Drop Impact and Spreading on Surfaces of Variable Wettability J.E Sprittles Y.D. Shikhmurzaev Bonn...

Post on 20-Dec-2015

215 views 2 download

Tags:

transcript

Swansea 2007

Drop Impact and Spreading on Surfaces of Variable WettabilityDrop Impact and Spreading on Surfaces of Variable Wettability

J.E Sprittles

Y.D. Shikhmurzaev

Bonn 2007

Swansea 2007

Motivation

• Drop impact and spreading occurs in many industrial processes.

• 100 million inkjet printers sold yearly.

• NEW: Inkjet printing of electronic circuits.

• Why study the ‘old problem’ of drops spreading on surfaces?

Swansea 2007

Worthington 1876 – First Experiments

Swansea 2007

Worthington’s Sketches

Millimetre sized drops of milk on smoked glass.

Swansea 2007

Modern Day Experiments (mm drops of water)

Courtesy of Romain Rioboo

Swansea 2007

Xu et al 03 Drops don’t splash at the top of Everest!

Swansea 2007

Renardy 03 et al - Pyramidal Drops

• Impact of oscillating water drops on super hydrophobic substrates

1

2 3

4

Swansea 2007

The Simplest Problem

• How does a drops behaviour depend on:

fluid properties,

drop speed,

drop size,.. etc?

Spread Factor

Apex Height

Contact Angle

a

0U

d

Swansea 2007

The Contact Angle

• In equilibrium the angle defines the wettability of a solid-liquid combination.

• How should we describe it in a dynamic situation?

2

More Wettable (Hydrophilic)More Wettable (Hydrophilic)

Less Wettable (Hydrophobic)Less Wettable (Hydrophobic)

Solid 1 Solid 2

1 2

Swansea 2007

Modelling of Drop Impact and Spreading Phenomena

• The Moving Contact Line Problem

• Conventional Approaches and

their Drawbacks

• The Shikhmurzaev Model

Swansea 2007

The Moving Contact Line Problem

Liquid

Inviscid Gas

Contact line

d

Contact angle

Solid

Swansea 2007

The Moving Contact Line Problem

No-SlipImpermeability

Kinematic condition Dynamic condition

Navier-StokesContinuity

d

Contact angle prescribed

• No solution!!!

Swansea 2007

The Conventional Approach

These are treated separately by:

1) Modifying the no-slip condition near the Contact Line (CL) to allow slip, e.g.

2) Prescribing the Contact Angle as a function of various parameters, e.g.

y

u

u

One must:1) Allow a solution to be obtained.2) Describe the macroscopic contact angle.

cd u3

Swansea 2007

Experiments Show This Is Wrong…

• Can one describe the contact angle as a function of the parameters?

“There is no universal expression to relate contact angle with contact line speed”.

(Bayer and Megaridis 06)

“There is no general correlation of the dynamic contact angle as a function of surface characteristics, droplet fluid and diameter and impact velocity.”

(Sikalo et al 02)

Swansea 2007

As in Curtain Coating

Used to industrially coat materials.

Conventional models:

Fixed substrate speed => Unique contact angle

Swansea 2007

‘Hydrodynamic Assist of Dynamic Wetting’

The contact angle depends on the flow field.

See: Blake et al 1994, Blake et al 1999, Clarke et al 2006

Swansea 2007

Angle Also Dependent On The Geometry: Flow Through a Channel

• The contact angle is dependent on d and U.

(Ngan & Dussan 82)

U

U

d

d

Conclusion:

Angle is determined by the flow field

Swansea 2007

The Shikhmuraev Model’s Predictions

Unlike conventional models:

• The contact angle is determined by the flow field.

• No stagnation region at the contact line.

• No infinite pressure at the contact line

=> Numerics easier

Swansea 2007

Shikhmurzaev ModelWhat is it?

• Generalisation of the classical boundary conditions.

• Considers the interface as a thermodynamic system with mass, momentum and energy exchange with the bulk.

• Used to relieve paradoxes in modelling of capillary flows such as …..

