Results
(a) (b)
(c) (d)
• In the 3-point bend test, as the displacement
increased, the load on the specimens also increased.
• When the cracks were initiated, the slope of the
curves decreased.
• The highest load at which the specimens fully
fractured was the critical force.
• Mode I fracture toughness KIc was calculated
according to the ASTM E399 standard:
𝐾𝐼𝑐 =
𝑐𝑟𝑖𝑡𝑖𝑐𝑎𝑙 𝑓𝑜𝑟𝑐𝑒 ∗ 𝑠𝑝𝑎𝑛 ∗𝑓(
𝑎
𝑊
)
𝑏𝑊1.5
f(
𝑎
𝑊
) =
3
𝑎
𝑊
(1.99−
𝑎
𝑊
(2.15−3.93
𝑎
𝑊
+2.7 (
𝑎
𝑊
)2)
2(1+2
𝑎
𝑊
)(1−
𝑎
𝑊
)2
where a is the notch length, b is the breadth, and W
stands for the height of the specimen.
• The fracture toughness of all specimens was in the
range of about 1.5 to 2.5 MPa m.
• Fracture toughness increased as the weight
percentage increased from 10% to 20%, and then
reduced as the weight percent kept increasing.
• Fracture paths were revealed by micro X-ray
computed tomography (micro-CT) images.
• The specimens were numerically rendered as
transparent to reveal the crack.
• The cracks (gold) occurred in front of the notch
(purple) and went into the specimens.
• Several smaller micro-cracks coalesced into
bigger cracks and propagated away from the
notch (Figure 7(a)).
• They went through the alumina particles and
the epoxy matrix and sometimes along the
matrix-particle interfaces (Figure 7(b-d)).
• The deflection of the crack path is also observed
in some slices (Figure 7(c)).
Figure 5. Typical Load-Displacement Curves of 3-point Bend Test for
Specimens with Different Weight Fractions
Figure 6. 𝐊 𝐈𝐜 v.s. Weight Percentage/Volume Percentage of the Particles
Figure 7. (a) 3-D Reconstruction of Fracture Paths and (b) to (d)
Representative slices of Micro-CT Images
Fracture Toughness of Particulate Polymer-ceramic Composites
• Composite materials are widely used in various fields for
their high strength- and stiffness-to-weight ratios.
• Understanding the mechanical behaviors of composites is
important to advance the design of these materials.
• This study focuses on the fracture toughness (KIc) of
polymer-ceramic composite materials.
Introduction
Authors: Ruyi Man1
, Jiacheng Gao1
, Abhinit Kothari1
, Kangning Su1
Supervisors: Jing Du1
, Michael Hillman2
1 Department of Mechanical and Nuclear Engineering, Pennsylvania State University
2 Department of Civil and Environmental Engineering, Pennsylvania State University
Acknowledgments
• David and Shirley Wormley Excellence Fund for the Support
of World Class Engineers;
• Student Research and Engagement Office, Penn State College
of Engineering;
• National Science Foundation Award #1826221.
Future Works
• Specimens with other filler fractions will be made and
tested to further explore the relationship between the
fracture toughness and filler fractions.
• Specimens with different filler sizes will also be made and
tested to explore the effects of filler size on the fracture
toughness.
• In situ 3-point bend coupled with micro-CT will be
performed to reveal the 3D fracture mechanisms in the
fracture processes.
• The data will be incorporated to numerical models to better
understand the mechanical behaviors of the composites and
to better design the composite.
Materials and Method
• Fracture toughness (KIc) values were measured using 3-point
bending test in an Instron Electro E3000 Static/Fatigue Tester.
• All tests were conducted following ASTM E399.
Figure 1. Silicone Mold
Figure 3. Instron Tester Figure 4. A Closer Look At the 3-
point Bend Test
Figure 2. Composite Specimens
Summary
• Composite specimens were made by mixing epoxy and
alumina particle fillers of various weight fractions from 10%
to 60%.
• Three-point bending tests were conducted in order to find
out the fracture toughness of the specimens.
• Highest fracture toughness was measured for specimens
with 20 wt.% fillers.
• Several different fracture paths were revealed using micro-CT
scans.
References
• ASTM E399 standard
• Fu et al. Composites Part B: Engineering 39.6 (2008): 933-961.
• Du et al. Journal of the Mechanical Behavior of Biomedical
Materials 46 (2015): 41-48.
• Du et al. Acta Biomaterialia, 9.2 (2013): 5273-9.
• Epoxy resin was mixed with alumina particles grit size 180
(~76 microns).
• Composite of different volume fractions were cured in
rectangular silicone molds.
• Single edge notched bending (SENB) specimens (5 mm × 5
mm × 25 mm) were made by cutting using a diamond saw
and polishing.
