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Effects of large-scale geometry on wettingdynamics: a story of sliding drops
L. Limat, A. Daerr (MSC, CNRS & Univ. Paris Diderot)I. Peters, K. Winkels, J. Snoeijer (Univ. Twente) B. Andreotti (PMMH,Univ. Paris Diderot & ESPCI)
T. Podgorski (UJF Grenoble), J.-M. Flesselles (Saint-Gobain),N. Le Grand, E. Rio (Univ. Orsay)
coll: H.-A. Stone (Princeton), J. Eggers (Bristol)
GDR films, 2012
Partial wetting
Static drop
[Young](real world: hysteresisΘa < Θ < Θr )
Moving drop
advancing front steeper (Θ1 > Θa),receding gentler (Θ2 < Θr )
-10-2-5 10-305 10-3
0.884
0.882
0.880
0.878
0.876
0.874
0.872
0.870
10-9 10-8 10-7 10-6 10-5
60
40
20
0
Rolley et al, Delon et al.
Dynamics of wetting: multi-scale problem
drop
m
θap
θm
R
U=Rθap
θ
mλ ∼nm
apθ
.
3CaR/
from: Bonn et al2009
molecular scale: unknownout-of-equilibrium physics(evaporation, diffuse interfaces,. . . )
intermediate scale: viscosity vs.capillary pressure
large scale: outer boundarycondition
Viscous-capillary range
Huh & Scriven’s paradox
U
−∇px
z
σ = ηU/(θx)F = η(U/θ)
∫dx/x
ε = 12η(U2/θ)
∫dx/x
→∞Divergence both at small and large scales
Cox-Voinov relationViscous stress balanced by surface curvature gradient, alsodiverging:
3ηU/h = h∇(γ∆h)
θ3 = θ3micro ± 9Ca log x/a, Ca = ηU/γ
(+ for advancing CL; a: microscopic cut-off)
Wetting transitions
Wetting transitions (2)
Delon et al2008
60
50
40
30
20
10
0
1050–5–10
θapp
Ca(×10–3)
Ca ∗
CacCa >
Ca d
Contact linePlate
Liquidbath
Overhangingridge
Landau–LevichfilmCapillary jump
2 film thicknesses, 3 velocities (Ca∗ film entrainment, Ca> obliquecontact line speed; Cad is the ‘corner’ contact line speed in drops) flow must match different boundary conditions
Sliding dropsexperimental set-up
α
miroir
verre avecrevêtementfluoro-polymères 3M
huile de silicone 10 ... 1000 cP
source de lumière
camera
Liquid: silicon oil
η = 20.8 cPγ = 20.1 mN/mρ = 0.95 g/cm3
Fluor-polymer coating
Θa=54° Θr=48°
A L
Θa
A L
Θr
Sliding dropsobserved regimes
by increasing speed:
roundblunt cornercornercuspperling (small)perling (big)
singularity at the rear
Transition to corner shape
round
dessus côté reflet
corner
conical geometry (non-zero rear contactangle) !
Contact line normal speed
a)
b) c)
Ca sin Φ ≈ cst in corner regime(green solid line →)
1mma)
b)
c)
0
20
40
60
80
100
0
0,2
0,4
0,6
0,8
1
0 0,001 0,002 0,003 0,004 0,005 0,006 0,007
10 cP
θ (°) sinφ
Ca
θa
θr
Oval
Roundedcorner
Corner
Cusp
Pearling
sinΦ
)2Φ 1/3((3/2).Ca.tan
Drop shape
0
20
40
60
80
100
0
0,2
0,4
0,6
0,8
1
0 0,001 0,002 0,003 0,004 0,005 0,006 0,007
10 cP
θ (°) sinφ
Ca
θa
θr
Oval
Roundedcorner
Corner
Cusp
Pearling
sinΦ
)2Φ 1/3((3/2).Ca.tan
θa
θr gouttes ovales
Ω gouttes pointues
2Φ
2θa
2Ω
Cox-Voinov fit of receding contact angle reaches zero atCa = 0.004. Corner transition occurs slightly before.
