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Modeling the combined effect of surface roughness
and shear rate on slip flow of simple fluids
Department of Mechanical Engineering Michigan State University
A. Niavarani and N.V. Priezjev, “Modeling the combined effect of surface roughness and
shear rate of slip flow of simple fluids,” Phys. Rev. E 81, 011606 (2010).
Anoosheh Niavarani and Nikolai Priezjev
www.egr.msu.edu/~niavaran
November 2009
Introduction
 MD simulations have shown that at the
interface between simple1 and polymeric2
liquids and flat walls the slip length is a
function of shear rate.
h
Solid wall
U
x
z
us
u(z)
1 P. A. Thompson and S. M. Troian, Nature (1997)
2 N. V. Priezjev and S. M. Troian, Phys. Rev. Lett. (2004)
 Surface roughness reduces effective slip length.
 For flow of simple1 and polymeric2 liquids past
periodically corrugated surface there is an
excellent agreement between MD and continuum
results for the effective slip length (if ).
Constant local slip length from MD was used as
a boundary condition for continuum simulation.
1 N. V. Priezjev and S. M. Troian, J. Fluid Mech. (2006)
2 A. Niavarani and N. V. Priezjev, J. Chem. Phys. (2008)
dz
zdu )(
=γ
Navier slip law
L0
γ0Lus = γγ )(0Lus =
)(0 γL
dz
zdu )(
=γ
σλ 30≥
 The no-slip boundary condition works
well for macro- flows, however, in micro
and nanoflows molecular dynamics
simulations and experiments report the
existence of a boundary slip.
x
z
n
nu
Lxu t
ss
∂
∂
=
)(
)()( γ
Introduction
Question: How to model the combined effect of surface roughness and shear rate?
Solution 1: Perform full MD simulation of the flow past rough surface (very expensive
computationally!!!).
Solution 2: From MD simulation extract only slip length as a function of shear rate
for flat walls. And then, use as a local boundary condition for the flow over rough
surface in the Navier-Stokes equation. (Is it possible?)
In this study we compare Solution 1 and Solution 2
)(γsL
)(γsL
Fluid flow
Rough surface
Department of Mechanical Engineering Michigan State University
Details of molecular dynamics (MD) simulations
ij
i i i
i j i
V
my m y f
y≠
∂
+ Γ =− +
∂
∑ 
1
τ −
Γ =
BT=1.1 kε
( ) ( ) 2 ( )i i Bf t f t mk T t tδ′ ′= Γ −
if
12 6
LJ
r r
V (r) 4ε
σ σ
− −
    
= −    
     
2 1/2
( )mτ σ ε=
σ LJ molecular length scale
ε LJ energy scale
LJ time scale
Lennard-Jones potential:
Department of Mechanical Engineering Michigan State University
Langevin Thermostat
Friction coefficient
Equation of motion:
Gaussian random force
ρ w = 3.1 σ −3
ρ w = 0.67 σ −3
ρ = 0.81 σ −3
σλ 42≈=zL 27.0
2
==
λ
πa
ka
3
81.0 −
= σρFluid density
( ) sin(2 / )z ax xπ λ=
Shear flow over a rough surface
The effective slip length Leff and intrinsic slip length L0
Leff is the effective slip length, which characterizes
the flow over macroscopically rough surface
Department of Mechanical Engineering Michigan State University
z
R(x) : local radius of curvature
Ls
us
R(x)
u(z)
x
Local velocity profile
Ls : local slip length
L0 : intrinsic slip length extracted
from MD simulation
n
zu
Lxu ss
∂
∂
=
)(
)(
)(
111
0 xRLLs
−=
Equations of motion (penalty formulation):
Boundary condition:
Bilinear quadrilateral elements
shape function
Details of continuum simulations (Finite Element Method)
Department of Mechanical Engineering Michigan State University
R(x): local radius of curvature
(+) concave, (–) convex
L0: intrinsic slip length as a function of
Galerkin formulation:
)](/))[((0 xRuunLu sss +∇⋅=

γ
)(/).( xRuun ss +∇=

γShear rate:
γ
us
Department of Mechanical Engineering Michigan State University
dz
zdu )(
=γγγ )(0Lus =
 Slip length is a highly nonlinear function of
shear rate
 Velocity profiles are linear across the channel
 Shear rate is extracted from a linear fit to
velocity profiles
 No-slip at the upper wall (commensurable
wall/fluid densities)
L0
h
U
us
u(z)
L0/σ
MD simulations: Velocity profiles and slip length for flat walls
Velocity profiles Slip length vs. shear rate
Ls
us
R(x)
u (z)
: polynomial fit






