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DHR Rheology Theory

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ƒ Basics in Rheology Theory ƒ Oscillation
ƒ Linear Viscoelasticity
ƒ TA Rheometers
ƒ Instrumentation
ƒ Choosing a Geometry
ƒ Calibrations
ƒ Flow Tests
ƒ Viscosity
ƒ Setting up Flow Tests
ƒ Setting up Oscillation Tests
ƒ Transient Testing
ƒ Applications of Rheology
ƒ Polymers
ƒ Structured Fluids
ƒ Advanced Accessories
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Rheology: The study of
stress-deformation relationships
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ƒ Rheology is the science of flow and deformation
of matter
ƒ The word ‘Rheology’ was coined in the 1920s by
Professor E C Bingham at Lafayette College in Indiana
ƒ Flow is a special case of deformation
ƒ The relationship between stress and deformation
is a property of the material
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Top plate Area = A
x(t)
Velocity = V0
Force = F
y
y
Bottom Plate
Velocity = 0
x
Shear Stress, Pascals
Shear Strain, %
Shear Rate,
sec-1
σ=
γ=
F
A
x(t )
γ =
y
η=
σ
γ
Viscosity, Pa⋅s
γ
t
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Ω
r
θ
h
r = plate radius
h = distance between plates
M = torque (μN.m)
θ = Angular motor deflection (radians)
Ω= Motor angular velocity (rad/s)
Stress (σ
σ)
ߪ ൌ ഏೝమయ ൈM
Strain (γγ)
θ
ߛ ൌ ೓ೝ ൈθ
ೝ
ߛሶ
ൌ
ൈΩ
Ω
Strain rate (ߛሶ )
೓
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ARES G2
DHR
Controlled Strain
Dual Head
Controlled Stress
Single Head
SMT
CMT
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Dual head or SMT
Separate motor & transducer
Measured
Torque
(Stress)
Single head or CMT
Combined motor & transducer
Displacement
Sensor
Transducer
Measured Strain
or Rotation
Non-Contact
Drag Cup
Motor
Applied
Torque
(Stress)
Sample
Applied
Strain or
Rotation
Direct Drive
Motor
Static
Plate
^ƚĂƚŝĐWůĂƚĞ
Note: With computer feedback, DHR and AR can work in controlled strain/shear
rate, and ARES can work in controlled stress.
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ƒ Rheometer – an instrument that measures both viscosity and
viscoelasticity of fluids, semi-solids and solids
ƒ It can provide information about the material’s:
ƒ Viscosity - defined as a material’s resistance to deformation and
is a function of shear rate or stress, with time and temperature
dependence
ƒ Viscoelasticity – is a property of a material that exhibits both
viscous and elastic character. Measurements of G’, G”, tan δ with
respect to time, temperature, frequency and stress/strain are
important for characterization.
ƒ A Rheometer works simply by relating a materials property from how hard it’s
being pushed, to how far it moves
ƒ by commanding torque (stress) and measuring angular displacement (strain)
ƒ by commanding angular displacement (strain) and measuring torque (stress)
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From the definition of rheology,
the science of flow and deformation of matter
or
the study of stress (Force / Area) – deformation
(Strain or Strain rate) relationships.
Fundamentally a rotational rheometer will apply or
measure:
1. Torque (Force)
2. Angular Displacement
3. Angular Velocity
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ƒ
ƒ
In a rheometer, the stress is calculated from the
torque.
The formula for stress is: σ сΜ п <σ
Where
σ = Stress (Pa or Dyne/cm2)
Μ = torque in N.m or gm.cm
<σ = Stress Constant
ƒ
The stress constant, <σ, is a geometry dependent factor
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In a SMT Rheometer, the angular displacement
is directly applied by a motor.
ƒ
The formula for strain is:
γ с<γ п θ
йγ сγ п ϭϬϬ
where γ = Strain
<γ = Strain Constant
θ = Angular motor deflection (radians)
ƒ
The strain constant, <γ, is a geometry dependent factor
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In Spec
Describe
Correctly
σ M ⋅ Kσ
G= =
γ
θ ⋅ Kγ
Rheological
Parameter
Constitutive
Equation
Raw rheometer
Specifications
Geometric
Shape
Constants
The equation of motion and other relationships have been used to determine the appropriate
equations to convert machine parameters (torque, angular velocity, and angular displacement) to
rheological parameters.
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ƒ
In a SMT rheometer, the angular speed is directly
controlled by the motor).
ƒ
The formula for shear rate is:
ߛሶ ൌ ‫ܭ‬ఊ ൈ :
where
ƒ
ߛሶ = Shear rate
<γ = Strain Constant
Ω = Motor angular velocity in rad/sec
The strain constant, <γ, is a geometry dependent factor
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In Spec
Describe
Correctly
σ M ⋅ Kσ
η= =
γ Ω ⋅ K γ
Rheological
Parameter
Constitutive
Equation
Raw rheometer
Specifications
Geometric
Shape
Constants
The equation of motion and other relationships have been used to determine the appropriate
equations to convert machine parameters (torque, angular velocity, and angular displacement) to
rheological parameters.
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Specification
Bearing Type, Thrust
Bearing Type, Radial
Motor Design
Minimum Torque (nN.m) Oscillation
HR-3
HR-2
HR-1
Magnetic
Porous Carbon
Drag Cup
0.5
Magnetic
Porous Carbon
Drag Cup
2
Magnetic
Porous Carbon
Drag Cup
10
Minimum Torque (nN.m) Steady
Shear
Maximum Torque (mN.m)
5
10
20
200
200
150
Torque Resolution (nN.m)
0.05
0.1
0.1
Minimum Frequency (Hz)
1.0E-07
1.0E-07
1.0E-07
Maximum Frequency (Hz)
100
100
100
Minimum Angular Velocity (rad/s)
0
0
0
Maximum Angular Velocity (rad/s)
300
300
300
Optical
encoder
Standard
Optical
encoder
N/A
Optical
encoder
N/A
Displacement Resolution (nrad)
2
10
10
Step Time, Strain (ms)
15
15
15
Step Time, Rate (ms)
5
5
5
FRT
FRT
FRT
Maximum Normal Force (N)
50
50
50
Normal Force Sensitivity (N)
0.005
0.005
0.01
0.5
0.5
1
Displacement Transducer
Optical Encoder Dual Reader
Normal/Axial Force Transducer
Normal Force Resolution (mN)
,ZͲϭ
,ZͲϮ
,ZͲϯ
DHR - DMA mode (optional)
Motor Control
FRT
Minimum Force (N) Oscillation
Maximum Axial Force (N)
Minimum Displacement (μm)
Oscillation
Maximum Displacement (μm)
Oscillation
Displacement Resolution (nm)
Axial Frequency Range (Hz)
0.1
50
1.0
100
10
1 x 10-5 to 16
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Force/Torque Rebalance Transducer (Sample Stress)
Transducer Type
Transducer Torque Motor
Transducer Normal/Axial Motor
Minimum Torque (μN.m) Oscillation
Minimum Torque (μN.m) Steady Shear
Maximum Torque (mN.m)
Torque Resolution (nN.m)
Transducer Normal/Axial Force Range (N)
Transducer Bearing
Force/Torque
Rebalance
Brushless DC
Brushless DC
0.05
0.1
200
1
0.001 to 20
Groove Compensated
Air
Driver Motor (Sample Deformation)
Maximum Motor Torque (mN.m)
Motor Design
Motor Bearing
Displacement Control/ Sensing
Strain Resolution (μrad)
Minimum Angular Displacement (μrad)
Oscillation
Maximum Angular Displacement (μrad)
Steady Shear
Angular Velocity Range (rad/s)
Angular Frequency Range (rad/s)
Step Change, Velocity (ms)
Step Change, Strain (ms)
800
Brushless DC
Jeweled Air, Sapphire
Optical Encoder
0.04
1
Unlimited
1x 10-6 to 300
1x 10-7 to 628
5
10
Orthogonal Superposition (OSP) and
DMA modes
Motor Control
FRT
Minimum Transducer Force (N)
Oscillation
Maximum Transducer Force
(N)
Minimum Displacement (μm)
Oscillation
Maximum Displacement (μm)
Oscillation
Displacement Resolution (nm)
Axial Frequency Range (Hz)
0.001
20
0.5
50
10
1 x 10-5 to 16
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Concentric
Cylinders
Cone and
Plate
Parallel
Plate
Very Low
to Medium
Viscosity
Very Low
to High
Viscosity
Very Low
Viscosity
to Soft Solids
Water
to
Torsion
Rectangular
Solids
Steel
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ƒ Assess the ‘viscosity’ of your sample
ƒ When a variety of cones and plates are available, select diameter
appropriate for viscosity of sample
ƒ Low viscosity (milk) - 60mm geometry
ƒ Medium viscosity (honey) - 40mm geometry
ƒ High viscosity (caramel) – 20 or 25mm geometry
ƒ Examine data in terms of absolute instrument variables
torque/displacement/speed and modify geometry choice to move
into optimum working range
ƒ You may need to reconsider your selection after the first run!
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Strain Constant:
‫ܭ‬ఊ ൌ ௛௥
(to convert angular velocity, rad/sec, to shear rate,
1/sec, at the edge or angular displacement, radians,
to shear strain (unitless) at the edge. The radius, r,
and the gap, h, are expressed in meters)
'ĂƉ;ŚͿ
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Stress Constant:
‫ܭ‬ఙ ൌ గ௥ଶ య
(to convert torque, N⋅m, to shear stress at the
edge, Pa, for Newtonian fluids. The radius, r, is
expressed in meters)
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ƒ Low/Medium/High Viscosity
Liquids
ƒ Soft Solids/Gels
ƒ Thermosetting materials
ƒ Samples with large particles
ƒ Samples with long relaxation time
ƒ Temperature Ramps/ Sweeps
ƒ Materials that may slip
ƒ Crosshatched or Sandblasted plates
ƒ Small sample volume
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Shear Stress
20 mm
40 mm
60 mm
As diameter decreases, shear stress increases
ʹ
ߪൌ‫ ܯ‬ଶ
ߨ‫ݎ‬
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2 mm
Shear
Rate
Increases
1 mm
0.5 mm
As gap height decreases, shear rate increases
‫ݎ‬
ߛሶ ൌ ȳ
݄
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ƒ For a given angle of deformation, there is a greater arc of
deformation at the edge of the plate than at the center
݀‫ݔ‬
ߛൌ
݄
dx increases further from the center,
h stays constant
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ƒ The cone shape produces a smaller gap height closer to inside,
so the shear on the sample is constant
݀‫ݔ‬
ߛൌ
݄
h increases proportionally to dx, γ is uniform
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Strain Constant:
‫ܭ‬ఊ ൌ ఉଵ
(to convert angular velocity, rad/sec, to shear rate.
