Upload
erikgherbert
View
2.675
Download
1
Embed Size (px)
DESCRIPTION
Nanoindentation, flat punch tip geometry, complex modulus, creep compliance
Citation preview
Measuring the constitutive behavior of viscoelastic
solids in the time and frequency domain using flat
punch nanoindentationpunch nanoindentation
E. G. Herbert, W. C. Oliver, A. L. Lumsdaine
Agilent Technologies, Oak Ridge, TN
G. M. PharrUniversity of Tennessee, Knoxville;
Materials Science and Technology Division,Oak Ridge National Laboratory, Oak Ridge, TN
NANOINDENTATION: A CLASSIC APPLICATION
MOTIVATION
What we’re after:– Constitutive behavior of small volumes of viscoelastic solids subjected time varying excitation over as wide a range of time or frequency as possible.
Extend the applicability of nanoindentation totime‐dependent behaviorp– Flat punch indentation, complex test geometry– DMA, triple clamp fixture, complex test geometry– Uniaxial compression simple test geometryUniaxial compression, simple test geometry
• Material’s response in the frequency domain ‐ short time
• Material’s response in the time domain ‐ long time
• Bringing them together
• Do it all with flat punch indentation
• Material selection: Highly plasticized PVC
NANOINDENTATION & DMA COMPARISON
PDMS, Tg ~ 120oC
C. C. White et al., Mater. R S S P 841Res. Soc. Symp. Proc. 841(2005)
MODELING THE INSTRUMENTATION
i d d i l i• Measure time‐dependent material properties
• Then we need to understand the time‐dependent
properties of the measurement tool
MODELING THE INSTRUMENTATION
FREE SPACENano Indenter® XP:
ti &&&Raw displacement, ± 1 mm
KhhChmeF tio ++=ω
( )φω −= tioehth )(2cos ωφ m
hF
K oS +=
( )( ) 1212222
−
⎥⎦⎤
⎢⎣⎡ +−= CmK
Fh
o
o ωω
Cωφsino
hF
C =
ho
2tanω
ωφmK
C−
=ωoh
MODELING THE INSTRUMENTATION
1 degree off d Z
Nano Indenter® XP:FREE SPACE
freedom, Z
ti &&&Raw displacement, ± 1 mm
KhhChmeF tio ++=ω
( )φω −= tioehth )(2cos ωφ m
hF
K oS +=
( )( ) 1212222
−
⎥⎦⎤
⎢⎣⎡ +−= CmK
Fh
o
o ωω
Cωφsino
hF
C =
ho
2tanω
ωφmK
C−
=ωoh
MODELING THE INSTRUMENTATION
1 degree off d Z
Nano Indenter® XP:FREE SPACE
freedom, Z
ti &&&Raw displacement, ± 1 mm
KhhChmeF tio ++=ω
( )φω −= tioehth )(2cos ωφ m
hF
K oS +=
( )( ) 1212222
−
⎥⎦⎤
⎢⎣⎡ +−= CmK
Fh
o
o ωω
C
FUNCTION OFPOSITION
ωφsino
hF
C =
ho
2tanω
ωφmK
C−
=ωoh
Measured stiffness and dampingin free space position = 18 8 μm
0
200 1000in free space, position = 18.8 μm
N/m
) Dam
400
-200
0
600
800Measured stiffnessModel
cos φ
(
mping, Fφω cos2 os h
FmK =− FREE SPACE
-600
-400
400Measured dampingF o /
h o c
Fo / h
o sioh
φω sino
o
hF
C =
-1000
-800200
Measured dampingModel
ffnes
s, in φ
(N/
-12000
1 10
Stif /m
)
Frequency (Hz)Frequency (Hz)
Measured stiffness and dampingin free space position = 18 8 μm
0
200 1000in free space, position = 18.8 μm
N/m
) Dam
400
-200
0
600
800Measured stiffnessModel
cos φ
(
mping, Fφω cos2 os h
FmK =− FREE SPACE
-600
-400
400Measured dampingF o /
h o c
Fo / h
o sioh
φω sino
o
hF
C =
-1000
-800200
Measured dampingModel
ffnes
s, in φ
(N/
-12000
1 10
Stif /m
)
Frequency (Hz)
m = 12.15 gKs = 95.4 N/mC = 2.81 Ns/mFrequency (Hz) /
ADD THE CONTACT
COUPLED2cos ωφ m
hF
S o +=ho
ωφsin
o
o
hF
C =
COUPLED RESPONSE = SAMPLE + INSTRUMENT
⎥⎥⎦
⎤
⎢⎢⎣
⎡+−
⎥⎥⎦
⎤
⎢⎢⎣
⎡+=
space) (free inst.