+
∂
∂
=
)(
)(0
xR
u
n
u
Lu ss
s γ






+
∂
∂
=
)(xR
u
n
u ss
γ
constant slip length at low shear rate
rate-dependent slip at high shear rates
)(0 γL
λ
πaka 2=
 Blue line is a polynomial fit used in Navier-Stokes solution
9th order polynomial fit
 Surface roughness reduces the effective slip length and its
shear rate dependence
monotonic increase
 Excellent agreement between MD and NS at low shear
rates but continuum results slightly overestimate MD
at high shear rates
 Constant slip length at low shear rate, highly nonlinear
function of shear rate at high shear rates
slight discrepancy
excellent agreement
detailed analysis
Slip length vs. shear rate
Effective slip length as a function of shear rate for a rough surface
Detailed analysis of the flow near the curved boundary
Local pressure Local temperature
 Pressure: average normal force on wall atoms from
fluids monomers within the cutoff radius
 For pressure is similar to equilibrium case
and is mostly affected by the wall shape
 For pressure increase when and
τσ /0.1≤U
τσ /0.1>U 12.0/ <λx
54.0/ >λx 5.0/ =λx 3
/36.2 σε== flatPP
 Average temperature is calculated in the
first fluid layer
 At small upper wall speeds, temperature
is equal to equilibrium temperature
 With increasing upper wall speed the
temperature also increases and eventually
becomes non-uniformly distributed
First fluid layer
Local velocity profiles in four region (I-IV) along the stationary lower wall
τσ /0.1=U
Small upper wall speed
17Re ≈
Local tangential velocity
 At small U, excellent agreement between NS
and MD especially inside the valley (IV)
 The slip velocity above the peak (II) is larger
than other regions
 Even at low Re, the inertia term in the NS
equation breaks the symmetry of the flow with
respect to the peak => ut (I) > ut (III)
 In regions I and III, negative and positive
normal velocities are due to high pressure
and low pressure regions
 The oscillation of the MD velocity profiles
correlates well with the layering of the
fluid density normal to the wall
Local normal velocity
Local normal velocityNormal velocity Density
Large upper wall speed τσ /0.6=U 100Re ≈
Local tangential velocity
 For large U, the tangential velocity from
NS is larger than from MD
 MD velocity profiles are curved close to the
surface, and, therefore, shear rate is subject
to uncertainty
 The oscillations in the normal velocity profiles
are more pronounced in MD simulations
 The location of maximum in the normal velocity
profile correlates with the minimum in the density
profile
Pressure Contours from Navier-Stokes
min
max
Intrinsic slip length and the effect of local pressure along a rough surface
 L0 in MD is calculated from friction coefficient
kf due to uncertainty in estimating local shear rate
 L0 in MD and NS is shear rate dependent
 L0 in NS solution is calculated from 9th order
polynomial fit and is not pressure dependent
 The viscosity is constant within the error bars fk
L
µ
=0
s
t
f
u
P
k = Pt: tangential stress
us: slip velocity
Local intrinsic slip length Local pressure
3
15.015.2 −
±= ετσµ
 Good agreement between L0 from MD and
continuum on the right side of the peak
 The L0 from MD is about 3-4 smaller
than NS due to higher pressure regions
σ
Intrinsic slip length and the effect of local pressure
Intrinsic slip length vs. pressure for flat wall Bulk viscosity
 By increasing the temperature of the Langevin thermostat the effect of pressure on L0 is studied
 The bulk density and viscosity are independent of the temperature
 The friction coefficient only depends on the L0
 L0 is reduced about 3 as a function of pressure at higher U
 The discrepancy between Leff from MD and continuum is caused by high pressure region on the
left side of the peak
σ
Important conclusions
Department of Mechanical Engineering http://www.egr.msu.edu/~niavaran Michigan State University
n
nu
Lxu t
ss
∂
∂
=
)(
)()( γ
Fluid flow
Rough surface
 The flow over a rough surface with local slip boundary
condition was investigated numerically.
 The local slip boundary condition can not be
determined from continuum analysis. Instead, MD
simulations of flow over flat walls give which
is a highly nonlinear function of shear rate.
 Navier-Stokes equation for flow over rough surface
is solved using as a local boundary condition.
 The continuum solution reproduced MD results for
the rate-dependent slip length in the flow over a rough
surface.
 The main cause of discrepancy between MD and
continuum at higher shear rates is due to reduction in
the local intrinsic slip length in high pressure regions.
)(γsL
)(γsL
)(γsL
 The oscillatory pattern of the normal velocity profiles correlates well with the fluid layering
near the wall in Regions I and III.