1/sec, or angular displacement, radians, to shear strain,
which is unit less. The angle, β, is expressed in radians)
ଷ
Stress Constant: ‫ܭ‬ఙ ൌ ଶగ௥ య
(to convert torque, N⋅m, to shear stress, Pa.
The radius, r, is expressed in meters)
Truncation (gap)
Diameter (2⋅⋅r)
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ƒ Very Low to High Viscosity Liquids
ƒ High Shear Rate measurements
ƒ Normal Stress Growth
ƒ Unfilled Samples
ƒ Isothermal Tests
ƒ Small Sample Volume
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Shear Stress
20 mm
40 mm
60 mm
As diameter decreases, shear stress increases
͵
ߪൌ‫ܯ‬
ʹߨ‫ ݎ‬ଷ
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Shear Rate
Increases
2°
1°
0.5 °
As cone angle decreases, shear rate increases
ͳ
ߛሶ ൌ ȳ
ߚ
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Typical Truncation Heights:
1° degree ~ 20 - 30 microns
2° degrees ~ 60 microns
4° degrees ~ 120 microns
Cone & Plate
Truncation Height = Gap
Gap must be > or = 10 [particle size]!!
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× Under Filled sample:
Lower torque contribution
× Over Filled sample:
Additional stress from
drag along the edges
9 Correct Filling
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Strain Constant:
‫ͳݎ‬ଶ ൅ ‫ʹݎ‬ଶ
‫ܭ‬ఊ ൌ
‫ʹݎ‬ଶ ‫ͳݎ‬ଶ
(to convert angular velocity, rad/sec, to shear rate,
1/sec, or angular displacement, radians, to shear
strain (unit less). The radii, r1 (inner) and r2 (outer),
are expressed in meters)
Stress Constant: ‫ܭ‬ఙ ൌ ଵ ସగ௟
ଶ
ଶ *
‫ ͳݎ‬൅ ‫ʹ ݎ‬
‫ʹݎ‬ଶ ‫ͳݎ‬ଶ
(to convert torque, N⋅m, to shear stress, Pa. The bob
length, l, and the radius, r, are expressed in meters)
*Note including end correction factor. See TRIOS Help
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ƒ
Use for very low viscosity systems (<1 mPas)
r1
r2
h
r3
r4
Strain Constant:
‫ͳݎ‬ଶ ൅ ‫ʹݎ‬ଶ
‫ܭ‬ఊ ൌ
‫ʹݎ‬ଶ െ‫ͳݎ‬ଶ
Stress Constant:
௥ଵమ ା௥ଶమ
‫ܭ‬ఙ ൌ ସగ௛ή௥ మ ௥ మ ା௥ మ
ଶ
ଵ
ଷ
ARES Gap Settings: standard operating gap DW = 3.4 mm
narrow operating gap DW = 2.0 mm
Use equation Gap > 3 × (R2 –R1)
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ƒ Low to Medium Viscosity Liquids
ƒ Unstable Dispersions and Slurries
ƒ Minimize Effects of Evaporation
ƒ Weakly Structured Samples (Vane)
ƒ High Shear Rates
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‫ܭ‬ఊ ൌ
‫ݐ‬
݈ ͳ െ ͲǤ͵͹ͺ
௧ ଶ
௪
w = Width
l = Length
t = Thickness
͵ ൅ ଵǤ଼
௪
‫ܭ‬ఛ ൌ
‫ ݓ‬ή ‫ݐ‬ଶ
Advantages:
ƒ
High modulus samples
ƒ
Small temperature
Disadvantages:
ƒ
No pure Torsion mode for
high strains
gradient
ƒ Simple to prepare
Torsion cylindrical also available
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ƒ
Torsion and DMA geometries allow solid samples to be
characterized in a temperature controlled environment
ƒ
ƒ
Torsion measures G’, G”, and Tan δ
DMA measures E’, E”, and Tan δ
ƒ
ƒ
ARES G2 DMA is standard function (50 μm amplitude)
DMA is an optional DHR function (100 μm amplitude)
Rectangular and
cylindrical torsion
DMA 3-point bending and tension
(cantilever not shown)
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Geometry
Application
Advantage
Disadvantage
Cone/plate
fluids, melts
viscosity > 10mPas
true viscosities
temperature ramp difficult
Parallel Plate
fluids, melts
viscosity > 10mPas
easy handling,
temperature ramp
shear gradient across
sample
Couette
low viscosity samples
< 10 mPas
high shear rate
large sample volume
Double Wall Couette
very low viscosity
samples < 1mPas
high shear rate
cleaning difficult
Torsion Rectangular
solid polymers,
composites
glassy to rubbery
state
Limited by sample stiffness
Solid polymers, films,
Composites
Glassy to rubbery
state
DMA
Limited by sample stiffness
(Oscillation and
stress/strain)
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Instrument Calibrations
ƒ
ƒ
ƒ
Geometry Calibrations:
ƒ
ƒ
ƒ
ƒ
ƒ
Inertia (Service)
Rotational Mapping
Inertia
Friction
Gap Temperature
Compensation
Rotational Mapping
Details in Appendix #4
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ƒ Instrument Calibrations
ƒ
ƒ
ƒ
ƒ
Transducer
Temperature Offsets
Phase Angle (Service)
Measure Gap Temperature
Compensation
ƒ Geometry Calibrations:
ƒ Compliance and Inertia (from table)
ƒ Gap Temperature Compensation
ƒ Details in Appendix #4
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ƒ Rheometers are calibrated from the factory and again at
installation.
ƒ TA recommends routine validation or confidence checks
using standard oils or Polydimethylsiloxane (PDMS).
ƒ PDMS is verified using a 25 mm parallel plate.
ƒ Oscillation - Frequency Sweep: 1 to 100 rad/s with 5% strain at 30°C
ƒ Verify modulus and frequency values at crossover
ƒ Standard silicone oils can be verified using cone, plate or
concentric cylinder configurations.
ƒ Flow – Ramp: 0 to 88 Pa at 25°C using a 60 mm 2° cone
ƒ
Service performs this test at installation
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ƒ Set Peltier temperature to 25°C and
equilibrate.
ƒ Zero the geometry gap
ƒ Load sample
ƒ Be careful not to introduce air bubbles!
ƒ Set the gap to the trim gap
ƒ Lock the head and trim with non-absorbent
tool
ƒ Important to allow time for temperature equilibration.
ƒ Go to geometry gap and initiate the
experiment.
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ƒ Viscosity is…
ƒ
ƒ
ƒ
“lack of slipperiness”
synonymous with internal friction
resistance to flow
ƒ The Units of Viscosity are …
ƒ SI unit is the Pascal.second (Pa.s)
ƒ cgs unit is the Poise
ƒ 10 Poise = 1 Pa.s
ƒ 1 cP (centipoise) = 1 mPa.s (millipascal second)
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In Spec
Describe
Correctly
σ M ⋅ Kσ
η= =
γ Ω ⋅ K γ
Rheological
Parameter
Constitutive
Equation
Raw rheometer
Specifications
Geometric
Shape
Constants
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6
6
6
6
6
6
6
6
Asphalt Binder -------------Polymer Melt ---------------Molasses --------------------Liquid Honey ---------------Glycerol ---------------------Olive Oil ---------------------Water ------------------------Air -----------------------------
100,000
1,000
100
10
1
0.01
0.001
0.00001
Need for
Log scale
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ƒ Newtonian Fluids - constant proportionality between
shear stress and shear-rate
ƒ Non-Newtonian Fluids - Viscosity is time or shear rate
dependent
ƒ
Time:
ƒ
ƒ
ƒ
ƒ
At constant shear-rate, if viscosity
Decreases with time – Thixotropy
Increases with time - Rheopexy
Shear-rate:
ƒ
ƒ
Shear - thinning
Shear - thickening
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σ, Pa
η, Pa.s
Ideal Yield Stress
(Bingham Yield)
γ ,1/s
γ ,1/s or σ, Pa
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105
103
103
η, Pa.s
η, Pa.s
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101
10-1
10-6
10-4
10-2
100
102
104
101
10-1
10-1
10-0
10-1
102
103
σ, Pa
,1/s
σ, Pa
105
103
,GHDO<LHOG6WUHVV
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ƒ Another name for a shear thinning
fluid is a pseudo-plastic
101
10-1
10-6 10-4 10-2 100 102
104
γ ,1/s
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Log η, Pa.s
ƒ Dilatant material resists
deformation more than in
proportion to the applied
force (shear-thickening)
Log ߛሶ , 1/s
ƒ Cornstarch in water or sand
on the beach are actually
dilatant fluids, since they do
not show the timedependent, shear-induced
change required in order to
be labeled rheopectic
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Viscosity
Rheopectic
Shear Rate = Constant
Thixotropic
time
ƒ Rheopectic materials
become more viscous
with increasing time of
applied force
ƒ Higher concentration
latex dispersions and
plastisol paste materials
exhibit rheopectic
behavior
ƒ Thixotropic materials
become more fluid with
increasing time of applied
force
ƒ Coatings and inks can
display thixotropy when
sheared due to structure
breakdown
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ƒ Flow Experiments
ƒ Constant shear rate/stress (or Peak hold)
ƒ Continuous stress/rate ramp and down
ƒ Stepped flow (or Flow sweep)
ƒ Steady state flow
ƒ Flow temperature ramp
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Stress /Rate
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ƒ
Constant rate vs. time
ƒ
Constant stress vs. time
USES
ƒ Single point testing
ƒ Scope the time for steady state under certain rate
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3.500
4.000
Hand Wash Rate 1/s
3.500
3.000
3.000
2.500
viscosity (Pa.s)
shear stress (Pa)
2.500
2.000
2.000
1.500
Viscosity at 1 1/s is 2.8 Pa⋅s
1.500
1.000
1.000
0.5000
0.5000
0
0
5.0000
10.000
15.000
time (s)
20.000
25.000
0
30.000
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Deformation
m =Stress rate
(Pa/min)
ƒ
Stress is applied to
material at a constant
rate. Resultant strain
is monitored with time.
time (min)
USES
ƒ Yield stress
ƒ Scouting Viscosity Run
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Deformation
ƒ
σ
time
Stress is first increased,
then decreased, at a
constant rate. Resultant
strain is monitored with
time.
USES
ƒ “Pseudo-thixotropy” from Hysteresis loop
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Run in Stress Control
TA Instruments
500.0
shear stress (Pa)
400.0
300.0
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200.0
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FORDB3.04F-Down step
FORDB3.05F-Up step
FORDB3.05F-Down step
100.0
0
0
0.1000
0.2000
0.3000
shear rate (1/s)
0.4000
0.5000
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Deformation
σ
Žƌ
ߛሶ
ƒ Stress is applied to sample.
Viscosity measurement is taken
when material has reached steady
state flow. The stress is
increased(logarithmically) and the
process is repeated yielding a
viscosity flow curve.