2
coupled
2contact coscos ωφωφ m
hF
mhF
Ko
o
o
o
PHASOR DIAGRAM: PHYSICAL INSIGHT
FREE SPACEDamped, forced oscillator
, N/m
)ng
, Cω
,(d
ampi
φω sinoFC =
ary
axis
o
o
hF
φω sinoh
C =
φω cos2 os
FmK =−
mag
ina
Real axis (stiffness K mω2 N/m)
φ
φo
s h
Im Real axis (stiffness, Ks-mω , N/m)
PHASOR DIAGRAM: PHYSICAL INSIGHT
Damped, forced oscillator
, N/m
)
FREE SPACE
ng, C
ω,
(dam
pi
φω sinoFC = COUPLED
ary
axis
o
o
hF
φω sinoh
C = COUPLED
φω cos2 os
FmK =−
mag
ina
Real axis (stiffness K mω2 N/m)
φ
φo
s h
Im Real axis (stiffness, Ks-mω , N/m)
PHASOR DIAGRAM: PHYSICAL INSIGHT
FREE SPACEDamped, forced oscillator
ω, N
/m)
ng, C
eqω
o
o
hF
φω sinoFC = COUPLED(d
ampi
n
φω sino
eq hC =
φω cos2 oeq
FmK =−
COUPLED
ry a
xis
(
φo
eq h
mag
inar
Real axis (stiffness K mω2 N/m)
φ
Im Real axis (stiffness, Keq
-mω , N/m)
PHASOR DIAGRAM: PHYSICAL INSIGHT
Depends on sample properties and the
Damped, forced oscillator
ω, N
/m)
FREE SPACE
p p p pgeometry of the contact
ng, C
eqω
o
o
hF
COUPLEDφω sinoFC =(d
ampi
n
COUPLEDCOUPLEDφω sino
eq hC =
φω cos2 oeq
FmK =−ry
axi
s ( COUPLED
φo
eq h
mag
inar
Real axis (stiffness K mω2 N/m)
φ
Im Real axis (stiffness, Keq
-mω , N/m)
FROM S AND Cω→ E’ AND E”
Phasor diagram of a linearviscoelastic solid
ss, P
a)
22* EEE ′′+′=
Phasor diagram of experimental measurements
ω, N
/m)
SAMPLE RESPONSE
cous
str
es
oEσ*
EEE +=
EiEE ′′+′=*
mpi
ng, C
ω
o
hF
F
SAMPLE RESPONSE
y ax
is (v
is
o
oEε
=
φεσ sin
o
oE =′′
y ax
is (d
am ohφω sin
o
o
hFC =
Imag
inar
yR l i ( l ti t P )
φφ
εσ cos
o
oE =′
Imag
inar
y
R l i ( tiff S N/ )
φφcos
o
o
hFS =
Real axis (elastic stress, Pa)Real axis (stiffness, S, N/m)
The fundamental equation of nanoindentation:
1π S 1 ωπ C)1(12
2νβ
π−=′
ASE )1(1
22νω
βπ
−=′′A
CE
DMA VS. NANOINDENTATION
Highly plasticized polyvinylchloride,the complex modulus at 22 oC
0.91
DMANanoindentation
10DMANanoindentationM
Pa)
0.50.60.70.80.9
Fact
or (-
)
6789
odul
us (M punch diameter = 100 μm
0.3
0.4
Loss
F4
5
6
tora
ge M
o
0.21 10
Frequency (Hz)
31 10
St
Frequency (Hz) q y ( )q y ( )
NEXT STEPS
• Do a better job comparing flat punch experiments to tests with simpler geometrywith simpler geometry.