Swansea 2007

Some Previous Applications

Swansea 2007

The Shikhmurzaev Model Qualitatively (Flow near the contact line)

lg

sl

Solid

Gas

Width of interfacial layer

Liquid

Swansea 2007

Shikhmurzaev Model

• Solid-liquid and liquid-gas interfaces have an asymmetry of forces acting on them.

• In the continuum approximation the dynamics of the interfacial layer should be applied at a surface.

• Surface properties survive even when the interface's thickness is considered negligible.

Surface tension

Surface density

Surface velocity s

s

v

Swansea 2007

Shikhmurzaev Model

231

2s221

s11

cos

0evev

d

ss

)u(v4)41(

)v(

n)vu(

0v

0)nnI(n

nnn

||||11

11s11

1

11s1

s1

1

1

s

se

ss

s

se

s

t

ft

f

P

P

Uv

)Uu(v

)v(

n)vu(

)Uu()nnI(n

2

2||||21

||2

22s22

2

22s2

||||221

s

s

se

ss

s

se

s

t

P

On liquid-solid interfaces:On free surfaces: At contact lines:

θd

e2

e1

n

n

f (r, t )=0

22,12,12,1 )( ss ba

Swansea 2007

What if (the far field) ?

ed

22,12,12,1 )( s

ees

eeee ba

Uv

)Uu(v

Uu

)Uu()nnI(n

2

||||21

||2

||||

s

s

P On liquid-solid interfaces:On free surfaces: At contact lines:

see

s2,12,1

uv

uv

0u

0)nnI(n

nnn

1

||||1

1

s

s

e

ft

f

P

P

Swansea 2007

Summary

• Classical Fluid Mechanics => No Solution

• Conventional Methods Are Fundamentally Flawed

• The Shikhmurzaev Model Should Be Investigated

Swansea 2007

Our Approach

• Bulk: Incompressible Navier-Stokes equations

• Boundary: Conventional Model (for a start!)

• Use Finite Element Method.

• Assume axisymmetric motion (unlike below!).

Swansea 2007

Numerical Approach

• Use the finite element method:

Velocity and Free Surface quadratic

Pressure Linear

• The ‘Spine Method’ is used to represent the free surface

• ~2000 elements

• Second order time integration

Swansea 2007

The Spine Method(Scriven and co-workers)

The Spine

Nodes fixed on solid.

Nodes define free surface.

Swansea 2007

Code Validation

• Consider large deformation oscillations of viscous liquid drops.

• Compare with results from previous investigations, Basaran 91 and Meradji 01.

)cos(1)( nn Pfr Microgravity Experiment

• Compare aspect ratio of drop as a function of time.

• Starting position is

Swansea 2007

Second Harmonic – Large Deformation

For Re=100, f2 = 0.9

Swansea 2007

Second Harmonic – Large Deformation (cont)

• Aspect ratio of the drop as a function of time.

• A damped wave.

Swansea 2007

Fourth Harmonic – Large Deformation

For Re=100, f4 = 0.9

Swansea 2007

Drop Impact on a Hydrophilic (Wettable) Substrate

Re=100, We=10, β = 100, .30s

Swansea 2007

The Experiment – Water on GlassCourtesy of Dr A. Clarke (Kodak)

Swansea 2007

Drop Impact on a Hydrophobic (non-wettable) Substrate

Re=100, We=10, β = 100, .120s

Swansea 2007

The Experiment – Water on HydrophobeCourtesy of Dr A. Clarke (Kodak)

Swansea 2007

High Speed Impact

Radius = 25 m, Impact Speed = 12.2 m/s

Re=345, We=51, β = 100, .67s

Swansea 2007

Non-Spherical Drops on Hydrophobic Substrates

Radius = 1.75mm, Impact Speed = 0.4 m/s,Re=1435, We=8, .

175s

Swansea 2007

Impact + Spreading of Non-Spherical Dropson Hydrophobic Substrates

Swansea 2007

Impact + Spreading of Non-Spherical Dropson Hydrophobic Substrates

The Pyramid!