Data point saved
time
Delay time
σ
Žƌ
ߛሶ
USES
Steady State Flow
γ or σ = Constant
ƒ
ƒ
Viscosity Flow Curves
Yield Stress Measurements
time
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ƒ A series of logarithmic stress steps allowed to reach steady state, each
one giving a single viscosity data point:
Viscosity
Data at each
Shear Rate
Shear
Thinning
Region
Time
Shear Rate, 1/s
η = σ / (d γ/dt)
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Control variables:
ƒ Shear rate
ƒ Velocity
ƒ Torque
ƒ Shear stress
Steady state algorithm
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0.8000
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0.7000
Which material would do a better job
coating your throat?
viscosity (Pa.s)
0.6000
0.5000
0.4000
0.3000
0.2000
0.1000
0
0.1000
1.000
10.00
shear rate (1/s)
100.0
1000
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10000
A.01F-Flow step
B.01F-Flow step
Low shear rates B>A
viscosity (Pa.s)
1000
100.0
10.00
Medium shear rates A>B
1.000
High shear rates B>A
0.1000
1.000E-4
1.000E-3
0.01000
0.1000
1.000
10.00
100.0
1000
shear rate (1/s)
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y
y
y
y
ƒ Hold the rate or stress
constant whilst
ramping the
temperature.
time (min)
USES
ƒ Measure the viscosity change vs. temperature
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Notice a nearly 2 decade decrease in viscosity. This displays the importance of
thermal equilibration of the sample prior to testing.
i.e. Conditioning Step or equilibration time for 3 to 5 min
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ƒ Small gaps give high shear rates
ƒ Be careful with small gaps:
ƒ
ƒ
ƒ
Gap errors (gap temperature compensation) and shear
heating can cause large errors in data.
Recommended gap is between 0.5 to 2.0 mm.
Secondary flows can cause increase in viscosity curve
ƒ Be careful with data interpretation at low shear rates
ƒ Surface tension can affect measured viscosity, especially
with aqueous materials
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Surface tension at low torques
Secondary flows at high shear rates
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ƒ
Wall slip can manifest as “apparent double yielding”
ƒ
Can be tested by running the same test at different gaps
ƒ
For samples that don’t slip, the results will be independent of the gap
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When Stress Decreases with
Shear Rate, it indicates that
sample is leaving the gap
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ƒ Edge Failure – Sample leaves gap because of normal
forces
ƒ Look at stress vs. shear rate curve – stress should not
decrease with increasing shear rate – this indicates sample
is leaving gap
ƒ Possible Solutions:
ƒ use a smaller gap or smaller angle so that you get the same
shear rate at a lower angular velocity
ƒ if appropriate (i.e. Polymer melts) make use of Cox Merz
Rule
*
η (γ ) ≡ η (ω )
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Hooke’s Law of Elasticity: Stress = Modulus ⋅ Strain
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γ1
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γ3
3
2
1
1
2
3
^ƚƌĂŝŶ;࠹Ϳ
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Hooke’s Law of Elasticity: Stress = Modulus ⋅ Strain
E
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γ1
E
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γ2
E
γ3
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Newton’s Law: stress
= coefficient of viscosity ⋅ shear rate
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Newton’s Law: stress= coefficient of viscosity ⋅ shear rate
Ș
<
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<
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Ʉൌ
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Ș
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Range of Material Behavior
Liquid Like---------- Solid Like
Ideal Fluid ----- Most Materials -----Ideal Solid
Purely Viscous ----- Viscoelastic ----- Purely Elastic
Viscoelasticity: Having both viscous
and elastic properties
ƒ
Materials behave in the linear manner, as described by Hooke and
Newton, only on a small scale in stress or deformation.
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ƒ Long deformation time: pitch behaves
like a highly viscous liquid
ƒ
9th drop fell July 2013
ƒ Short deformation time: pitch behaves
like a solid
Started in 1927 by Thomas Parnell in Queensland, Australia
ŚƚƚƉ͗ͬͬǁǁǁ͘ƚŚĞĂƚůĂŶƚŝĐ͘ĐŽŵͬƚĞĐŚŶŽůŽŐLJͬĂƌĐŚŝǀĞͬϮϬϭϯͬϬϳͬƚŚĞͲϯͲŵŽƐƚͲĞdžĐŝƚŝŶŐͲǁŽƌĚƐͲŝŶͲƐĐŝĞŶĐĞͲƌŝŐŚƚͲŶŽǁͲƚŚĞͲƉŝƚĐŚͲĚƌŽƉƉĞĚͬϮϳϳϵϭϵͬ
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T is short [< 1s]
T is long [24 hours]
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ƒ
ƒ
Silly Putties have different characteristic relaxation times
Dynamic (oscillatory) testing can measure time-dependent
viscoelastic properties more efficiently by varying frequency
(deformation time)
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ƒ Old Testament Prophetess who said (Judges 5:5):
"The Mountains ‘Flowed’ before the Lord"
ƒ Everything Flows if you wait long enough!
ƒ Deborah Number, De - The ratio of a characteristic
relaxation time of a material (τ) to a characteristic time of
the relevant deformation process (T).
Ğсτͬd
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ƒ
ƒ
ƒ
Hookean elastic solid - IJ is infinite
Newtonian Viscous Liquid - IJ is zero
Polymer melts processing - IJ may be a few seconds
High De
Low De
Solid-like behavior
Liquid-like behavior
IMPLICATION: Material can appear solid-like because
1) it has a very long characteristic relaxation time or
2) the relevant deformation process is very fast
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(E' or G')
(E" or G")
(E' or G')
(E" or G")
log Frequency
Temperature
log Time
log Time
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"If the deformation is small, or applied sufficiently slowly,
the molecular arrangements are never far from
equilibrium.
The mechanical response is then just a reflection of
dynamic processes at the molecular level which go on
constantly, even for a system at equilibrium.
This is the domain of LINEAR VISCOELASTICITY.
The magnitudes of stress and strain are related
linearly, and the behavior for any liquid is completely
described by a single function of time."
Mark, J., et. al., Physical Properties of Polymers, American Chemical Society, 1984, p. 102.
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Measuring linear viscoelastic properties helps us bridge the gap
between molecular structure and product performance
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ƒ Define Oscillation Testing
ƒ Approach to Oscillation Experimentation
ƒ Stress and Strain Sweep
ƒ Time Sweep
ƒ Frequency Sweep
ƒ Temperature Ramp
ƒ Temperature Sweep (TTS)
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Phase angle δ
Strain, ε
Stress, σΎ
Dynamic stress applied sinusoidally
User-defined Stress or Strain amplitude and frequency
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ƒ Time to complete one oscillation
ƒ Frequency is the inverse of time
ƒ Units
ƒ Angular Frequency = radians/second
ƒ Frequency = cycles/second (Hz)
ƒ Rheologist must think in terms of rad/s.
ƒ 1 Hz = 6.28 rad/s
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ω = 6.28 rad/s
ω = 12.560rad/s
0
0
dŝŵĞсϭƐĞĐ
0
0
ω = 50 rad/s
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ƒ Strain and stress are calculated from peak amplitude in the
displacement and torque waves, respectively.
0
0
0
0
dŝŵĞсϭƐĞĐ
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Deformation
ƒ An oscillatory (sinusoidal)
deformation (stress or strain)
is applied to a sample.
ƒ The material response
(strain or stress) is measured.
ƒ The phase angle δ, or phase
shift, between the deformation
and response is measured.
Response
Phase angle δ
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Purely Elastic Response
(Hookean Solid)
Purely Viscous Response
(Newtonian Liquid)
δ сϵϬ°
δ сϬ°
Strain
Strain
Stress
Stress
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Phase angle 0°< δ < 90°
Strain
Stress
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ƒ The stress in a dynamic experiment is referred to as the
complex stress σ*
ƒ The complex stress can be separated into two components:
1) An elastic stress in phase with the strain. σ' = σ*cosδ
δ
σ' is the degree to which material behaves like an elastic solid.
2) A viscous stress in phase with the strain rate. σ" = σ*sinδ
δ
σ" is the degree to which material behaves like an ideal liquid.
Phase angle δ
Complex Stress, σ*
σ* = σ' + iσ
σ"
Complex number: ‫ ݔ‬൅ ݅‫ ݕ‬ൌ
Strain, ε
‫ݔ‬ଶ ൅ ‫ݕ‬ଶ
The material functions can be described in
terms of complex variables having both real and
imaginary parts. Thus, using the relationship:
TAINSTRUMENTS.COM
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The Modulus: Measure of
materials overall resistance to
deformation.
The Elastic (Storage) Modulus:
Measure of elasticity of material.
The ability of the material to store
energy.
The Viscous (loss) Modulus:
The ability of the material to
dissipate energy. Energy lost as
heat.
Tan Delta:
Measure of material damping such as vibration or sound
damping.
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RUBBER BALL y
TENNIS
BALL
LOSS
(G”)
y
STORAGE
(G’)
G*
Dynamic measurement
represented as a vector
G"
Phase angle δ
G'
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ƒ The viscosity measured in an oscillatory experiment is a Complex
Viscosity much the way the modulus can be expressed as the
complex modulus. The complex viscosity contains an elastic
component and a term similar to the steady state viscosity.
ƒ The Complex viscosity is defined as:
Ș* = Ș’ + i Ș”
or
Ș* = G*/Ȧ
Note: frequency must be in rad/sec!
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Parameter
Shear
Elongation
Units
Strain
ɶ сɶϬƐŝŶ;ʘƚͿ
ɸ сɸϬ ƐŝŶ;ʘƚͿ
---
Stress
σ сσϬƐŝŶ;ʘƚнɷͿ
τ сτϬƐŝŶ;ʘƚнɷͿ
Pa
Storage Modulus
(Elasticity)
'͛с;σϬͬɶϬͿĐŽƐɷ
͛с;τϬͬɸϬͿĐŽƐɷ
Pa
Loss Modulus
(Viscous Nature)
'͟с;σϬͬɶϬͿƐŝŶɷ
͟с;τϬͬɸϬͿƐŝŶɷ
Pa
Tan į
'ͬ͟'͛
ͬ͛͟
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Complex Modulus
'Ύ с;'͛Ϯн'͟ϮͿϬ͘ϱ
Ύ с;͛Ϯн͟ϮͿϬ͘ϱ
Pa
Complex Viscosity
ηΎ с'Ύͬʘ
ηΎ сΎͬʘ
Pa·sec
Cox-Merz Rule for Linear Polymers: η*(Ȧ) = η(ߛሶ ) @ ߛሶ = Ȧ
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ƒ Define Oscillation Testing
ƒApproach to Oscillation Experimentation
1. Stress and Strain Sweep
2. Time Sweep
3. Frequency Sweep
4. Temperature Ramp
5. Temperature Sweep (TTS)
TAINSTRUMENTS.COM
Stress or strain
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Time
ƒ The material response to
increasing deformation
amplitude (strain or
stress) is monitored at a
constant frequency and
temperature.