• Study creep compliance with a flat punch.
• Combine frequency specific results with creep compliance.
COMPRESSION SAMPLES
COMPRESSION & INDENTATION
910
i i l i
)(cos factorgeometryhF
Eo
o φ=′
)(i f ttF
E o′′
789 uniaxial compression
1 mm dia. flat punch100 μm dia. flat punch
a)
)(sin factorgeometryhF
Eo
o φ=′′
5
6E'
(MPa
Geometry factors:
3
4
E
Compression:AL
FREQUENCY DOMAIN3
0.01 0.1 1 10 100Indentation: )1(11
22υ
βπ
−A
Frequency (Hz)
1uniaxial compression
)(cos factorgeometryhF
Eo
o φ=′
)(i f ttF
E o′′ uniaxial compression1 mm dia. flat punch100 μm dia. flat punch
r (-)
)(sin factorgeometryhF
Eo
o φ=′′
0 1Fact
orGeometry factors: 0.1
Loss
Compression:AL
FREQUENCY DOMAIN
0.01 0.1 1 10 100Indentation: )1(11
22υ
βπ
−A
Frequency (Hz)
205
79.6
80m
N)
Displace
transient response
Indentation:
PH =ασ hαε
Compression:
P=σ LΔ
=ε
195
200
78 4
78.8
79.2
On
Sam
ple
(m
ement Into S6 mN step load
transient response
AH =ασ
Dαε
A=σ
L=ε
LPLAtD Δ
=)()1(
)(2)( 2ν−=
PtRhtJc
10-6
190
195
77.6
78
78.4
2300 2400 2500 2600 2700 28002900
Load
O
urface (μm)
J (t), flat punch indentation2 /N)
Time On Sample (s)
10-7 c( ), p
(diameter = 983 μm)
D(t), uniaxial compression
D(t)
(m2
o
ttDσε )()( =
8
TIME DOMAIN
10-8
10-3 10-2 10-1 100 101 102 103
Creep Time (s)
TRANSFORMING FROM FREQUENCY TO TIME
4 term Prony series:
EJ′
′
FREQUENCY DOMAIN:
22 EEJ
′′+′=′
∑+=′4
220iJJJ ∑
= +1220 1i i ωτ
TIME DOMAIN:
t
∑=
−
−+=4
10 )1()(
i
t
iieJjtD τ
)(cos factorgeometryhF
Eo
o φ=′4
6
0.05 Hz Oscillation1 mm Dia. Flat Punch ho
)(sin factorgeometryhF
Eo
o φ=′′
-2
0
2
Load
(mN
)
3x10-7
5x10-7
FREQUENCY DOMAIN-6
-4
-1800 -1200 -600 0 600 1200 1800
L
3x102 /N
)22 EE
EJ′′+′
′=′
1800 1200 600 0 600 1200 1800Displacement (nm)
2x10‐7
88x10-81x10-7
uniaxial compression
1 mm dia. mm flat punchJ' (m
2EE +
Geometry factors:
4x10-8
6x10-8Compression:
AL
0.01 0.1 1 10 100Frequency (Hz)
Indentation: )1(112
2υβ
π−
A
J’ (FREQ. DOMAIN) FIT TO PRONY SERIES
3.2x10-7fit parameters:
= 7 5198E 03
FLAT PUNCH INDENTATION
E ′′
FREQ. DOMAIN:
2.4x10-7
2.8x10-7
N)
fit parameters:J
0 = 3.6960E-08
J 8 2830E 08
τ1
= 7.5198E-03
τ2 = 3.8620E+00
τ3 = 4.1034E-02
τ4 = 2.9883E-01
22 EEEJ
′′+′=′
∑+=′4
iJJJ
1.6x10-7
2x10-7
J' (m
2 /N J1 = 8.2830E-08
J2 = 4.6922E-08
J3 = 8.8235E-08
J4 = 7.5425E-08
4 ∑= +
+=1
220 1i i
JJωτ
8x10-8
1.2x10-7
nanoindentation data4 term parametric modelc r e fit
J 4 TIME DOMAIN:
∑=
−
−+=4
10 )1()(
i
t
iieJjtD τ
4x10-8
10-2 10-1 100 101 102 103
curve fit
ω (rad/s)ω (rad/s)
MAXIMIZING THE TIME AND FREQUENCY RANGE
3x10-7
5x10-7
D(t), uniaxial compression,measured in the time Combining indentation
3x10
2 /N)
measured in the timedomain
s 10H0101.0
=s002.01.0=
data acquired in the
frequency and time
domain allows the PVC
8x10-81x10-7
D(t)
(m2 Hz01.0s002.0
Hz 50reference material to be
characterized over nearly
6 decades in time (2x10‐3
4x10-8
6x10-8
D Predicted from flat punchnanoindentation dataacquired in the frequencydomain, 0.01 < f < 50 Hz
to 6x102).