Swansea 2007

Impact + Spreading of Non-Spherical Dropson Hydrophobic Substrates

Experiment shows pinch off of drops from the apex

Swansea 2007

Impact + Spreading of Non-Spherical Dropson Hydrophobic Substrates

As in experiments, drop becomes toroidal

Swansea 2007

Current Work

• Quantitatively compare results against experiment.

• Incorporate the Shikhmurzaev model.

• Consider variations in wettability ….

Swansea 2007

How to Incorporate Variations in Wettability?

• Technologically, why are flows over patterned surfaces important?

• What are the issues with modelling such flows?

• How will a single change in wettability affect a flow?

• How about intermittent changes?

Swansea 2007

Using Patterned Surfaces

• Manipulate free surface flows using unbalanced surface tension forces.

Swansea 2007

Mock 05 et al - Drop Impact onto Chemically Patterned Surfaces

• Pattern a surface with areas of differing wettability.

• ‘Corrects’ deposition.

Swansea 2007

Mock 05 et al - Drop Impact onto Chemically Patterned Surfaces

• Pattern a surface to ‘correct’ deposition.Courtesy of Professor Roisman

Swansea 2007

The Problem• What if there is no free surface?

• Do variations in the wettability affect an adjacent flow?

1 2

2

Solid 1 Solid 2

What happens in this region?

Shear flow in the far fieldShear flow in the far field

Swansea 2007

Molecular Dynamics Simulations

Courtesy of Professor N.V. Priezjev

More wettable CompressedMore wettable CompressedLess wettable RarefiedLess wettable Rarefied

Swansea 2007

Hydrodynamic Modelling:Defining Wettability

• Defining wettability

ee 1lg1 cos

e1

lg

e1

• The Young equation:

The contact lineThe contact line

Solid 1

Swansea 2007

Hydrodynamic Modelling:Which Model?

• No-Slip

No effect

• Slip Models (e.g. Navier Slip)

There is no theta!

• A Problem..

We have no tools!

Swansea 2007

Qualitative Picture

e1 e2

BulkBulk

• Fluid particles are driven into areas of differing wettability.

• Surface properties take a finite time to relax to their new equilibrium state.

• What happens when flow drives fluid particles along the interface?

• Mass, momentum and energy exchange between surface and bulk.

• The process of interface formation.

0

2

Solid 1 Solid 2

• Consider region of interest.

Finite thicknes: For Visualisation Only

Finite thicknes: For Visualisation Only

Swansea 2007

Interface Formation Equations – Hydrodynamic of Interfaces

• Surface density is related to surface tension:

,)0(ss

.2,1;

coslg0 iiess

ie

• Equilibrium surface density defines wettability:

• Surface possesses integral properties such as a surface tension, ; surface velocity, and surface density, . sv

s

Equation of

State

Equation of

State

Input of Wettability

Input of Wettability

Swansea 2007

The Shikhmurzaev Model:Constant Wettability

Const se

s

BulkBulk

Interfacial Layer: For Visualisation Only. In the continuum limit..

Interfacial Layer: For Visualisation Only. In the continuum limit..

• If then we have Navier Slip

0n.u

t.utuun

u.t

Swansea 2007

Solid-Liquid Boundary Conditions – Shikhmurzaev Equations

.2

tu2

1tv

,tu2

1uun

s

ses

e

s

ses

e

s

BulkBulk

tu

Tangential velocityTangential velocity

Surface

velocity

Surface

velocity

Solid facing side of interface: No-slip

Solid facing side of interface: No-slip

se

se

s

ntLayer is for VISUALISATION only. In the continuum limit…

Layer is for VISUALISATION only. In the continuum limit…

Swansea 2007

Solid-Liquid Boundary Conditions – Shikhmurzaev Equations

.v

,nu

s

se

ss

se

s

BulkBulk

nutv s s

es sv

Continuity of surface mass

Continuity of surface mass

Normal velocityNormal velocity

Solid facing side of interface: Impermeability

Solid facing side of interface: Impermeability

Layer is for VISUALISATION only. In the continuum limit…

Layer is for VISUALISATION only. In the continuum limit…

Swansea 2007

Problem Formulation

• 2D, steady flow of an incompressible, viscous, Newtonian fluid over a stationary flat solid surface (y=0), driven by a shear in the far field.