ƒ Main use is to determine LVR
ƒ
All subsequent tests require an amplitude found in the LVR
ƒ Tests assumes sample is stable
ƒ If not stable use Time Sweep to determine stability
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Linear Region:
Modulus
independent
of strain
Non-linear Region:
Modulus is a function of strain
G'
Stress
Constant
Slope
γĐ сCritical Strain
Strain (amplitude)
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ƒ In general, the LVR is shortest when the sample is in its
most solid form.
G’
Solid
Liquid
% strain
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ƒ LVR decreases with increasing frequency
ƒ Modulus increases with increasing frequency
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Linear response to a sinusoidal excitation
is sinusoidal and represented by the
fundamental in the frequency domain
Nonlinear response to a sinusoidal
excitation is not sinusoidal and
represented in the frequency domain by
the fundamental and the harmonics
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γ(t) = γ0 sin(ωt)
τ(t) = τ0 sin(ωt+δ)
γ(t) = γ0 sin(ωt)
>K^
Fourier Series expansion:
τ(t) = τ1 sin(ω1t+ϕ1) + τ3 sin(3ω1t+ϕ3) +
τ5 sin(5ω1t+ϕ5) + ...
’
=
Σ τ sin(nω +ϕ )
n
n=1
odd
1
n
Lissajous plot: Stress vs. Strain (shown)
or stress vs. Shear rate
TAINSTRUMENTS.COM
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ƒ The material response
is monitored at a
constant frequency,
amplitude and
temperature.
Time
USES
ƒ Time dependent Thixotropy
ƒ Cure Studies
ƒ Stability against thermal degradation
ƒ Solvent evaporation/drying
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ƒ Important, but often overlooked
ƒVisually observe the sample
ƒ Determines if properties are changing over the time of
testing
ƒ Complex Fluids or Dispersions
ƒ
Preshear or effects of loading
ƒ
Drying or volatilization (use solvent trap)
ƒ
Thixotropic or Rheopectic
ƒ Polymers
ƒ
Degradation (inert purge)
ƒ
Crosslinking
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Under air
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Structural Recovery after Preshear
ϭϬϬ͘Ϭ
G' (Pa)
ϴϬ͘ϬϬ
ϲϬ͘ϬϬ
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ϭϳϱ͘Ϭ
ϮϬϬ͘Ϭ
ϮϮϱ͘Ϭ
time (s)
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Delay after pre-shear = 150 sec
Sample “A” time sweep
100.0
Delay after pre-shear = 0 sec
G' (Pa)
100.0
Pre-shear conditions:
100 1/s for 30 seconds
10.00
10.00
0
25.00
50.00
75.00
100.0
time (s)
125.0
150.0
175.0
0.1000
1.000
10.00
100.0
osc. stress (Pa)
ƒ End of LVR is indicative of “Yield” or “Strength of Structure”
ƒ Useful for Stability predictions (stability as defined by yield)
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Solvent trap cover picks up heat from Peltier Plate to insure uniform temperature
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TA Instruments
G'
1000000
1000000
5 min
100000
100000
G"
1000
10000
1000
Gel Point: G' = G"
t = 330 s
100.0
100.0
10.00
10.00
1.000
0
200.0
400.0
600.0
time (s)
800.0
1000
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G' (Pa)
10000
1.000
1200
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The material response to
increasing frequency (rate of
deformation) is monitored at
a constant amplitude (strain
or stress) and temperature.
dŝŵĞ
ƒ
Strain should be in LVR
ƒ
Sample should be stable
ƒ
Remember – Frequency is 1/time so low frequencies
will take a long time to collect data – i.e. 0.001Hz is
1000 sec (over 16 min)
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Terminal
Region
Rubbery
Plateau
Region
Transition
Region
Glassy Region
1
2
Storage Modulus (E' or G')
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log Frequency (rad/s or Hz)
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Frequency of modulus
crossover correlates
with Relaxation Time
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Flow instability
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LDPE Freq sweep 2mm gap – Cox Merz
LDPE shear rate 1mm gap
LDPE Shear rate 2 mm gap
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ƒ High and low rate (short and long time) properties
ƒ Viscosity Information - Zero Shear Viscosity, shear
thinning
ƒ Elasticity (reversible deformation) in materials
ƒ MW & MWD differences polymer melts and solutions
ƒ Finding yield in gelled dispersions
ƒ Can extend time or frequency range with TTS
η0 ≈ M
3.4
w
§ Mw ·
G'
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and J e =
≈ ¨¨
2
( G" ) © M z ¹
3.4
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ƒ DHR has a combined motor and transducer design.
ƒ In an DHR rheometer, the applied motor torque and
the measured amplitude are coupled.
ƒ The moment of inertia required to move the motor and
geometry (system inertia) is coupled with the angular
displacement measurements.
ƒ This means that BOTH the system inertia and the
sample contributes to the measured signal.
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ƒ What is Inertia?
ƒ Definition: That property of matter which manifests
itself as a resistance to any change in momentum of a
body
ƒ Instrument has inertia
ƒ Sample has inertia
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ƒ Inertia consideration
ƒ Viscosity limitations with frequency
ƒ Minimize inertia by using low mass geometries
ƒ Monitor inertia using Raw Phase in degree
ƒ When Raw Phase is greater than:
ƒ
150°° degrees for AR series
ƒ
175°° degrees for DHR series
ƒ
This indicates that the system inertia is dominating the
measurement signal. Data may not be valid
Raw Phase × Inertia Correction = delta
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Access to raw phase angle
only available with TA
Instruments Rheometers!
Waveforms at high frequencies
Inertial effects at
high frequencies
Negligible correction at low frequencies
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ƒ ARES-G2 has a separate motor and transducer
design.
ƒ In an ARES-G2, the motor applies the deformation
independent of the torque measurement on the transducer.
ƒ The moment of inertia required to move the motor is
decoupled from the torque measurements.
ƒ This means the motor inertia does not contribute to the test
results.
ƒ Benefits of ARES-G2:
ƒ System inertia free
ƒ Capable of running low viscosity samples up to high
frequency
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FRT
Deflection
Purest
Measurement !
Motor
Inertia
NOT Part of
Measurement
Motor torque and
sample torque are
separated.
FRT null Position
Torque to drive FRT
To maintain Zero
Position = Sample
Torque
Motor
Measured
Displacement
Target
Strain
Or
Speed
Torque to
drive motor
to desired displacement
TAINSTRUMENTS.COM
ƒ
A linear heating rate is
applied. The material
response is monitored at a
constant frequency and
constant amplitude of
deformation. Data is taken
at user defined time
intervals.
Temperature (°C)
'\QDPLF7HPSHUDWXUH5DPS
time between
data points
m = ramp rate
(°C/min)
Denotes Oscillatory
Measurement
time (min)
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ƒ A step and hold temperature
profile is applied. The
material response is
monitored at one, or over a
range of frequencies, at
constant amplitude of
deformation.
–
Soak
Time
Step Size
Oscillatory
Measurement
Time
No thermal lag
Soak
Time
Oscillatory
Measurement
Step Size
Time
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log E' (G') and E" (G")
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Terminal Region
Storage Modulus (E' or G')
Loss Modulus (E" or G")
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ƒ Solid in torsion rectangular
ƒ Look at Tg, secondary transitions and study structureproperty relationships of finished product.
ƒ Themosetting polymers
ƒ Follow curing reactions
ƒ Polymer melts and other liquids
ƒ Measure temperature dependence of viscoelastic
properties
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ƒ
It is important to setup normal force control during any temperature
change testing or curing testing
ƒ Some general suggestions for normal force control
ƒ For torsion testing, set normal force in tension: 1-2N ± 0.5-1.0N
ƒ For curing or any parallel plate testing, set normal force in
compression: 0 ± 0.5N
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ƒ Videos available at www.tainstruments.com under the Videos tab or on the TA
tech tip channel of YouTube™ (ŚƚƚƉƐ͗ͬͬǁǁǁ͘LJŽƵƚƵďĞ͘ĐŽŵͬƵƐĞƌͬddĞĐŚdŝƉƐ)
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ƒ Cures are perhaps the most challenging experiments to conduct on
rheometers as they challenge all instrument specifications both high
and low.
ƒ The change in modulus as a sample cures can be as large as 7-8
decades and change can occur very rapidly.
ƒ AR, DHR, and ARES instruments have ways of trying to cope with
such large swings in modulus
ƒ AR: Non-iterative sampling (w/ Axial force control)
ƒ DHR: Non-iterative sampling (w/ Axial force control) and
Auto-strain (w/ Axial force active) in TRIOS v3.2 or higher
ƒ ARES: Auto-strain (w/ Axial force or auto-tension active)
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At start of test have a material that starts as
liquid, paste, pressed power Pellet, or prepreg
Material fully cured
Maximum h or G’ reached
η
Žƌ
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Crosslinking
reaction causes
h and G’ to increase
dĞŵƉ
Material hits minimum viscosity which depends on
Max temperature, frequency, ramp rate and may depend
on strain or stress amplitude
As the temp increases
the viscosity of resin
decreases
Time
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ƒNon-Iterative Sampling – motor
torque is adjusted based on
previous stress value and predicts
new value required to obtain the
target strain (good for rapid
measurements)
ƒPrecision Sampling – motor torque
is adjusted at the end of an
oscillation cycle in order to reach
commanded strain
ƒContinuous Oscillation (direct
strain)* – motor torque is adjusted
during the oscillation cycle to apply
the commanded strain
*Continuous oscillation only available with DHR-2 and DHR-3
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Continuous oscillation (or direct strain control): incremental approach
controls the strain and hits the target during a single cycle
Non-iterative: uses the settings entered for the first data point and then uses
previous cycle
Precision: iterates using the initial settings entered for each data point
θ(t+1)1
θ(t)1
Μ(t+1)1
Μ(t)1
Point 1
or cycle
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η
Žƌ
'͛
Torque
Strain
Concern: How high does strain go at minimum
viscosity. Does higher strain inhibit the cure
(break structure that begins to form as material
crosslinks). Does this affect time to minimum
viscosity or gel time?
Temp
Time
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Torque
Upper torque limit
Strain
η
Žƌ
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Temp
Lower
torque limit
Time
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ƒ Strain
ƒ Depends on sample
ƒ Verify the LVR in the cured state ( e.g. 0.05%)
ƒ Normal force control or auto-tension
ƒ Requires active to adjust for sample shrinkage and/or thermal
expansion in parallel plates
ƒ Temperature
ƒ Isothermal
ƒ Fast ramp + isotherm: the fastest ramp rate
ƒ Continuous ramp rate: 3 – 5 °C/min.
ƒ Frequency
ƒ Typically 1Hz (6.28 rad/s), 10 rad/s or higher
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Strain is applied to sample instantaneously
(in principle) and held constant with time.
