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Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1723-
PAPER REF: 5452
PEAK LOAD ESTIMATION OF PRE-CRACKED PLAIN CONCRETE
BEAMS IN MIXED-MODE FRACTURE
X. Guo1,2(*)
, R. K.L. Su3, B. Young
3
1School of Mechanical Engineering, Tianjin University, Tianjin 300072, China
2Tianjin Key Laboratory of Nonlinear Dynamics and Chaos Control, Tianjin 300072, China
3Department of Civil Engineering, The University of Hong Kong, Pokfulam Road, Hong Kong
(*)Email: [email protected]
ABSTRACT
A major difficulty in simulating load response of a concrete structure in mixed-mode fracture
is that crack path is not known a priori. Predicting both the crack path and the associated load
response involves advanced simulation techniques and novel numerical methodologies, and
making these predictions remains a fundamental challenge to the community interested in
investigating mixed-mode fracture. Here, an intrinsic cohesive crack model is employed to
study mixed-mode fracture in a plain concrete beam with regular meshes. Simulations
illustrate that this concise approach can provide a reasonable estimation of peak load of the
pre-cracked plain concrete beams in mixed-mode fracture.
Keywords: mixed-mode fracture, cohesive crack, peak load.
INTRODUCTION
In a three-point-bending test of a concrete beam, a pre-crack, which shifts from load plane,
leads to asymmetric loading and thus a mixed-mode fracture event (John and Shah, 1990;
Guo et al., 1995). In addition, a double-edge-notched specimen in a Nooru-Mohamed test
(1992), a three-dimensional four-edge-notched specimen in a Hassanzadeh test (1991), and a
concrete plate with an embedded steel disk in a dowel disk test (1995) fracture in mixed
mode.
In contrast to simulating a concrete structure in mode-I fracture, simulating load response of a
concrete structure in mixed-mode fracture faces an extra difficulty because the crack path is
not known a priori. There have been numerous attempts to predict the load response of a
concrete structure in mixed-mode fracture. Galvez et al. (1998) found that the crack path from
linear elastic fracture mechanics (LEFM) analysis was a satisfactory approximation of the
actual crack path for concrete structures. Building on Galvez et al.’s finding, Cendon et al.
(2000) and Galvez et al. (2002a, 2002b) developed a two-step approach including numerically
predicting the crack path using the maximum tensile stress (MTS) criterion (Erdogan and Sih,
1963) and incorporating spring elements or cohesive elements.
Currently, in a framework of the finite element method (FEM), several available
methodologies to predict both the crack path and the associated load response of a concrete
structure in mix-mode fracture include the cohesive crack model, smeared crack model,
discontinuity approach, and eXtended FEM (XFEM).
The cohesive crack model was proposed to characterize phenomenology of a failure process,
based on a softening law (Dugdale, 1960; Barenblatt, 1962). Later, it was incorporated into
the FEM as an application to concrete fracture, allowing for fracture processes to be resolved
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Mechanical Behaviours of Advanced Materials and Structures at All Scales
-1724-
explicitly (Hillerborg et al., 1976; Bazant, 2002; Elices et al., 2002). Two approaches are
available in the framework of the cohesive crack model. The intrinsic cohesive crack model
usually embeds cohesive elements along the boundaries of volumetric elements as a part of
the physical model (Needleman, 1987; Guo et al., 2012a, 2012b, 2012c, 2013), whereas the
extrinsic model inserts cohesive elements into the model as fracture develops based on an
extrinsic fracture initiation criterion (Camacho and Ortiz, 1996; Ruiz et al., 2001; Yu and
Ruiz, 2006; Yu et al., 2008). Song et al. (2006) employed an intrinsic cohesive crack model
with a visco-elastic bulk material model to investigate mixed-mode fracture of asphalt
concrete. The predicted crack path was found to be in agreement with the experimental
results, but no result for the associated load response was presented. Lens et al. (2009)
investigated mixed-mode fracture of concrete and demonstrated that the cohesive model with
a “plastic” potential defined by Coulomb’s law with adherence was able to cope with the
spurious traction components. Using the extrinsic cohesive crack model, Ruiz et al. (2001)
formulated mixed-mode fracture of concrete specimens subjected to dynamic loading, and
accounted for micro-cracking, macroscopic crack development, and inertia effect. Yang and
Deeks (2007) coupled the FEM and the scaled-boundary FEM (SBFEM) for cohesive crack
propagation with a LEFM-based re-meshing procedure. The results showed that the SBFEM–
FEM coupled method was capable of predicting both the crack path and the load response
with a small number of degrees of freedom.