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Modeling the combined effect of surface roughness and shear rate on slip flow of simple fluids

  • 1. Modeling the combined effect of surface roughness and shear rate on slip flow of simple fluids Department of Mechanical Engineering Michigan State University A. Niavarani and N.V. Priezjev, “Modeling the combined effect of surface roughness and shear rate of slip flow of simple fluids,” Phys. Rev. E 81, 011606 (2010). Anoosheh Niavarani and Nikolai Priezjev www.egr.msu.edu/~niavaran November 2009
  • 2. Introduction  MD simulations have shown that at the interface between simple1 and polymeric2 liquids and flat walls the slip length is a function of shear rate. h Solid wall U x z us u(z) 1 P. A. Thompson and S. M. Troian, Nature (1997) 2 N. V. Priezjev and S. M. Troian, Phys. Rev. Lett. (2004)  Surface roughness reduces effective slip length.  For flow of simple1 and polymeric2 liquids past periodically corrugated surface there is an excellent agreement between MD and continuum results for the effective slip length (if ). Constant local slip length from MD was used as a boundary condition for continuum simulation. 1 N. V. Priezjev and S. M. Troian, J. Fluid Mech. (2006) 2 A. Niavarani and N. V. Priezjev, J. Chem. Phys. (2008) dz zdu )( =γ Navier slip law L0 γ0Lus = γγ )(0Lus = )(0 γL dz zdu )( =γ σλ 30≥  The no-slip boundary condition works well for macro- flows, however, in micro and nanoflows molecular dynamics simulations and experiments report the existence of a boundary slip.
  • 3. x z n nu Lxu t ss ∂ ∂ = )( )()( γ Introduction Question: How to model the combined effect of surface roughness and shear rate? Solution 1: Perform full MD simulation of the flow past rough surface (very expensive computationally!!!). Solution 2: From MD simulation extract only slip length as a function of shear rate for flat walls. And then, use as a local boundary condition for the flow over rough surface in the Navier-Stokes equation. (Is it possible?) In this study we compare Solution 1 and Solution 2 )(γsL )(γsL Fluid flow Rough surface Department of Mechanical Engineering Michigan State University
  • 4. Details of molecular dynamics (MD) simulations ij i i i i j i V my m y f y≠ ∂ + Γ =− + ∂ ∑  1 τ − Γ = BT=1.1 kε ( ) ( ) 2 ( )i i Bf t f t mk T t tδ′ ′= Γ − if 12 6 LJ r r V (r) 4ε σ σ − −      = −           2 1/2 ( )mτ σ ε= σ LJ molecular length scale ε LJ energy scale LJ time scale Lennard-Jones potential: Department of Mechanical Engineering Michigan State University Langevin Thermostat Friction coefficient Equation of motion: Gaussian random force ρ w = 3.1 σ −3 ρ w = 0.67 σ −3 ρ = 0.81 σ −3 σλ 42≈=zL 27.0 2 == λ πa ka 3 81.0 − = σρFluid density
  • 5. ( ) sin(2 / )z ax xπ λ= Shear flow over a rough surface The effective slip length Leff and intrinsic slip length L0 Leff is the effective slip length, which characterizes the flow over macroscopically rough surface Department of Mechanical Engineering Michigan State University z R(x) : local radius of curvature Ls us R(x) u(z) x Local velocity profile Ls : local slip length L0 : intrinsic slip length extracted from MD simulation n zu Lxu ss ∂ ∂ = )( )( )( 111 0 xRLLs −=
  • 6. Equations of motion (penalty formulation): Boundary condition: Bilinear quadrilateral elements shape function Details of continuum simulations (Finite Element Method) Department of Mechanical Engineering Michigan State University R(x): local radius of curvature (+) concave, (–) convex L0: intrinsic slip length as a function of Galerkin formulation: )](/))[((0 xRuunLu sss +∇⋅=  γ )(/).( xRuun ss +∇=  γShear rate:
  • 7. γ us Department of Mechanical Engineering Michigan State University dz zdu )( =γγγ )(0Lus =  Slip length is a highly nonlinear function of shear rate  Velocity profiles are linear across the channel  Shear rate is extracted from a linear fit to velocity profiles  No-slip at the upper wall (commensurable wall/fluid densities) L0 h U us u(z) L0/σ MD simulations: Velocity profiles and slip length for flat walls Velocity profiles Slip length vs. shear rate
