Alfonso M. Gañán-Calvo ,
In collaboration with Miguel A. Herrada, Antonio Ojeda-Monge, g j g Benjamin Bluth, Pascual Riesco-Chueca
ESI, Dept. Aerospace Engineering and Fluid Mechanics University of Seville, Spain.
IPPT PAN Seminars. Warsaw, January 2008
Focusing fluid
D1 D
r
L H
z
Focused fluid
V V
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Ganan-Calvo et al. 2007 Nature Phys. 3, 737-742 Gañán-Calvo 1997, W9700034ES
We may wish to control these structures & make them as small as possible
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We seek for the geometrical and operational conditionsg p
where the smallest possible, monodisperse droplets are generated at a productivity of practical use
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Pa
g
T φ θ
j
T C O l
l
φ
H
D
j
D
iθ θ
t SD
tParameter ranges in experiments (G-C et al.):
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The small yield per orifice has led to the design of multi-orifice devices:
.5 mm1
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3D (axisymmetric) Flow focusing in silicon
Ranges of pressure
FF FB
drop and flow rate:
FF FB
ΔP, bar 0.05 – 30 0.7 – 7.0 Q, uL/min 10 - 5800 10 - 14000
8 ) 1
(
1 Re
2
2 l
Q
lv Q
p ≈ ρ ≈ ρ
Δ
>>
2 / 1 4 /
8
l 1Q d ⎟⎟ ⎞
⎜⎜ ⎛ ρ ) 2
(
2 4j l
l
gas
v d
Q
p ≈ ρ ≈ π Δ
*A. M. Gañán-Calvo. Phys. Rev. Letter, 80, 285, 1998.
/
2 l
l
j
Q
d ≈ ⎜⎜ ⎝ Δ p ⎟⎟ ⎠ π
ρ
(Bernoulli)
( )
4 / 2 1 4
/ 1 2
8 ⎟⎟ ⎞
⎜⎜ ⎛
⎟ ⎠
⎜ ⎞
⎝
= ⎛
Qdo
ρ
l lCharacteristic length
2
⎟⎟
⎜⎜ ⎠
⎟ ⎝ Δ
⎜ ⎠
⎝
pdo
π
Based on previous characteristic dimension, four main parameters inform on the role played by surface tension, viscosity and geometry (orifice size and tube-orifice distance)
) 1 ( We
4 / 3 1 4 2
/ 2 3
p O Ql
l
⎟⎟ ⎞ ≥
⎜⎜ ⎛ Δ
⎟⎟ ⎞
⎜⎜ ⎛
= π ρ 2
1/4 3 2 1/4R ⎟ ⎞
⎜ ⎛ Δ
⎟ ⎞
⎜ ⎛ ρ
l Ql p viscosity and geometry (orifice size and tube orifice distance)) 1 8 (
We
l⎟⎟ ⎜⎜ ⎝
4⎟⎟ ⎠ ≥
O⎜⎜ ⎠
= ⎝
σ Re = ⎜ ⎝ ⎛
2⎟ ⎠ ⎞ ⎜⎜ ⎝
4⎟⎟ ⎠
l l l l
p Q
μ ρ π
4 / 1 4/ 1
4 4 2
/ 1 2
8 ⎟⎟
⎠
⎜⎜ ⎞
⎝
⎛
⎟ Δ
⎠
⎜ ⎞
⎝
= ⎛
p D G
ρ
lQlπ
GH=
H/
DVarious geometries:
H
D H GH
= /
Role played byWater 2,60
1
Ethanol
2,20 2,40
1
d50/do
1 60 1,80 2,00
GSD
0,1
1,20 1,40 1,60
0,01
1 10 100 1000 10000
Wel
1,00
1 10 100 1000 10000
Wel Flow Focusing
Flow Blurring
R l l d b d
Role played by and
l
10 Water 2,20
1
Water
Ethanol tFF
cFF
1 80 2,00 1
d50/do
1,60 1,80
GSD
0,1
1,20 1,40
0,01
1 10 100 1000 10000
Wel
1,00
1 10 100 1000 10000
Wel
20
We
l≈ 20
We
l≈
10 2,20
1 80 2,00 1
1.89
1,60 1,80
GSD
1
Water Ethanol
d50/do
1,20 0,1 1,40
1,00
1 10 100
Wel
0,01
1 10 100
Wel
• Why some liquids (water) exhibit larger sizes than predicted, in some (most) conditions?
• Why some conditions exhibit extremely good monodispersity (without external excitation)?
• Why some conditions exhibit extremely good monodispersity (without external excitation)?
• What exactly sets the minimum flow rate: C/A instability of the jet? Cone-jet flow transition?
• Is the dripping mode so bad?
Some recents FF numerical simulations:
• Liquid-liquid configuration for the production of microemulsions:
Michael M Dupin et al Physical Review E 73 2006 Michael M. Dupin et al. Physical Review E,73, 2006.
• Microbubbling: M. J. Jensen et al. Physics of Fluids, 18, 2006.
Geometrical configuration is fixed:
• R /R = 0 75
Q • R1/R = 0.75,
• R2/R = 1.75,
• R3/R = 3.5,
• L/R = 0 75 Qg
• L/R = 0.75.