• Bulk– Navier Stokes equations:

)vu, (u

• Boundary Conditions– Shear flow in the far field, which, using

gives:

.uuu,0u 2 p

.as0, 22

yxvSy

u

Swansea 2007

Results - Streamlines• Consider solid 1 (x<0) more wettable than solid 2 (x>0).

• Coupled, nonlinear PDEs were solved using the finite element method.

Swansea 2007

Results – Different Solid Combinations

• Consider different solid combinations.

110,10:3

110,60:2

60,10:1

21

21

21

ee

ee

ee

Swansea 2007

Results – Size of The Effect

eeJ 21 coscos

• Consider the normal flux out of the interface, per unit time, J.

• We find:

• The constant of proportionality is dependent on the fluid and the magnitude of the shear applied.

Swansea 2007

Results - The Generators of Slip

• Variations in slip are mainly caused by variations in surface tension.

1) Deviation of shear stress on the interface from equilibrium.

2) Surface tension gradients.

1) Deviation of shear stress on the interface from equilibrium.

2) Surface tension gradients.

Swansea 2007

Periodically Patterned Surface

• Consider Solid 1 More Wettable.

• Consider a=1 -> Strips Have Equal Width.

Swansea 2007

Results - Streamlines

Solid 2 less wettableSolid 2 less wettable

Qualitative agreementQualitative agreement

Swansea 2007

Results – Velocity Profiles

Tangential (slip) velocity varies around its equilibrium value of u=9.8.

Tangential (slip) velocity varies around its equilibrium value of u=9.8.

Fluxes are both in and out of the interfacial layer. Overall mass is conserved.

Fluxes are both in and out of the interfacial layer. Overall mass is conserved.

Swansea 2007

Further Work

Compare results with molecular dynamics simulations.

Devise experiments to test predictions.

Fully investigate periodic case.

Single transition investigation is in:

Sprittles & Shikhmurzaev, Phys. Rev. E 76, 021602 (2007).

Swansea 2007

Thanks!

Swansea 2007

Numerical Analysis of Formula for J

Shapes are numerical results.

Lines represent predicted flux

Shapes are numerical results.

Lines represent predicted flux

Swansea 2007

Interface Formation Equations + Input of Wettability

se2

se1

se

x

,.tanh2

1

2

11221 l

xse

se

se

se

se

Transition in wettability centred at x=y=0.

Transition in wettability centred at x=y=0.

Input of wettability

Input of wettability

Swansea 2007

Surface Equation of State

)( :2

)( :1

0

2

ss

ss ba

Break-up Dynamicwetting

Swansea 2007

Deviation of The Actual Contact Angle => Non Equilibrium Surface Tensions

Left: Curtain Coating Experiments (+) vs Theory (lines)Blake et al 1999 Wilson et al 2006

Right: Molecular Dynamics Koplik et al 1989

Swansea 2007

Comparison of Theory With Experiment

0.0001 0.0010 0.0100 0.1000 1.0000

0

30

60

90

120

150

180

d

C a

0.0001 0.0010 0.0100 0.1000 1.0000

0

30

60

90

120

150

180

d

Ca

Perfect wetting (Hoffman 1975; Ström et al. 1990; Fermigier & Jenffer 1991)

Partial wetting (□: Hoffman 1975;

: Burley & Kennedy 1976; , ,: Ström et al. 1990)

It has been shown that the theory is in good agreementwith all experimental data published in the literature.

Swansea 2007

Mechanism of Relaxation

s/P. 10-103 , 67

0.0 0.1 0.2 0.3

60

90

120

150

180d

C a

0.0 0.1 0.2 0.3 0.4 0.5

60

90

120

150

180

d

Ca

0.0 0.1 0.2 0.3 0.4

60

90

120

150

180

d

C a

Comparison of the theory with experimentson fluids with different viscosity (1.5-672 cP) confirms that the mechanism of the interface formation is diffusive in nature (J. Coll. Interface Sci. 253,196 (2002)). Estimates for parameters of the modelhave been obtained, in particular, showingthat for water-glycerol mixtures one has:

where