Asymptotic matching problem
Visco-capillary solution (valid near contact line)must match
gravito-capillary solution (valid away from contact line):
limx→0
hgc(x) = limx→b
hvc(x)
where the matching scale for the inner solution is the scale atwhich gravity starts dominating viscous shear:
ρgh(b)P ≈ 3ηU/h(b), P = sinα− h′ cosα
viscosity molecule9 log
x
a
x/a Ca∗(x) Cao→c Cao→c
(cP) size (µm/nm) meas. theo.10 3 nm 129.0 200 / 0.1 4.0e-3 3.7e-3 3.5e-3
104 20 nm 80.0 200 / 28 5.1e-3 4.4e-3 4.4e-31040 100 nm 70.5 200 / 84 7.6e-3 6.2e-3 6.4e-3
20 n.c. 80 50 / 7 6.0e-3 4.0e-3 4.5e-3
How is the wetting transition avoided ?
x
y
z
R
2d
3d
2d
U
−∇px
z
viscous stress ⇔ longitudinalcurvature variation
3d
x
y
zaugmentationcourbure &pression
viscous stress ⇔ transversecurvature variation
Dewetting in conical geometry
x
y
zΩ
Φθ
Self-similar solutions h(x , y) = Ca1/3xH(y/x) by Stone & Limat(2003), Snoeijer et al(2005) for 3d lubrication model
3Cahx = ∇[h3∇(∆h)
]∧ ht = −U hx
link cone opening angles Ω and Φ:
tan Ω =35
16Ca tan2 Φ
Dewetting in conical geometry (2)
Imposing a Cox-Voinov-type law on the cone boundary selects theopening angle:
Ca =2Φ
35 + 18(log ba )Φ2
What about the tip itself ?
Corner formation a way to avoid wetting transition: normalcontact line speed reduced to U0 sin Φ < U0.
x
y
z
R
2d
3d
But: always small region near tip where contact line speed is U0.
Tip curvature increases
. . . but remains finite.
Tip matching
Idea: match near 2d solution at tip to 3d cone solution at scale R.
x
y
z
R
2d
3d
θ(R)3 = θ3e − 9Ca logR
a∧ θ(R) = Ω
⇒ R ≈ a exp[(θ3e − Omega3)/9Ca] ≈ a exp[θ3e/9Ca]
Tip matching advanced
More precise matching procedure with hyperbolic Ansatzh(x , y) = h0(x)[1− y2/w(x)2],w(x)2 ≈ 2Rx + Φ2x2 yields
Ω3 = θ3e − 9Ca logβR
Φ2awith Ω3 ≈ 35
16Ca tan2 Φ, β = O(1)
1
R≈ f (Φ)
aexp[− θ3e
9Ca]
tip size comes from microscopic scale !
Tip measurements in two geometries: sliding drop &immersion set-up
turntable setup: Riepen et al. 2008 (Twente)
wafer velocity
Axi-symmetric
side view
camera
bott
om
vie
w
cam
era
water
supply
water
supply
motor
wafer
extraction
flow
a) waferside view
bottom view
b)
Microscopic origin
Conclusion
• Drops sliding down an incline develop a conical pointsingularity, on the already singular contact line.
• The regularisation of this point singularity involves an ‘inner’length scale, not the ‘outer’ one.
• Corner is a truly three-dimensional, self-similar solution (bothcontact line and bulk dissipation select the opening angle).
• Classical hydrodynamics with a molecular cut-off describesthese experiments satisfactorily. Need lower speeds to seemicroscopic effects ?
Contact angle varies along drop perimeter
• How to go smoothly from Θa at front toΘr at rear ?
• On substrate with hysteresis, whathappens at transition from advancing(red) to receding (blue) part ?
Contact angle measurementthrough light refraction
laser sheet
glassplate
translucidscreen
CCDcamera
α
translucentscreen
Φ
laserdiode
sliding puddle
Φ∆
a) b)
Measurement scale:∼ 10µm
Results on contact angleMeasurement around a single drop
Θas
Θrs
Ca sin Φ: capillary number based on contact line speed
Results on contact angleMeasurement around a single drop
Θas
Θrs
Ca sin Φ: capillary number based on contact line speed
Results on contact angleMeasurement around a single drop
Ca sin Φ: capillary number based on contact line speed
Results on contact angleComparison to measurements at front and rear of multiple drops
et
black discs: front/rear of drops empty circles: around one drop
Velocity field of sliding drop
1mma)
b)
c)
Velocity ⊥ contact line
Velocity field of sliding drop
1mma)
b)
c)
Velocity ⊥ contact line
Velocity normal to contact linemicroscopic interpretation
Near contact line,
• viscous stresses and balancing forces(capillarity, disjoining pressure, . . . ) diverge
• properties vary much slower tangent to CLthan normal to CL
tangential velocity component quickly dampedby viscosity⇒ ~u ⊥ contact line
situation essentially symmetry wrt planenormal to contact line
Axis of
symmetry