Stress is monitored as a function of time σ(t).
DHR and AR
ƒ
Response time dependent on feedback loop
Strain
ƒ
Ϭ
time
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time
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stress for
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Response of ViscoElastic Material
Stress decreases with time
starting at some high value
and decreasing to zero.
Ϭ
time
ƒ For small deformations (strains within the linear region)
the ratio of stress to strain is a function of time only.
ƒ This function is a material property known as the
STRESS RELAXATION MODULUS, G(t)
G(t) = σ(t)/γγ
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Glassy Region
Transition
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log time
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ƒ Research Approach, such as generation of a family of
curves for TTS, then the strain should be in the linear
viscoelastic region. The stress relaxation modulus will be
independent of applied strain (or will superimpose) in the
linear region.
ƒ Application Approach, mimic real application. Then the
question is "what is the range of strain that I can apply on
the sample?" This is found by knowing the Strain range
the geometry can apply.
ƒ The software will calculated this for you.
γ с<γ п θ ;йγ с γ п ϭϬϬͿ
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Stress Relaxation of PDMS, Overlay
105
G(t)
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50% strain
10% strain
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[Pa]
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103
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10
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10
1
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5.0
10.0
15.0
20.0
25.0
30.0
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Stress
ƒ Stress is applied to sample instantaneously, t1, and held
constant for a specific period of time. The strain is
monitored as a function of time (γ(t) or ε(t))
ƒ The stress is reduced to zero, t2, and the strain is
monitored as a function of time (γ(t) or ε(t))
ƒ Native mode on AR (<1 msec)
t1 time
t2
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t1 time
t2
Response of Classical Extremes
ƒ
ƒ
Stain for t>t1 is constant
Strain for t >t2 is 0
t1
time
t2
ƒ
ƒ
ƒ
Stain rate for t>t1 is constant
Strain for t>t1 increase with time
Strain rate for t >t2 is 0
t1
time t2
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log Creep Compliance, Jc
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Rubbery
Plateau
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Transition
Region
Glassy Region
Terminal Region
ůŽŐƚŝŵĞ
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Recovery σ = 0 (after steady state)
Creep σ > 0
σ/η
Less Elastic
More Elastic
Creep Zone
t1
Recovery Zone
t2
time
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more elastic
:;ƚͿ
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:ƌ;ƚͿ
ϭͬη
Je = Equilibrium recoverable compliance
Recovery Zone
time
time
Creep Compliance
– ൌ
Recoverable Compliance
ஓሺ୲ሻ
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The material property obtained from
Creep experiments:
Compliance = 1/Modulus (in a sense)
୰
Where
– ൌ
ɀ୳ െ ɀ –
ɐ
γu = Strain at unloading
γ(t) = time dependent
recoverable strain
Mark, J., et. al., Physical Properties of Polymers, American Chemical Society, 1984, p. 102.
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• The ringing oscillations can be rather short-lived and may not be apparent unless using log time scale.
• The sudden acceleration, together with the measurement system’s inertia, causes a strain overshoot. For
viscoelastic materials, this can result in viscoelastic ringing, where the material undergoes a damped
oscillation just like a bowl of Jell-o when bumped.
Creep ringing in rheometry or how to deal with oft-discarded data in step stress tests!
RH Ewoldt, GH McKinley - Rheol. Bull, 2007
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ƒ Stress is controlled by closing the loop around the sample Æ
requires optimization of control PID parameters
ƒ Pretest to determine material’s response and PID Constants
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Set up a pre-test and get the sample information into the loop
Stress Control Pre-test: frequency sweep within LVR
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Pretest Æ Frequency Sweep from 2 to 200 rad/s Æ data analyzed in
software to optimize Motor loop control PID constants
LDPE melt
Freq. Sweep
T = 190°C
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3.5000
HDPE Creep Recovery at 200°C
3.0000
% strain
2.5000
2.0000
1.5000
1.0000
0.50000
0
0
2000.000
4000.000
6000.000
time global (s)
8000.000
10000.000
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ƒ Research Approach - If you are doing creep on a polymer
ƒ
melt, and are interested in viscoelastic information (creep
and recoverable compliance), then you need to conduct the
test at a stress within the linear viscoelastic region of the
material.
Application Approach - If you are doing creep on a solid,
you want to know the dimension change with time under a
specified stress and temperature, then the questions is
"what is the max/min stress that I can apply to the
sample?". This is found by knowing the Stress range the
geometry can apply.
ƒ The software will calculated this for you.
σ = Kσ x Μ
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Three main reasons for rheological testing:
ƒ Characterization
MW, MWD, formulation, state of flocculation, etc.
ƒ Process performance
Extrusion, blow molding, pumping, leveling, etc.
ƒ Product performance
Strength, use temperature, dimensional stability, settling
stability, etc.
TAINSTRUMENTS.COM
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Molecular Structure
ƒ MW and MWD
ƒ Chain Branching and Cross-linking
ƒ Interaction of Fillers with Matrix Polymer
ƒ Single or Multi-Phase Structure
Viscoelastic Properties
As a function of:
ƒ Strain Rate(frequency)
ƒ Strain Amplitude
ƒ Temperature
Processability & Product Performance
TAINSTRUMENTS.COM
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Material
Composites, Thermosets
Cured Laminates
Property
Viscosity, Gelation, Rate of Cure, Effect of
Fillers and Additives
Glass Transition, Modulus Damping, impact
resistance, Creep, Stress Relaxation, Fiber
orientation, Thermal Stability
Thermoplastics
Blends, Processing effects, stability of
molded parts, chemical effects
Elastomers
Curing Characteristics, effect of fillers,
recovery after deformation
Coating, Adhesives
Damping, correlations, rate of degree of
cure, glass transition temperature, modulus
TAINSTRUMENTS.COM
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ƒ Oscillation/Dynamic
ƒ Time Sweep
ƒ
Degradation studies, stability for subsequent testing
ƒ Strain Sweep – Find LVER
ƒ Frequency Sweep – G’, G”, η*
ƒ
Sensitive to MW/MWD differences melt flow can not see
ƒ Temperature Ramp/Temperature Step
ƒ
Transitions, viscosity changes
ƒ TTS Studies
ƒ Flow/Steady Shear
ƒ Viscosity vs. Shear Rate Plots
ƒ Find Zero Shear Viscosity
ƒ Low shear information is sensitive to MW/MWD differences melt flow
can not see
ƒ Creep and Recovery
ƒ Creep Compliance/Recoverable Compliance
ƒ Very sensitive to long chain tails
TAINSTRUMENTS.COM
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Polyester Temperature stability
Modulus G' [Pa]
10
Temperature stability
good
poor
5
250
225
10
200
4
Temperature T [°C]
275
Determines if properties
are changing over the
time of testing
ƒ Degradation
ƒ Molecular weight
building
ƒ Crosslinking
175
-2
0
2
4
6
8
10
12
14
16
18
Time t [min]
Important, but often overlooked!
TAINSTRUMENTS.COM
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Power Law Region
First Newtonian Plateau
η0 = Zero Shear Viscosity
η0 = K x MW 3.4
log η
Extend Range
with TimeTemperature
Superposition (TTS)
& Cox-Merz
Measure in Flow Mode
Extend Range
with Oscillation
& Cox-Merz
Molecular Structure
1.00E-5
1.00E-4
1.00E-3
Compression Molding
0.0100
0.100
1.00
Extrusion
10.00
100.00
Second Newtonian
Plateau
Blow and Injection Molding
1000.00
1.00E4
1.00E5
shear rate (1/s)
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ƒ
ƒ
log ηo
ƒ
Sensitive to Molecular Weight, MW
For Low MW (no Entanglements) η0 is proportional to MW
For MW > Critical MWc, η0 is proportional to MW3.4
η0 с<⋅⋅Dǁ
3.4
MWc
log MW
η0 с<⋅⋅Dǁ ϯ͘ϰ
Ref. Graessley, Physical Properties of Polymers, ACS, c 1984.
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10
7
10
6
10
5
10
4
10
3
Zero Shear
Viscosity
10
5
100000
2
10
6
Slope 3.08 +/- 0.39
10
10
The high frequency
behavior
(slope -1) is
independent of the
molecular weight
SBR Mw [g/mol]
130 000
230 000
320 000
430 000
Zero Shear Viscosityηo [Pa s]
Viscosity η* [Pa s]
The zero shear viscosity increases with increasing molecular weight.
TTS is applied to obtain the extended frequency range.
Molecilar weight M w [Daltons]
-4
10
-3
10
-2
10
-1
10
0
10
1
10
2
10
3
10
4
10
5
Frequency ω aT [rad/s]
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A Polymer with a broad MWD exhibits non-Newtonian flow
at a lower rate of shear than a polymer with the same η0,
but has a narrow MWD.
Narrow MWD
Broad MWD
Log Shear Rate (1/s)
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Modulus G', G'' [Pa]
The G‘ and G‘‘ curves are shifted to lower frequency
with increasing molecular weight.
10
6
10
5
10
4
10
3
10
2
10
1
10
SBR M w [g/mol]
G' 130 000
G'' 130 000
G' 430 000
G'' 430 000
G' 230 000
G'' 230 000
-4
10
-3
10
-2
10
-1
10
0
10
1
10
2
10
3
10
4
10
5
Freq ω [rad/s]
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Modulus G', G'' [Pa]
10
5
10
ƒ
4
10
SBR polymer melt
G' 310 000 broad
G" 310 000 broad
G' 320 000 narrow
G" 320 000 narrow
3
10
-3
10
-2
10
-1
10
10
0
1
10
2
10
3
10
The maximum in G‘‘ is a good
indicator of the broadness of the
distribution
EĂƌƌŽǁ
4
10
ƌŽĂĚ
Frequency ωaT [rad/s]
Higher crossover frequency : lower Mw
Higher crossover Modulus: narrower MWD
(note also the slope of G” at low
frequencies – narrow MWD steeper slope)
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400,000 g/mol PS
400,000 g/mol PS
+ 1% 12,000,000 g/mol
Macosko, TA Instruments Users’ Meeting, 2015
400,000 g/mol PS
+ 4% 12,000,000 g/mol
TAINSTRUMENTS.COM
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ƒ
ƒ
Good thermal stability
ƒ one crossover point,
ƒ Ș* plateaus at low Ȧ
Poor thermal stability
ƒ multiple crossover points
ƒ Ș* continues to increase
over time
ƒ Time Sweep can verify if
the sample is unstable
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HDPE pipe surface defects
ƒ
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5
5
10
4
4
10
10
G' rough surface
G' smooth surface
η* rough surface
η* smooth surface
3
10
0.1
1
10
3
10
Complex viscosity η* [Pa s]
Modulus G' [Pa]
10
Surface roughness
correlates with G‘ or
elasticity → broader
MWD or tiny
amounts of a high
MW component
100
Frequency ω [rad/s]
Blue-labled sample shows a rough surface after extrusion
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Tack and Peel performance of a PSA
ƒ It can be related to
the viscoelastic
properties at
different
frequencies
good tack and peel
Bad tack and peel
Storage Modulus G' [Pa]
ƒ Bond strength is
obained from peel
(fast) and tack
(slow) tests
4
10
peel
3
10
tack
0.1
1
10
Frequency ω [rad/s]
Tack and peel have to be balanced for an ideal adhesive
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Compliance J(t) [1/Pa]
10
10
-1
-2
10
-3
10
-4
10
-5
0.1
-1
10
LDPE Melt
o
T=140 C
10 Pa
50 Pa
100 Pa
500 Pa
1000 Pa
5000 Pa
slope 1
-2
10
increasing
stress
-3
10
-4
10
Recoverable Compliance Jr(t) [1/Pa]
LDPE Melt creep recovery
ƒ Non linear effects
can be detected in
recovery before
they are seen in the
creep (viscosity
dominates)
-5
10
1
10
100
1000
Time t [s]
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Neat and Filled LDPE
10
7
10
6
10
5
10
4
10
3
o
Temperature 180 C
LDPE filled
LDPE neat
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The material has a yield, when rate and viscosity are
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ƒ Application to processing: many processing flows are
elongation flows - testing as close as possible to
processing conditions (spinning, coating, spraying)
ƒ Relation to material structure: non linear elongation
flow is more sensitive for some structure elements
than shear flows (branching, polymer architecture)
ƒ Testing of constitutive equations: elongation results in
addition to shear data provide a more general picture
for developing material equations
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ƒ Thermosetting polymers are perhaps the
most challenging samples to analyze on
rheometers as they challenge all instrument
specifications both high and low.