• H/R = 1 Ql
Characteristic magnitudes:g
* R
* V=Q
g/( π R
2)IPPT PAN Seminars. Warsaw, January 2008
ratio densities
,
*
l
=
gρ α ρ
833 33 α =
ratio ies
viscosit ,
*
l g l
= μ β μ
ρ
Water-air experiments:55.55 833.33 β =
α
(gas) Weber
, We
*
2 g l
R
= V
σ ρ μ
(gas) Reynolds
, Re
*
g
g
VR
= μ
ρ σ
Case 1 Re = 465.8
Case 2 Re = 931.6
(tube) Reynolds
, Re
*
Rl l l g
R
= U μ
ρ
We = 8.13 We = 32.55In these cases, we have studied the effect of changing Q in:
ratio rates
Flow
,
*
g l
Q Q = Q
changing Q in:
1. Meniscus-jet shape.
2. Minimum flow rate Q* for stable jet.
3 Flow structure inside the meniscus 3. Flow structure inside the meniscus.
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-VOF scheme:
a) Explicit time advance b) CICSAM reconstruction
*Commercial code used: FLUENT 6.3Co e c a code used U 6 3
Basic mesh: Δz = Δr = 0.02 Refined mesh: Δ Δ 0 01 Refined mesh: Δz = Δr = 0.01
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Case 1 Q=0.004 Q
θ
din dout
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Case 1 Case 2
Q* (minimum) Q* (minimum)
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Case 1 Case 2
Diameters
“Contact angles”
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1 Re >>
(*) 8
2 ) 1 (
1 Re
4 2
2
2 l l
l l
gas
d
v Q Q
p π
ρ ≈ ρ
≈ Δ
>>
2 π d
j2 / 1 4 / 1 2
8
l l
j
Q
d p ⎟⎟
⎠
⎜⎜ ⎞
⎝
⎛
≈ Δ π
ρ p ⎠
⎝
Case 1 Case 2
Q = 0 00004
Q = 0.00024 Q = 0.00004
Q 0.000
Case 1
Q = 0.00024 Q 0.00024
Case 2 Q=0.00004 Q
High periodicity near the exit orifice (but not necessarily outside)
water (from syringe pump)
(Cole-Palmer 74900 Series) with a 20 ml syringe
jetting dripping
Air (pressure gauge)
370 mm OD, 150 mm ID stainless steel capillary Aluminium box
Two cameras to verify alignment
Air (pressure gauge)
PMMA window
4 mm stainless steel disk 75μm thick
200 μm orifice Variable distance H
PMMA window
μ
5 H=0,200mm Up
4
H=0,200mm Down H=0,150mm Up H=0,150mm Down H=0,100mm Up Pressure increasing
Jetting
3
Wel
H=0,100mm Down H=0,075mm Up H=0,075mm Down H=0,050mm Up
g
1
W 2 , p
H=0,050mm Down C/A transition
0 1
jetting dripping
Dripping
20 30 40 50 60 70
Rel
Optimum distance H: H/D~0.5
JETTING
DRIPPING
Case 1 Case 2
Experimental observations
• Co-flowing systems:
• S. L. Anna and H. C. Mayer, Phys. Fluids, 18, 121512 (2006).
• R. Suryo, O. A. Basaran, Phys. Fluids, 18, 082102 (2006)
Experimental observations
of recirculation cells: • Taylor cones: Barrero et al. Phys. Rev. E, 58, 7309-7314 (1998)
Saddle (max. pressure) Saddle (max. pressure)
Qr Qr
Saddle (max. pressure)
Q Q
( )
1/2( )
2
2 / 1
/ /
~
l s R
s l l
l
U Q
U R
δ ρ μ
δ
=
1
2 ) ~ /( ) Re
/(
~
/ = −
= R g s δl g μl ρl g μρ
r Q Q U Q R Q
Q
) 1 ( S ~ O
Q Q
Q
r l
l R
B
μ
−
=
R r
r l
l R
l
r Q Q s S R C C
S ~ ρ ( − )/μ ⇒ = / = 1 − 2 Re )
1 ( QB O
ρl
R
r
C C
s
r= C
1− C
2Re
Rs
1 2Re
Articles per year
Subject: Flow Focusing Subject: Flow Focusing(Source: Scopus)
300
200 250
100 150
0 50
1998 2000 2002 2004 2006
“Gañán-Calvo [21] pioneered the use of a technique now called flow-focusing where he used a co-flowing accelerating gas stream to reduce the radius of a liquid jet issuing out of a nozzle.[32] He showed that a nearly
monodisperse spray is produced when the Weber number which characterizes the relative importance of inertial force in the monodisperse spray is produced when the Weber number, which characterizes the relative importance of inertial force in the gas phase to the surface tension force, lies below a critical value.”
Suryo, R. & Basaran O. A. (2006) Phys. Fluids 18, 082102
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Most work (experimental) has been devoted to Most work (experimental) has been devoted to
liquid-liquid FF in microfluidics
A S L B N S H A (2003) A l Ph L 8 364 ( i d b 199)
(“planar” FF)
or gas in liquid FF (microbubbles) in microfluidics
•Anna, S.L., Bontoux, N., Stone, H.A. (2003), Appl. Phys. Lett. 85, 364 (cited by 199)
…or gas in liquid FF (microbubbles) in microfluidics
• Ganan-Calvo, A.M., Gordillo, J.M., (2001), Phys. Rev. Lett. 87, 274501 (cited by 89)
• Garstecki, P., Gitlin, I., Diluzio, W., Whitesides, G.M., Kumacheva, E., Stone, H.A.
(2004), Appl. Phys. Lett. 85, 2649 (cited by 66)
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… however, the original liquid-in-gas configuration has been subject of smaller attention:
• Ganan-Calvo, A.M. (1998), Phys. Rev. Lett. 80, 285 (cited by 69)
•Almagro, B., Gañán-Calvo, A.M., Canals, A. (2004), J. Anal. Atom. Spectrom., 19, 1346 (cited by 5)
•Arumuganathar, S., Irvine, S., McEwan, J.R., Jayasinghe, S.N. (2008), J. Appl. Polymer Sci. 107, 1215
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