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© 2011, University of Delaware, all rights reserved
MOTIVATION SPLIT HOPKINSON PRESSURE BAR RESISTANCE-BASED DAMAGE SENSING
Resistance-Based Sensing in Carbon Nanotube Composites Under Dynamic Loads
A. S. Wu, Q. An (PhDMSEG), T-W. Chou and E. T. Thostenson
University of Delaware . Center for Composite Materials . Department of Mechanical Engineering
t Failure prediction in advanced materials is critical to their success in high-performance applications. • In FRPs, the onset of failure due to matrix cracking and
interphase debonding often occurs without a significant decrease in load-carrying capability.
t Nondestructive damage sensing approaches: • off-line (e.g., ultrasonic C-scanning, X-ray microtomography
and liquid penetrant)
• real-time (e.g., time-domain reflectometry, acoustic emission and electrical resistance measurements)
t Resistance-based sensing allows for both off-line and real-time health monitoring.
Conductively modified carbon nanotube-based composites and their electrical response to dynamic loading is the focus of this research.
CURRENT RESEARCH CONCLUSIONS
ACKNOWLEDGEMENTS U.S. Army Research Office
Grant No. W911NF-09-1-0114 Dr. Bruce LaMattina
U.S. Office of Naval Research Grant No. N00014-09-1-0365
Dr. Yapa Rajapakse
Specimen (SP)
LSB
LIB LTB
LSG-1 LSG-2
HS
Incident Bar (IB)
Transmission Bar (TB)
Striker Bar (SB)Strain Gage (SG-1) Strain Gage (SG-2)
t Consists of a striker bar (SB), incident bar (IB) and transmission bar (TB)
t A gas gun propels the striker bar, which impacts the incident bar. • This results in a stress wave to propagate through the
incident bar (σI) to the bar-specimen interface. • The degree of acoustic impedance mismatch and the
specimen geometry control the amount of stress reflected back through the incident bar (σR) and transmitted through the transmission bar (σT).
t Measures the mechanical response of a specimen to dynamic compression loading.
t Preform: twenty plies of plain woven E-glass fabric • Fabric is treated with a carbon nanotube-based sizing agent
then infused with SC-15 epoxy resin.
t Carbon nanotubes are deposited at the fiber surface resulting in electrical percolation in a composite specimen. • The resistance of this nanotube
network is particularly sensitive to interphase debonding and delamination.
t Panel is cut to yield 45º off-axis specimens
0.00 0.02 0.04 0.06 0.08 0.10 0.120
20
40
60
80
100
120
140
160
(7)
(6)
(5)(4)(3)
(2)
σ (MPa)
ε
εmax
(s -‐1)
(1) 618(2) 572(3) 851(4) 1000(5) 1260(6) 1130(7) 1202
.
(1)
RESULTS
11 12 13 14 150
5
10
15
20
25
30
7
6
53,4
ΔR (kΩ
)
VE (m/s )
1,2
t Single specimen impacted multiple times at increasing energy • Stiffness decreases after each impact. • Anomaly in stress response due to large
delamination during impact (6)
t Permanent resistance changes after each loading indicates damage.
t Record resistance on the experimental timescale (~300 µs) • Stress and resistance are plotted vs. time below:
t Resistance increases during compression due to radial electrode configuration • Specimens undergo axial compression and radial
tension (Poisson’s effect).
100 200 300 4000
10
20
30
σ (MPa)
t (µs )
σ
loading
unloading
4
5
6
7
8
9
10
11
R
R (k
Ω)
t Achieved electrical percolation in a thick section composite using a carbon nanotube-based fiber sizing agent.
t Demonstrated effectiveness of the carbon nanotube network in sensing damage during dynamic compressive loading.
Lim, An, Chou and Thostenson (2010) Mechanical and electrical response of carbon nanotube-based fabric composites to Hopkinson bar loading. Composites Science and Technology 71:616-621
DAMAGE BEHAVIOR t Delamination occurs in these 45º off-axis
specimens. t Future work includes:
• Exploring electrode configurations which are more sensitive to this mode of failure and
• Measuring the resistance response to dynamic compression-induced shear failure