ƒ The change in modulus as a sample cures
can be as large as 7-8 decades and
change can occur very rapidly.
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ƒ Monitor the curing process
ƒViscosity change as function of time or temperature
ƒ Gel time or temperature
ƒ Test methods for monitoring curing
ƒTemperature ramp
ƒIsothermal time sweep
ƒCombination profile to mimic process
ƒ Analyze cured material’s mechanical properties (G’,
G”, tan δ , Tg etc.)
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Molecular weight Mw goes to infinity
ƒ
System loses solubility
ƒ
Zero shear viscosity goes to infinity
ƒ
Equilibrium Modulus is zero and starts to rise
to a finite number beyond the gel point
Note: For most applications, gel point can be
considered as when G’ = G” and tan δ = 1
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G'
1000000
5 min
100000
100000
G"
10000
1000
10000
1000
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t = 330 s
100.0
100.0
10.00
10.00
1.000
1.000
1200
0
200.0
400.0
600.0
time (s)
800.0
G'' (Pa)
G' (Pa)
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1000
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• The process of viscosity increasing takes place in two
stages: the gelation process (frequency independent) and
vitrification (related to the network Tg relative to cure
temperature and is frequency dependent).
• When you look at an isothermal cure at a constant
frequency the modulus crossover point has both the
information of gelation and vitrification.
ƒ To avoid this, run multiple isothermal runs at different
frequencies and plot the cross over in tan delta. This is the
frequency independent gel point.
‹
Alternatively, use a single mutliwave test
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140°C 135°C
120°C
125°C
G’ (MPa)
145°C
130°C
Tire Compound:
Effect of Curing Temperature
Time (min)
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Collimated light and mirror assembly insure uniform irradiance
Maximum intensity at plate 300 mW/cm2
Broad range spectrum with main peak at 365 nm
Cover with nitrogen purge ports
Optional disposable acrylic plates
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Glass transition
ƒ Secondary transitions
ƒ Crystallinity
ƒ Molecular weight/cross-linking
ƒ Phase separation (polymer blends, copolymers,...)
ƒ Composites
ƒ Aging (physical and chemical)
ƒ Curing of networks
ƒ Orientation
ƒ Effect of additives
ƒ
Reference: Turi, Edith, A, Thermal Characterization of Polymeric Materials, Second Edition, Volume I., Academic Press, Brooklyn, New
York, P. 489.
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G' Onset: Occurs at lowest temperature - Relates to
mechanical failure
G" Peak: Occurs at middle temperature - more closely
related to the physical property changes attributed to the
glass transition in plastics. It reflects molecular processes agrees with the idea of Tg as the temperature at the onset
of segmental motion.
tan δ Peak: Occurs at highest temperature - used
historically in literature - a good measure of the "leatherlike"
midpoint between the glassy and rubbery states - height
and shape change systematically with amorphous content.
Reference: Turi, Edith, A, Thermal Characterization of Polymeric Materials, Second Edition, Volume I., Academic Press, Brooklyn, New York, P. 980.
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ƒ
Allows samples to be
characterized while fully
immersed in a temperature
controlled fluid using Peltier
Concentric Cylinder Jacket
Track changes in mechanical
properties such as swelling or
plasticizing
Addition of Water
1.000E10
100.0
Isotherm with
water at 22 °C
90.0
Isotherm
with water
at 95 °C
1.000E9
80.0
70.0
1.000E8
Temperature
ramp to 95 °C
60.0
temperature (°C)
(Pa)
G’G'(Pa)
ƒ
1.000E7
50.0
40.0
1.000E6
30.0
1.000E5
0
10.0
20.0
30.0
time global (min)
40.0
50.0
20.0
60.0
time (min)
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ƒ Torsion and DMA geometries allow solid samples to be
characterized in a temperature controlled environment
–
DMA functionality is standard with ARES G2 and optional DHR
сϮ';ϭнʆͿ
Modulus: G’, G”, G*
Rectangular and
cylindrical torsion
ʆ ͗WŽŝƐƐŽŶ͛ƐƌĂƚŝŽ
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DMA 3-point bending and tension
(Cantilever not shown)
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Glass Transition - Cooperative motion among a large number of
chain segments, including those from neighboring polymer chains
Secondary Transitions
ƒ Local main-chain motion - intramolecular rotational motion of
main chain segments four to six atoms in length
ƒ Side group motion with some cooperative motion from the main
chain
ƒ Internal motion within a side group without interference from
side group
ƒ Motion of or within a small molecule or diluent dissolved in the
polymer (e.g. plasticizer)
Reference: Turi, Edith, A, Thermal Characterization of Polymeric Materials, Second Edition, Volume I.,
Academic Press, Brooklyn, New York, P. 487.
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log Modulus
Increasing
Crystallinity
Amorphous
Crystalline
Cross-linked
3 decade drop
in modulus at Tg
Increasing MW
Tm
Temperature
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ƒ Multiphase systems consisting of a dispersed phase
(solid, fluid, gas) in surrounding fluid phase
ƒExamples are:
ƒ Paints
ƒ Coatings
ƒ Inks
ƒ Personal Care Products
ƒ Cosmetics
ƒ Foods
ƒ Properties:
ƒ Yield Stress
ƒ Non-Newtonian
Viscous Behavior
ƒ Thixotropy
ƒ Elasticity
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log η
What shear rate?
8) Spraying and brushing
9) Rubbing
10) Milling pigments
11) High Speed coating
4) Chewing, swallowing
5) Dip coating
6) Mixing, stirring
7) Pipe flow
1) Sedimentation
2) Leveling, Sagging
3) Draining under gravity
4
5
6
1
1.00E-5
1.00E-4
3
2
1.00E-3
0.0100
0.100
8
7
1.00
10.00
9
10
100.00
1000.00
1.00E4
11
1.00E5
1.00E6
shear rate (1/s)
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This viscosity is often called
the Zero Shear Viscosity, η0,
or the Newtonian Viscosity
log η
First
Newtonian
Plateau
Second
Newtonian
Plateau
Power-Law
Shear Thinning
Possible
Increase in
Viscosity
σ ∝ ߛሶ m or, equivalently, η ∝ ߛሶ m-1
m is usually 0.15 to 0.6
log ߛሶ
Reference:Barnes, H.A., Hutton, J.F., and Walters, K., An Introduction to Rheology,
Elsevier Science B.V., 1989. ISBN 0-444-87469-0
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Brownian diffusion
randomizes
Shear field aligns
particles along
streamlines
ůŽŐ η
Shear thinning
Turbulent flow pushes
particles out of
alignment, destroying
order and causing
increase in viscosity
(shear thickening)
Shear thickening
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ƒLinear or Exponential speed profile after reaching ‘Closure Distance’
ƒNormal Force set not to exceed a certain value after reaching the user
defined ‘Closure Distance’
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G' (Pa)
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Lowering the gap can introduce shear, breaking down weakly structured samples
Reducing the gap closure speed can minimize this effect
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ƒ Monitor the viscosity signal during the pre-shear to
determine if the rate and duration are appropriate
ƒ If the viscosity is increasing during the pre-shear, the sample is
rebuilding. The pre-shear should be higher than the shear
introduced during loading to erase sample loading history
ƒ The viscosity should decrease and then level off
ƒ Typical Pre-Shear: 1- 100 sec-1, 30-60 seconds
ƒ Use an amplitude sweep to determine what strain to use
for time sweep
ƒ A high strain will break down the sample, and not allow rebuilding
ƒ A low strain will give a weak signal
ƒ Based on the Time Sweep, determine an appropriate
equilibration time for that sample
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The goal for pre-shear is to remove the sample history at loading
For high viscosity sample, use low rate (10 1/s) and long time (2 min.)
For low viscosity sample, use high rate (100 1/s) and short time (1 min.)
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1.
2.
3.
Three consecutive time sweeps:
ƒ Time sweep within LVR (check if loading destroyed structure)
ƒ Time sweep at large strain
ƒ Time sweep back to LVR (check structure rebuild)
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ƒStructured fluids exhibit yield-like behavior, changing from ‘solid-like’ to
readily flowing fluid when a critical stress is exceeded. Rheological
modifiers are often used to control the yield behavior of fluids.
ƒThere are multiple methods to measure Yield stress. The apparent
yield stress measured is not a single value, as it will vary depending
on experimental conditions.
Why modify the yield behavior?
ƒ
ƒ
ƒ
to avoid sedimentation and increase the shelf live
to reduce flow under gravity
to stabilize a fluid against vibration
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ƒ Stress is ramped linearly from 0 to a value above Yield Stress and the stress at
viscosity maximum can be recorded as Yield Stress
ƒ The measured yield value will depend on the rate at which the stress is increased.
The faster the rate of stress increase, the higher the measured yield value
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Yield Stress
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When the Yield Stress is small, a flow rate sweep from high
to low shear rate is preferred
ƒ Eliminates start-up effects for
more accurate measurements
slope: -0.995
ƒ Initial high shear rate acts as a
pre-shear, erasing loading effects
ƒ Steady State sensing allows the
sample time to rebuild
ƒ The plateau in shear stress is a
measure of the yield stress.
ƒ At the plateau, Viscosity vs.
