. London, Laminar Flow Forced Convection in Ducts (Academic, London, 1978). see solutions for rhombi), the most recent of which are plotted in Fig. 7. It is found that for the triangular channel 0.1405Fi(α)1/6, or Ficonst1/6—approximately 50% that of the rectangular channel, which is also plotted in Fig. 7 in terms of α, where tanα=a/b. Nondimensionalizing Eq. (22) using the relevant global scales for this problem xHtanα, hH, zL, and tL/ws, where Δs=1/H2tan2α+1/1H2=1/H2sin2α, produces the governing evolution equation
(h2)t=(Fih4hz)z.(23)
3. Trapezoidal channel
In keeping with the schematic of Fig. 8 for this flow, x¯s=(a+htanα), y¯s=h, z¯s=L, and A=(2a+htanα)h. Using global scales xa+Htanα, hH, zL, and tL/ws and taking [(a+htanα)/L]21 produces the governing dimensionless equation
(A)t=[AFi(w¯sws)]z=[AFi(ΔsΔ¯s)hz]z,(24)
where it is observed that all interesting geometric dependence is contained within the ratio of global-to-local Laplacian scales. The expanded form of Eq. (24) is
[(2λ+htanα)h]t={(2λ+htanα)hFi(λ+htanαλ+tanα)2[1+(λ+tanα)2h2+(λ+htanα)2]h2hz}z,(25)
where again λa/H. By inspection of Eq. (25), rectangular channel form (19) is recovered when α0 (or htanα/λ1, tanα/λ1), and triangular channel form (23) is recovered when λ0 (htanα/λ1, tanα/λ1).
Fi(h;α,λ) for the trapezoidal section is computed numerically using Eqs. (3) and (4). Equation (3) is solved using MATLAB® and the PDE toolbox88. D. Bolleddula, “Capillary flow analysis and computation of dewetting and wetting resistances in angular geometries,” M.S.M.E. thesis, Portland State University, 2007. and an adaptive mesh of 50000 finite elements. The results are also plotted in Fig. 7 (dots) with the limiting values for the rectangular (α0) and triangular (λ0) channel sections noted. Thus, in approximation, Fi(λ=0)=1/6Fi1/3=Fi(α=0) for all values of α, λ, and h for the trapezoidal channel flow.
Furthermore, it can be shown for such Cartesian scaled geometries that
FiFn3AsectArect=Fn3AtrapArect=Fn6(2λ+htanα)(λ+htanα),(26)
where Asect is the local quadrant area of the section and Arect=x¯sy¯s is the scale quadrant area. The numerical values of Fi in Fig. 7 are converted using Fn from Eq. (26) and replotted in Fig. 9. “Worst case” limiting values for Fi are represented in Fig. 10, revealing that the weak h dependence is largely confined to h0.1. The collapse of the numerical data to Fn0.97 (±0.08 standard deviation for all values computed) favors the use of Eq. (26) and appears suitable for a family of duct sections possessing x- and y-axis symmetry such as simple even-sided convex polygons and ellipses sketched in Fig. 11. It is also suitable for free surface flows where the free surface is coincident with zero shear stress symmetry planes. Substituting Eq. (26) into Eq. (25), the full evolution equation for the trapezoidal channel section is
[(2λ+htanα)h]t{(2λ+htanα)Fn6(2λ+htanα)(λ+htanα)(λ+htanαλ+tanα)2[1+(λ+tanα)2h2+(λ+htanα)2]h3hz}z,(27)
where 0.825Fn(h;α,λ)1.125 and Fn1 might be a reasonable approximation. A concise assessment of the error incurred by taking Fn=1 is provided in Fig. 12 where exact numerical solutions to the steady solution of Eq. (27) are compared. The exact solutions employ a sixth order polynomial for Fi and thus Fn before solving Eq. (27) numerically. The agreement is excellent. For the worst case a=0.02° and λ=3.49×104, errors <3% are typical with maximum errors <7% near z=1 where the function h becomes vertical. For the other more typical values of α shown, the scaled Laplacian and exact numerical solutions are essentially coincident.
Equation (27) is quickly obtained using the present method and embodies the majority of the sought geometric dependence of the flow. It serves as an adequate “starter” form for subsequent analysis. Such equation formulations are particularly helpful for analysis for more intricate geometries where limiting behavior may not be perceived a priori. The example of capillary-driven flow along interior corners that are rounded44. Y. Chen, M. M. Weislogel, and C. Nardin, “Capillary-driven flows along rounded interior corners,” J. Fluid Mech. https://doi.org/10.1017/S0022112006001996 566, 235 (2006). provides a case in point (see Fig. 13). Such free surface flows can possess a variety of limiting behaviors for a single geometry and require fully numerical solutions. Nonetheless the Laplacian method quickly captures the correct form and order of terms in a governing evolution equation facilitating theoretical understanding as well as numerical setup, solution, and benchmark.
As briefly mentioned in Sec. I A, the Laplacian scaling method characterizes the geometric dependence of viscous diffusion with greater accuracy than the hydraulic diameter scaling. It does so by characterizing the effective viscous length with greater accuracy. If one exploits these benefits to compute Fanning friction factors f for such flows (Fig. 11) one might define a Laplacian diameter,
DΔ(FiΔ¯s)1/2=(FnAs3(T¯sxy+T¯sxy1))1/2,(28)
and a Laplacian Reynolds number, ReΔ=ρUDΔ/μ, to find that
2.67PoΔfReΔ23.(29)
This result implies that the Laplacian Poiseuille number, PoD3(±10%), is a weak O(1) function of the section geometry and may be treated approximately as a constant for laminar flows. As a consequence, f3/ReD for all applicable cross sections. This compares to 14.2PofRe24 for traditional laminar flows, where Re is scaled on Dhyd.
In summary, the Laplacian scaling method amounts to nothing more than treating the operator as its own geometric scale quantity, Δ¯s. It appears to be a quick and effective method for certain predominately 2D fields with possibilities for weak three-dimensional as well as temporal dependence. The subsequent process of nondimensionalization yields a modified 2D Poisson equation with z- and t-dependent variables and coefficients [Eq. (3)], which when solved for the dimensionless area-averaged velocity w¯Fi [Eq. (4)] possesses a weak dependence on numerical data—a dependence that is further reduced when Fn from Eq. (26) is employed. In such situations exact or approximate average quantities are readily determined as are the subsequent equations that depend on them.
This work is supported in part by the National Aeronautics and Space Administration through Grant No. NNC05AA29A and National Science Foundation Grant No. CTS-0521890. M.M.W. would like to thank A. Bejan for an introduction to scale analysis and G. Recktenwald for a push.
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