  • 8. Ls us R(x) u (z) : polynomial fit       + ∂ ∂ = )( )(0 xR u n u Lu ss s γ       + ∂ ∂ = )(xR u n u ss γ constant slip length at low shear rate rate-dependent slip at high shear rates )(0 γL λ πaka 2=  Blue line is a polynomial fit used in Navier-Stokes solution 9th order polynomial fit  Surface roughness reduces the effective slip length and its shear rate dependence monotonic increase  Excellent agreement between MD and NS at low shear rates but continuum results slightly overestimate MD at high shear rates  Constant slip length at low shear rate, highly nonlinear function of shear rate at high shear rates slight discrepancy excellent agreement detailed analysis Slip length vs. shear rate Effective slip length as a function of shear rate for a rough surface
  • 9. Detailed analysis of the flow near the curved boundary Local pressure Local temperature  Pressure: average normal force on wall atoms from fluids monomers within the cutoff radius  For pressure is similar to equilibrium case and is mostly affected by the wall shape  For pressure increase when and τσ /0.1≤U τσ /0.1>U 12.0/ <λx 54.0/ >λx 5.0/ =λx 3 /36.2 σε== flatPP  Average temperature is calculated in the first fluid layer  At small upper wall speeds, temperature is equal to equilibrium temperature  With increasing upper wall speed the temperature also increases and eventually becomes non-uniformly distributed First fluid layer
  • 10. Local velocity profiles in four region (I-IV) along the stationary lower wall τσ /0.1=U Small upper wall speed 17Re ≈ Local tangential velocity  At small U, excellent agreement between NS and MD especially inside the valley (IV)  The slip velocity above the peak (II) is larger than other regions  Even at low Re, the inertia term in the NS equation breaks the symmetry of the flow with respect to the peak => ut (I) > ut (III)  In regions I and III, negative and positive normal velocities are due to high pressure and low pressure regions  The oscillation of the MD velocity profiles correlates well with the layering of the fluid density normal to the wall Local normal velocity
  • 11. Local normal velocityNormal velocity Density Large upper wall speed τσ /0.6=U 100Re ≈ Local tangential velocity  For large U, the tangential velocity from NS is larger than from MD  MD velocity profiles are curved close to the surface, and, therefore, shear rate is subject to uncertainty  The oscillations in the normal velocity profiles are more pronounced in MD simulations  The location of maximum in the normal velocity profile correlates with the minimum in the density profile Pressure Contours from Navier-Stokes min max
  • 12. Intrinsic slip length and the effect of local pressure along a rough surface  L0 in MD is calculated from friction coefficient kf due to uncertainty in estimating local shear rate  L0 in MD and NS is shear rate dependent  L0 in NS solution is calculated from 9th order polynomial fit and is not pressure dependent  The viscosity is constant within the error bars fk L µ =0 s t f u P k = Pt: tangential stress us: slip velocity Local intrinsic slip length Local pressure 3 15.015.2 − ±= ετσµ  Good agreement between L0 from MD and continuum on the right side of the peak  The L0 from MD is about 3-4 smaller than NS due to higher pressure regions σ
  • 13. Intrinsic slip length and the effect of local pressure Intrinsic slip length vs. pressure for flat wall Bulk viscosity  By increasing the temperature of the Langevin thermostat the effect of pressure on L0 is studied  The bulk density and viscosity are independent of the temperature  The friction coefficient only depends on the L0  L0 is reduced about 3 as a function of pressure at higher U  The discrepancy between Leff from MD and continuum is caused by high pressure region on the left side of the peak σ
  • 14. Important conclusions Department of Mechanical Engineering http://www.egr.msu.edu/~niavaran Michigan State University n nu Lxu t ss ∂ ∂ = )( )()( γ Fluid flow Rough surface  The flow over a rough surface with local slip boundary condition was investigated numerically.  The local slip boundary condition can not be determined from continuum analysis. Instead, MD simulations of flow over flat walls give which is a highly nonlinear function of shear rate.  Navier-Stokes equation for flow over rough surface is solved using as a local boundary condition.  The continuum solution reproduced MD results for the rate-dependent slip length in the flow over a rough surface.  The main cause of discrepancy between MD and continuum at higher shear rates is due to reduction in the local intrinsic slip length in high pressure regions. )(γsL )(γsL )(γsL  The oscillatory pattern of the normal velocity profiles correlates well with the fluid layering near the wall in Regions I and III.