Shear Rate will have a slope of -1
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ƒ
1000
Sun Block Lotion
Perform strain or stress
sweep in oscillation
ƒ
G' (Pa)
G’ curve. It is the critical
stress at which irreversible
Onset point
osc. stress: 1.477 Pa
G': 346.6 Pa
End condition: Finished normally
100.0
0.01000
Yield stress is the on set of
0.1000
1.000
osc. stress (Pa)
plastic deformation occurs.
10.00
Yield stress of a sun block lotion
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ƒ Low shear viscosity 10-3 to 1 s-1
ƒ leveling, sagging, sedimentation
ƒ Medium shear viscosity10-103 s-1
ƒ mixing, pumping and pouring
ƒ High shear viscosity 103 - 106 s-1
ƒ brushing, rolling spraying
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At Rest
4
10
Processing
Performance
3
10
MSV
LSV
HSV
2
Viscosity h [Pas]
10
Roling
Brushing
Spraying
1
10
0
10
Mixing
Pumping
Consistency
Appearence
Leveling
Sagging
Sedimentation
-1
10
-2
10
-3
10
0.1
1
10
100
shear rate
1000
10000
100000
g [1/s]
The two coatings show the same consistency after formulation,
but they exhibit very different application performance
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The thixotropy characterizes the time dependence of
reversible structure changes in complex fluids. The
control of thixotropy is important to control:
ƒ
process conditions for example to avoid structure build up in pipes
at low pumping rates i.e. rest periods, etc....
ƒ
sagging and leveling and the related gloss of paints and coatings,
etc..
Sag
Leveling
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Stress is ramped up linearly,
and then back down, over the
same duration
In a thixotropic material, there will be a hysterisis between the two curves
The further the up ramp and down ramp curves differ, the larger the area
between the curves, the higher the thixotropy of the material.
See also AAN 016 – Structured Fluids
TAINSTRUMENTS.COM
Structure build up
Pre-shear the sample
to break down
structure. Then
monitor the increase
of the modulus or
complex viscosity as
function of time.
Modulus G', G'' [Pa]; Viscosity η* [Pas]
6WUXFWXUH5HFRYHU\
η*
after preshear
G'
G''
2
10
G'oo
Frequency 1Hz
strain 2%
-1
preshear 10s at 60 s
G'o
0
20
40
60
80
100
120
time t min]
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ƒThe non-sagging formula (with additive) has both a shorter recovery
time and a higher final recovered viscosity (or storage modulus), and
the recovery parameter takes both of these into account to predict
significantly better sag resistance.
ƒThe ratio η(∞) /t, is the recovery parameter (a true thixotropic index),
and has been found to correlate well to thixotropy-related properties
such as sag resistance and air entrainment.
Rheology in coatings, principles and methods
RR Eley - Encyclopedia of Analytical Chemistry, 2000 - Wiley Online Library
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100.0
Paint A
10.00
viscosity (Pa.s)
Paint B
Paint C
1.000
0.1000
0.01000
Paint D
0.1000
1.000
shear rate (1/s)
10.00
100.0
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120.0
Thixotropy (Pa/s):
Paint A = 657.0
Paint B = 436.5
Paint C = 254.0
Paint D = 120.3
100.0
shear stress (Pa)
80.00
Paint A
60.00
Paint B
40.00
Paint C
20.00
Paint D
0
0
10.00
20.00
30.00
40.00
50.00
60.00
shear rate (1/s)
70.00
80.00
90.00
100.0
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Paint A
12.50
G' (Pa)
10.00
7.500
Paint B
5.000
2.500
Paint C
Paint D
0
0
100.0
200.0
300.0
400.0
500.0
time (s)
600.0
700.0
800.0
900.0
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Paint B
Paint C
Paint D
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Roll-ons: Rheology and end-use performance
viscosity
The viscosity has to be balanced to provide the correct viscosity at a
given shear rate
storage
application
shear rate
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use small particles to reduce sedimentation speed
ƒ
add rheological modifier like clay to stabilize the suspension
and keep the particles in suspension
x x x x x x
x
x
x
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The temperature
dependence of the
modulus governs the
behavior during the
application to the skin
x
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Cosmetic lotion
ƒ Many dispersion exhibit
solid like behavior at rest
3
10
1.5
1.0
2
0.5
10
0.0
complex viscosity
G'
G''
tan δ
1
10
tan δ
Modulus G', G'' [Pa]; Viscosity η* [Pa s]
2.0
ƒ The frequency
dependence and the
absolute value of tan δ
correlate with long time
stability
-0.5
-1.0
0.1
1
10
100
frequency ω [rad/s]
ƒ Note: strain amplitude has to be in the linear region
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ƒ Access to Getting Started
Guides also found through
the help menu.
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ƒFrom www.tainstruments.com click on Videos, Support or Training
ƒSelect Videos for TA Tech Tips, Webinars and Quick Start Courses
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Quickstart e-Training Courses
Strategies for Better Data - Rheology
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ƒ Check the online manuals and error help.
ƒ Contact the TA Instruments Hotline
ƒ Phone: 302-427-4070 M-F 8-4:30 EST
ƒ Select Thermal , Rheology or Microcalorimetry Support
ƒ Email: thermalsupport@tainstruments.com or
rheologysupport@tainstruments.com or
microcalorimetersupport@tainstruments.com
ƒ Call your local Technical or Service Representative
ƒ Call TA Instruments
ƒ Phone: 302-427-4000 M-F 8-4:30 EST
ƒ Check out our Website: www.tainstruments.com
ƒ For instructional videos go to: www.youtube.com/user/TATechTips
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Temperature
ƒ Linear viscoelastic properties are both time-dependent and
temperature-dependent
ƒ Some materials show a time dependence that is proportional to the
temperature dependence
ƒ Decreasing temperature has the same effect on viscoelastic
properties as increasing the frequency
ƒ For such materials, changes in temperature can be used to “re-scale”
time, and predict behavior over time scales not easily measured
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TTS can be used to extend the frequency beyond the
instrument’s range
Creep TTS or Stress Relaxation TTS can predict
behavior over longer times than can be practically
measured
Can be applied to amorphous, non modified polymers
Material must be thermo-rheological simple
ƒ
One in which all relaxations times shift with the same shift factor aT
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If crystallinity is present, especially if any melting
occurs in the temperature range of interest
The structure changes with temperature
ƒ
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ƒ
Cross linking, decomposition, etc.
Material is a block copolymer (TTS may work within a limited
temperature range)
Material is a composite of different polymers
Viscoelastic mechanisms other than configuration changes of the
polymer backbone
ƒ
e.g. side-group motions, especially near the Tg
ƒ
Dilute polymer solutions
ƒ
Dispersions (wide frequency range)
ƒ
Sol-gel transition
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ƒ Decide first on the Reference Temperature: T0. What is the
use temperature?
ƒ If you want to obtain information at higher frequencies or
shorter times, you will need to conduct frequency (stress
relaxation or creep) scans at temperatures lower than T0.
ƒ If you want to obtain information at lower frequencies or
longer times, you will need to test at temperatures higher
than T0.
ƒ Good idea to scan material over temperature range at
single frequency to get an idea of modulus-temperature
and transition behavior.
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Master Curves can be generated using shift factors
derived from the Williams, Landel, Ferry (WLF)
equation
log aT= -c1(T-T0)/c2+(T-T0)
ƒ
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ƒ
aT = temperature shift factor
T0 = reference temperature
c1 and c2 = constants from curve fitting
ƒ
Generally, c1=17.44 & c2=51.6 when T0 = Tg
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Sometimes you shouldn’t use the WLF equation (even if it
appears to work)
If T > Tg+100°C
If T < Tg and polymer is not elastomeric
If temperature range is small, then c1 & c2 cannot be calculated
precisely
In these cases, the Arrhenius form is usually better
ln aT = (Ea/R)(1/T-1/T0)
ƒ
ƒ
ƒ
ƒ
ƒ
ƒ
aT = temperature shift factor
Ea = Apparent activation energy
T0 = reference temperature
T = absolute temperature
R = gas constant
Ea = activation energy
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Polystryene
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1)
Ward, I.M. and Hadley, D.W., "Mechanical Properties of Solid Polymers",
Wiley, 1993, Chapter 6.
2)
Ferry, J.D., "Viscoelastic Properties of Polymers", Wiley, 1970, Chapter 11.
3)
Plazek, D.J., "Oh, Thermorheological Simplicity, wherefore art thou?"
Journal of Rheology, vol 40, 1996, p987.
4)
Lesueur, D., Gerard, J-F., Claudy, P., Letoffe, J-M. and Planche, D., "A
structure related model to describe asphalt linear viscoelasticity", Journal of
Rheology, vol 40, 1996, p813.
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Control variables:
ƒ Shear rate
ƒ Velocity
ƒ Torque
ƒ Shear stress
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Thixotropic loop be done by adding another ramp step
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Control variables:
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Steady state algorithm
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To minimize thermal
lag, the ramp rate
should be slow.
1-5°C/min.
Control variables:
ƒ Shear rate
ƒ Velocity
ƒ Torque
ƒ Shear stress
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Control variables:
ƒ Osc torque
ƒ Osc stress
ƒ Displacement
ƒ % strain
ƒ Strain
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the time sweep.
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Structure Recovery
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Strain control mode
ƒ
Stress control mode
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Fast data acquisition is used for monitoring fast changing
reactions such as UV initiated curing
ƒ The sampling rate for this mode is twice the functional oscillation
frequency up to 25Hz.
ƒ The fastest sampling rate is 50 points /sec.
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Control variables:
ƒ Osc torque
ƒ Osc stress
ƒ Displacement
ƒ % strain
ƒ Strain
ƒ
ƒ
ƒ
Common frequency range: 0.1 – 100 rad/s.
Low frequency takes long time
As long as in the LVR, the test frequency can be set either from
high to low, or low to high
ƒ The benefit doing the test from high to low
ƒ Being able to see the initial data points earlier
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Control variables:
ƒ Osc torque
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ƒ % strain
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The strain needs to be in the LVR
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To minimize thermal
lag, recommend
using slow ramp rate
e.g. 1-5°C/min.
ƒ
The strain needs
to be in the LVR
Control variables:
ƒ Osc torque
ƒ Osc stress
ƒ Displacement
ƒ % strain
ƒ Strain
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It is important to setup normal force control during any temperature
change testing or curing testing
ƒ Some general suggestions for normal force control
ƒ For torsion testing, set normal force in tension: 1-2N ± 0.5-1.0N
ƒ For curing or any parallel plate testing, set normal force in
compression: 0 ± 0.5N
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Control variables:
ƒ Shear rate
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Multiple rate can be done by adding more peak hold steps
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Control variables:
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ƒ Velocity
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ƒ Shear stress
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Or go through the template
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Control variables:
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Control variables:
ƒ Shear rate
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Steady state algorithm
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During the test, the dependent variable (speed in controlled stress mode or torque in
controlled shear rate mode) is monitored with time to determine when stability has
been reached.