10-5 10-4 10-3 10-2 10-1 100 101 102 103
Creep Time (s)p ( )
CONCLUSIONS
* Dynamic nanoindentation of viscoelastic solids requires robust dynamic characterization of the measurement tool itself, a known contact geometry, steady‐state harmonic motion, and linear viscoelasticity.
* In the frequency domain Sneddon’s stiffness equation works* In the frequency domain, Sneddon s stiffness equation works remarkably well.
* The Prony series model provides a valid path to transition between the y p pfrequency and time domains.
* It is possible to combine frequency and time domain data from a flat f ’punch indentation experiment and therefore characterize the sample’s
behavior over the widest possible range of time and frequency.
GEOMETRY OF THE CONTACT
Advantages:– Known contact area
Circular flat punch:
Known contact area– Area not affected by creep or
thermal drift
Disadvantages:Disadvantages:
– Full contact
– Stress concentration
Any tip geometry, consider:
– Steady‐state harmonic motion
– Linear viscoelasticityLinear viscoelasticity
• Compression distance
• Oscillation amplitude
3Pre-Compression Dependence
33 μm5 μm10 μm1M
Pa)
punch dia. = 103 µm
101
15 μm20 μm
ulus
(M
Loss FStorage
ho = 50 nm
0.6
0.8
e M
odu Factor
0.4AVG LF (-)AVG LF (-)AVG LF (-)AVG LF ( )St
orag
e (-)
Loss factor
1 0.21 10
AVG LF (-)S
F (H )Frequency (Hz)
3Amplitude Independence
3
50 nm100 nm500 nmM
Pa) punch dia. = 103 µm
101
500 nm1500 nm3000 nm
ulus
(M
Loss FStorage
comp. dist. = 3 µm
0.6
0.8
e M
odu Factor
p µ
0.4AVG LF (-)AVG LF (-)AVG LF (-)AVG LF (-)St
orag
e (-)
Loss factor
1 0.21 10
AVG LF (-)S
F (H )Frequency (Hz)
22 C, 1 mm dia. punch15 C, 100 μm dia. punch
100 10 C, 100 μm dia. punch5 C, 100 μm dia. punch
Pa)
E' (M
P
10
1 10Frequency (Hz)
22 C, 1 mm dia. punch15 C 100 μm dia punch
10015 C, 100 μm dia. punch10 C, 100 μm dia. punch5 C, 100 μm dia. punch
Pa)
Shift factors:
E' (M
P 5 to 22: 20010 to 22: 140
15 to 22: 8
10
1 10 100 1000 104 105
ω*At (rad/s)
1000loss factor
100
1
a)
Loss
loss factor
storage modulus
E' (M
Pa
s Factor 10
0 1
(-)Freq range: 1 to 10 kHz
0.110 100 1000 104 105
ω (At) (rad/s)
THANKS EVERYONE!