Weight Fraction
Notch
Cracks
Specimen
Notch
100 µm
(MPam)

Undergraduate research poster presentation

  • 1.
    Results (a) (b) (c) (d) •In the 3-point bend test, as the displacement increased, the load on the specimens also increased. • When the cracks were initiated, the slope of the curves decreased. • The highest load at which the specimens fully fractured was the critical force. • Mode I fracture toughness KIc was calculated according to the ASTM E399 standard: 𝐾𝐼𝑐 = 𝑐𝑟𝑖𝑡𝑖𝑐𝑎𝑙 𝑓𝑜𝑟𝑐𝑒 ∗ 𝑠𝑝𝑎𝑛 ∗𝑓( 𝑎 𝑊 ) 𝑏𝑊1.5 f( 𝑎 𝑊 ) = 3 𝑎 𝑊 (1.99− 𝑎 𝑊 (2.15−3.93 𝑎 𝑊 +2.7 ( 𝑎 𝑊 )2) 2(1+2 𝑎 𝑊 )(1− 𝑎 𝑊 )2 where a is the notch length, b is the breadth, and W stands for the height of the specimen. • The fracture toughness of all specimens was in the range of about 1.5 to 2.5 MPa m. • Fracture toughness increased as the weight percentage increased from 10% to 20%, and then reduced as the weight percent kept increasing. • Fracture paths were revealed by micro X-ray computed tomography (micro-CT) images. • The specimens were numerically rendered as transparent to reveal the crack. • The cracks (gold) occurred in front of the notch (purple) and went into the specimens. • Several smaller micro-cracks coalesced into bigger cracks and propagated away from the notch (Figure 7(a)). • They went through the alumina particles and the epoxy matrix and sometimes along the matrix-particle interfaces (Figure 7(b-d)). • The deflection of the crack path is also observed in some slices (Figure 7(c)). Figure 5. Typical Load-Displacement Curves of 3-point Bend Test for Specimens with Different Weight Fractions Figure 6. 𝐊 𝐈𝐜 v.s. Weight Percentage/Volume Percentage of the Particles Figure 7. (a) 3-D Reconstruction of Fracture Paths and (b) to (d) Representative slices of Micro-CT Images Fracture Toughness of Particulate Polymer-ceramic Composites • Composite materials are widely used in various fields for their high strength- and stiffness-to-weight ratios. • Understanding the mechanical behaviors of composites is important to advance the design of these materials. • This study focuses on the fracture toughness (KIc) of polymer-ceramic composite materials. Introduction Authors: Ruyi Man1 , Jiacheng Gao1 , Abhinit Kothari1 , Kangning Su1 Supervisors: Jing Du1 , Michael Hillman2 1 Department of Mechanical and Nuclear Engineering, Pennsylvania State University 2 Department of Civil and Environmental Engineering, Pennsylvania State University Acknowledgments • David and Shirley Wormley Excellence Fund for the Support of World Class Engineers; • Student Research and Engagement Office, Penn State College of Engineering; • National Science Foundation Award #1826221. Future Works • Specimens with other filler fractions will be made and tested to further explore the relationship between the fracture toughness and filler fractions. • Specimens with different filler sizes will also be made and tested to explore the effects of filler size on the fracture toughness. • In situ 3-point bend coupled with micro-CT will be performed to reveal the 3D fracture mechanisms in the fracture processes. • The data will be incorporated to numerical models to better understand the mechanical behaviors of the composites and to better design the composite. Materials and Method • Fracture toughness (KIc) values were measured using 3-point bending test in an Instron Electro E3000 Static/Fatigue Tester. • All tests were conducted following ASTM E399. Figure 1. Silicone Mold Figure 3. Instron Tester Figure 4. A Closer Look At the 3- point Bend Test Figure 2. Composite Specimens Summary • Composite specimens were made by mixing epoxy and alumina particle fillers of various weight fractions from 10% to 60%. • Three-point bending tests were conducted in order to find out the fracture toughness of the specimens. • Highest fracture toughness was measured for specimens with 20 wt.% fillers. • Several different fracture paths were revealed using micro-CT scans. References • ASTM E399 standard • Fu et al. Composites Part B: Engineering 39.6 (2008): 933-961. • Du et al. Journal of the Mechanical Behavior of Biomedical Materials 46 (2015): 41-48. • Du et al. Acta Biomaterialia, 9.2 (2013): 5273-9. • Epoxy resin was mixed with alumina particles grit size 180 (~76 microns). • Composite of different volume fractions were cured in rectangular silicone molds. • Single edge notched bending (SENB) specimens (5 mm × 5 mm × 25 mm) were made by cutting using a diamond saw and polishing. Weight Fraction Notch Cracks Specimen Notch 100 µm (MPam)