nsf-reu project at uic
DESCRIPTION
Spreading of Herschel- Bulkley fluid using lubrication approximation. NSF-REU Project at UIC. Nadiya Klep Clemson University, SC David Pelot , UIC Dr. Yarin , UIC August 2,2013. Source: www.alibaba.com. Outline:. Purpose and applications Background S ample preparation - PowerPoint PPT PresentationTRANSCRIPT
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NSF-REU PROJECT AT UIC
Nadiya KlepClemson University, SCDavid Pelot, UICDr. Yarin, UIC August 2,2013
Spreading of Herschel-Bulkley fluid using lubrication approximation
Source: www.alibaba.com
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OUTLINE: Purpose and applications
Background
Sample preparation
Methods of data collection
Data
Results
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PURPOSE AND APPLICATION Small Angles <2˚
• Bearings• Screw extruder
Larger angles (5 ˚+)• Construction***
• Grout, mortar, joint compound
• Foods • Industrial processing
• Spreading of• Jams• Frosting• Peanut
butters• Etc.…
• Personal care products• Creams• Hair jells
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BACKGROUND:
Source: www.substech.com
Source: Schlichting, Boundary-Layer Theory,McGraw-Hill,Inc,1987.
Small angles in a nutshell:• small angle between the two surfaces.• convective acceleration• viscous forces predominate over inertial forces • Navier–Stokes equations becomes simpler:
• With the use of boundary conditions :at y = 0, u = U at x = 0, p = p0
at y = h, u = 0 and at x = l, p = p0
• and the fact that volume flow must be a constant:
From this the equation for velocity (:
Where:
• Backflow occurs in areas of increasingpressure near the stationary wall
V0
2
0y H dp y yu = V 1 - - 1 - H 2μ dx H H
dpdx
= 12μ(V0
2 H2 − QH3 )p ( x ) = p0 + 6 μV 0∫
0
x dxH2 − 12 μQ∫
0
x dxH3
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SAMPLE PREPARATION:
Source: Noveon Source: wikipedia.com
2. Neutralized with NaOH 3. Stress yield fluid: Herschel-Bulkley 1. 1.5% Solution of Carbopol
Source: www.pharmainfo.net
Source: www.alibaba.com
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CARBOPOL VISCOSITY
0.1 1 10 1001
10
100
1000 Vane Visc
Shear rate (1/s)
Visc
osity
(Pa·
s)
Power Law: fluids=µ Newtonian=non-Newtonian =µeff : eff. viscosity
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METHODS OF DATA COLLECTION: Apparatus to mimic the wedge: High-speed camera Phantom video player MatLab OriginPro graphing
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DATA AND ANALYSIS
Source: Schlinchting, Boundary-Layer Theory,McGraw-Hill,Inc,1987.
𝐹 𝑛=∫0
𝑙
𝜎𝑛𝑛𝑑𝑥
cos (𝛼)
2
0y H dp y yu = V 1 - - 1 - H 2μ dx H H
2 2nn n xx xy yyσ = n σ = sin (α) σ + 2sin(α)cos(α)σ + cos (α)σ
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RESULTS: At larger larger amount of fluid under
wedge faster reverse flow
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.00
5
10
15
20
25
30
35
40
x
0H
-0.20.00.30.50.81.0
f) 20 ˚, 1300um, 0.167m/s
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.00
10
20
30
40
50
60
70
80
0H
x
-0.2
0.0
0.3
0.5
0.8
1.0
e) 20˚, 600um, 0.167m/s
0.0 0.2 0.4 0.6 0.8 1.00
3
6
9
12
15
18
x
0H
-0.2
0.0
0.3
0.5
0.8
1.0
d) 10 ˚ , 1500um, 0.167m/s
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RESULTS: At same as h1 increases Force
decreases
-1 1 3 5 7 9 11 13 150
4
8
12
16
20
a
c
d
f
Time t, sec
Forc
e F
(N)
Ho=23 h1 =600um
Ho=34 h1=800um
Ho=15 h1=1500um
Ho=40 h1=1300um
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RESULTS: At same h1 increases Force, F (N) decreases
Ho=23 h1=600umHo=34 h1=800um
Ho=87 h1=600um
0 2 4 6 8 10 12 14 16 180
2
4
6
8
10
12
14
16a
c
e
Time t, sec
Forc
e F,
N
0 2 4 6 8 10 12 14 16 180
4
8
12b
d
f
Time t, sec
Forc
e F,
N
Ho=10 h1=1500umHo=18 h1=1500um
Ho=40 h1=1300um
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RESULTS: At same h1 & as V0 (U) increases
Force increases
0 2 4 6 8 10 12 140
1
2
3
4
5
6
7
8
9 g
h
e
f
TIme t, sec
Forc
e F,
N
V=0.167m/s
Ho=80 h1=650umV=0.24m/s
Ho=35 h1=1500um
Ho=87 h1=600um
Ho=40 h1=1300um
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SUMMARY OF RESULTS
Trial (Fig. 5)
Angle (deg)
H1 (mm)
Velocity (m∙s-1)
Force (N)
Viscosity (Pa∙s)
a 5 0.60 23 0.167 19.1 4.7b 5 1.50 10 0.167 15.0 5.9c 10 0.80 34 0.167 13.5 11.4d 10 1.50 18 0.167 7.9 8.3e 20 0.60 87 0.167 8.1 20.2f 20 1.30 40 0.167 6.8 19.5g 20 0.65 80 0.240 9.8 17.2h 20 1.50 35 0.240 9.7 20.0
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VISCOSITY
1
10
100
1000
0.1 1 10 100
Visc
osity
(Pa·
s)
Strain rate (1/s)
Max shear rate was calculated to be: 300s-1 : Viscosity: 0.6PasMin shear rate was calculated to be: 3s-1 : Viscosity 30 Pas
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Questions?
Thank you to: NSF grant # 1062943 Dr. Yarin David Pelot Everyone in Dr. Yarin’s group Professors Takoudis and Jursich Everyone involved with the REU program at UIC