An average value for the dependent variable is recorded over the Sample period.
When consecutive average values (Consecutive within tolerance) are within the
Percentage tolerance specified here, the data is accepted.
The software will also accept the point at the end of the Maximum point time, should
the data still not be at a steady state value.
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To minimize thermal
lag, the ramp rate
should be slow.
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Control variables:
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ƒ Velocity
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Variables:
Stress
Torque
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For running an unknown sample, it is recommended to sweep torque instead of
stress. Because stress is geometry dependent
ƒ The starting torque can be from the lowest of the instrument specification
ƒ The maximum torque is sample dependent. You can setup a high number and
manually stop the test when it gets outside the LVR.
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Control variables:
ƒ Osc torque
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For high viscosity sample, use low rate (10 1/s) and long time (2 min.)
For low viscosity sample, use high rate (100 1/s) and short time (1 min.)
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Control variables:
ƒ Osc torque
ƒ Osc stress
ƒ Displacement
ƒ % strain
ƒ Strain
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ƒ
ƒ
Common frequency range: 0.1 – 100 rad/s.
Low frequency takes long time
As long as in the LVR, the test frequency can be set either from
high to low, or low to high
ƒ The benefit doing the test from high to low
ƒ Being able to see the initial data points earlier
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ƒ % strain
ƒ Strain
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The strain needs to be in the LVR
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lag, recommend
using slow ramp rate
e.g. 1-5°C/min.
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The strain needs to be in the LVR
Control variables:
ƒ Osc torque
ƒ Osc stress
ƒ Displacement
ƒ % strain
ƒ Strain
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During a test
Before starting a test
ƒ
It is important to setup normal force control during any temperature
change testing or curing testing
ƒ Some general suggestions for normal force control
ƒ For torsion testing, set normal force in tension: 1-2N ± 0.5-1.0N
ƒ For curing or any parallel plate testing, set normal force in
compression: 0 ± 0.5N
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Default
values
shown
ƒ During the test, the angular velocity is monitored with time to
determine when stability has been reached.
ƒ An average value for the angular velocity is recorded over the
Sample period.
ƒ When consecutive average values (Consecutive within
tolerance) are within the tolerance specified here, the data is
accepted.
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Instrument Calibrations
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Inertia (Service)
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Oscillation Mapping (recommended for interfacial measurements)
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Geometry Calibrations:
ƒ
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Inertia
Friction
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ƒ Videos available at www.tainstruments.com under the Videos tab or on the TA tech
tip channel of YouTube™ (http://www.youtube.com/user/TATechTips)
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ƒ Instrument Calibrations
ƒ Temperature Offsets
ƒ Phase Angle (Service)
ƒ Measure Gap Temperature
Compensation
ƒ Transducer
ƒ Geometry Calibrations:
ƒ Compliance and Inertia (from table)
ƒ Gap Temperature Compensation
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ƒ Gap Temperature Compensation
ƒ Enter manually or run calibration
ƒ Compliance and Inertia
ƒ (from table in Help menu)
ƒ Geometry Constants
ƒ Calculated based on dimensions
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What if the online table does not list a compliance value for my specific geometry?
Use the compliance value for a geometry of the same/similar dimension, type, and
material.
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ƒ Air Supply
ƒ Dry particulate-free air (dew point -40 °C)
ƒ Check filters/regulators on a periodic basis to ensure proper
pressure, free of moisture/oil/dirt buildup.
ƒ If air must be turned off, then make sure that the bearing lock is
fastened
ƒ NOTE: Do not rotate drive-shaft if air supply is OFF!
ƒ Location
ƒ Isolate the instrument from vibrations with a marble table or
Sorbathane pads.
ƒ Drafts from fume hoods or HVAC systems and vibrations from
adjacent equipment can contribute noise to measurements,
particularly in the low torque regime. Use a Draft Shield to
isolate instrument from drafts.
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ƒ Circulator Maintenance
ƒ Proper operation of a fluid circulator is vital for correct
and efficient operation of Peltier-based temperature
control devices.
ƒ Check fluid levels and add anti-fungal additive regularly.
ƒ
Note: if operating circulator below 5°C then it is
recommended to fill the circulator with a mixture or
material with a lower freezing point than water to
prevent permanent circulator damage.
ƒ Example: add ~20% v/v ethanol to water
ƒ Keep it clean!
ƒ Flush and clean circulator, Peltier system, and tubing at
first sight of contamination.
ƒ When not in use, it is strongly recommended to
deactivate the Peltier device and turn off the circulator.
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Geometry
Diameter (mm)
8
20
Parallel Plate
and Cone and
Plate
25
40
60
Concentric
Cylinder
Conical Din Rotor
Recessed End
Double Wall
Pressure Cell
Standard Vane
Degree
Gap (micron)
0
0
0.5
1
2
4
0
0.5
1
2
4
0
0.5
1
2
4
0
0.5
1
2
4
0
0
0.5
1
2
4
1000
500
18
28
52
104
1000
18
28
52
104
1000
18
28
52
104
1000
18
28
52
104
1000
500
18
28
52
104
Sample
Volume (mL)
0.05
0.03
1.17E-03
2.34E-03
4.68E-03
9.37E-03
0.31
0.02
0.04
0.07
0.15
0.49
0.04
0.07
0.14
0.29
1.26
0.15
0.29
0.59
1.17
2.83
1.41
0.49
0.99
1.97
3.95
19.6
6.65
11.65
9.5
28.72
Max Shear Rate
(approx) 1/s
1.20E+03
Min Shear Rate
(approx) 1/s
4.00E-07
3.00E+03
3.44E+04
1.72E+04
8.60E+03
4.30E+03
3.75E+03
1.00E-06
1.15E-05
5.73E-06
2.87E-06
1.43E-06
1.25E-06
6.00E+03
3.44E+04
1.72E+04
8.60E+03
4.30E+03
9.00E+03
2.00E-06
1.15E-05
5.73E-06
2.87E-06
1.43E-06
3.00E-06
3.44E+04
1.72E+04
8.60E+03
4.30E+03
4.36E+03
4.36E+03
1.59E+04
1.15E-05
5.73E-06
2.87E-06
1.43E-06
1.45E-06
1.45E-06
5.31E-06
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ƒ Polymer samples come in different forms (e.g. powder, flakes,
pellets) and can be sensitive to environmental conditions
ƒ Careful sample preparation techniques are required to prepare
good test specimens for reproducible testing
ƒ Molding a sample
ƒ Handling powders, flakes
ƒ Controling the environment
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ƒ The best approach is to mold a sample plate (50x50 mm2 or 100x100 mm2)
ƒ Molding temperature: 10 - 20°C > than test temperature
ƒ Apply pressure: 8 – 12,000 lbs
ƒ Keep at elevated temperature long enough to let the sample relax
ƒ Cool down slowly under pressure to avoid orientations
ƒ Punch out a sample disk (8 or 25 mm)
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ƒ Before molding at high temperature, the sample has to be compacted
cold to reduce the volume
ƒ The compacted samples are transferred to the mold
ƒ Follow steps from the molding pellets procedure
ƒ Note: Sample may need to be stabilized or dried to avoid degradation
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ƒ Cut rectangular sheets of prepreg or adhesive (30x30mm)
ƒ Alternate direction of layer approx. 5 layer on top of each other
(remove release paper from PSA)
ƒ Compress the stack of sample layers in a press (4 – 5000 lbs)
ƒ Punch out 25 mm disks
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ƒ Polypropylene and Polyolefines in general tend
to degrade fast – need to be stabilized by
adding antioxidents
ƒ Moisture sensitive materials such as
polyamides and polyester require drying in
vacuum or at temperatures around 80°C.
ƒ Materials such as Polystyrene or Polymethylmethacrylate (PMMA) also absorb moisture. In
the melt phase, the gas separates into bubbles
and the sample foams
ƒ Pre-drying in vacuum is essential prior to
testing
Vacuum oven
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Geometry gap and Trim gap icons
Set Environmental
System to test
temperature
Load molded disk
onto lower plate
Close the oven and
bring the upper
plate to the trim
gap position
Monitor Axial or
Normal force
during this
period
After sample
relaxes, open the
oven and trim
excess sample
Close the oven and
adjust gap to
geometry/test gap
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Set Environmental
System to test
temperature
Mount melt ring
onto the lower plate
and load pellets
Bring the upper
plate close to top of
melt ring and close
the oven
After few minutes,
open the oven,
remove melt ring
and go to trim gap
After sample
relaxes, open the
oven and trim
excess sample
Close the oven and
adjust gap to
geometry/test gap
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ƒ Structured fluids can range in consistency from low viscosity (e.g. milk)
to high viscosity, pasty materials (e.g. tooth paste)
ƒ Structured materials are very sensitive to mechnical and
environmental conditions
ƒ Be aware of largest particle size in sample and choose the geometry
appropriately (cone vs parallel plate vs vane geometry)
ƒ Samples can also be time dependent – how you treat the sample
(handling, loading, pre-conditioning) may affect test results!
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ƒ Fluid samples which pour freely are relatively easy to handle prior to loading
ƒ Keep the container closed to avoid evaporation of solvent or continuous phase
ƒ Shake or stir sample to remove concentration gradients in suspensions
ƒ Adequate shelf temperature may be necessary to avoid phase separation in
emulsions
ƒ Never return used sample into original flask to avoid contamination
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ƒ Deposit fluid in the middle of the plate
ƒ Set a motor velocity of ~ 1 rad/s and move to geometry gap
ƒ Add additional material along the sides of the geometry – capillary forces will
draw the sample between the gap
ƒ When finished, click on the “Stop Motor” button
ƒ NOTE: If the sample is a structured fluid, setting a motor velocity will introduce
shear history onto the sample and can destroy the sample structure!
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ƒ The structure of high viscosity pastes and slurries may change with time
ƒ Food samples, like dough, can change continuously
ƒ The test samples need to be prepared carefully and consistently for
each experiment to obtain reproducibility
ƒ Slurries that may settle can gradually build a cake – these samples
have to be tested before sedimentation
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ƒ
ƒ
ƒ
ƒ
Scoop up the paste with a spatula and deposit it at the center of the lower plate
For less viscous materials, a syringe with a cut-off tip can be used
Load ~ 10-20 excess material to ensure complete sample filling
Set the gap to the trim gap and use exponential gap closure profile to minimize
shear in the sample
ƒ Lock the bearing, trim excess material and set final gap
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ƒ Gels, especially chemical gels, may change irreversibly when large deformations
are applied (for example, while loading)
ƒ Prepare (formulate) the sample in the final shape required for the measurement
so it can be loaded without deforming (cut, punch, …)
ƒ Alternatively, prepare the sample in situ – on the rheometer Æ systemic rheology
ƒ Take care to avoid introducing air bubbles!
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