In the smeared crack model, infinite parallel cracks with infinitesimal openings are distributed
over the finite element, and crack propagation is simulated by a reduction in the stiffness and
strength of the material. The total strain is a sum of the strains resulting from the deformation
of the un-cracked material and the cracking process. The constitutive laws show strain
softening and introduce numerical difficulties (i.e., the system of equations may become ill-
posed) and localization instabilities and spurious mesh sensitivity may occur (Bazant and
Cedolin, 1979). Prisco et al. (2000) adopted multiple smeared crack models including
Ottosen’s model, the gradient Rankine plasticity model, and the crush-crack model based on
local and non-local approaches to investigate the mechanical behavior of plain and reinforced
concrete in mixed-mode fracture. Ozbolt and Reinhardt (2002) used a micro-plane model, a
type of the smeared crack model, for concrete in mixed-mode fracture, and predicted the
structural response and crack patterns realistically.
Sancho et al. (2007b) developed a strong discontinuity model with crack equilibrium at the
element level, cohesive cracking with central forces, and limited local crack adaptability; they
found that it could describe the crack propagation with adequate accuracy. Cohesive crack
propagation was formulated based on a truly-mixed discretization with the stresses as main
regular variables, while discontinuous displacements played the role of Lagrangian
multipliers (Bruggi and Venini, 2009). The approach handled the cohesive cracks through the
appropriate inclusion of cohesive energy terms that enrich the formulation. Generally, a major
difficulty in the discontinuity approach is that the crack propagation may lock because of
kinematical incompatibility among the cracks; therefore, special implementation should be
taken to prevent crack locking (Sancho et al., 2007a).
In the XFEM, crack propagation through a finite element is modeled by the enrichment of the
classical displacement-based finite element’s approximation by a discontinuous function
obtained through the partition of unity (Babuska and Melenk, 1997). Areias and Rabczuk
(2008) modeled set-valued softening laws in plate bending and plane crack propagation and
presented an algorithm for the softening law to determine the crack path. Generally, a major
difficulty with the XFEM lies in modeling spontaneous multiple crack initiation, branching,
and coalescence (Song et al., 2008).
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1725-
Overall, simulating both the crack path and the associated load response of a plain concrete
structure in mixed-mode fracture requires advanced simulation techniques and even novel
numerical methodologies and remains a fundamental challenge in the community interested in
investigating mixed-mode fracture. Among the above methodologies in the framework of the
FEM, the cohesive crack model is comparatively simpler in concept and easier in application
and has come to be popular in the research on non-linear fracture mechanics. Compared with
the intrinsic cohesive crack model, the extrinsic one involves some issues, both in the model
implementation and in the results interpretation (Zhang et al., 2007). Therefore, in a previous
study of Guo et al. (2012c), the intrinsic cohesive crack model was employed to investigate
mode-I fracture of three-point-bending specimens and to extract the best-fit energy and stress
ratios for both normal-strength and high-strength concrete. As an extension of Guo et al.
(2012c), the intrinsic cohesive crack model with a bilinear softening law is employed here to
study mixed-mode fracture in a plain concrete beam. Simulations with regular (not oriented)
meshes illustrate that the approach can provide a reasonable estimation on the peak load of
the pre-cracked plain concrete beam. Parametric studies are conducted to investigate effects of
the energy and stress ratios and cohesive strength on the load response and energy terms.
COHESIVE CRACK MODEL WITH A BILINEAR SOFTENING LAW
The cohesive crack model is formulated on the virtual work (Roesler et al., 2007). The
internal work done by the virtual strain tensor ( εδ ) in the domain (Ω ) and the internal work
by the virtual crack opening displacement vector ( wδ ) along the crack line ( cΓ ) are equal to
the external work by the virtual displacement vector ( uδ ) at the traction boundary (Γ ), i.e.,
∫∫∫ ΓΓΩΓ=Γ+Ω dδdδdδ TTT PuTwσε
cc
(1)
where σσσσ is the stress tensor, T is the traction vector in the cohesive zone, and P is the
external traction vector. The resulting cohesive crack model has been implemented in
ABAQUS (2011).
A bilinear softening law has been gradually accepted as a reasonable approximation to the
softening behavior in concrete. It can be fully characterized by four parameters: cohesive
strength mT , fracture energy FG , initial fracture energy fG , and kink stress kT , a stress level
corresponding to kw (a separation at the kink point). Equivalently, in line with the previous
study of Guo et al. (2012), mT , FG , an energy ratio (the ratio of the fracture energy to the
initial fracture energy FG / fG ), and a stress ratio (the ratio of the kink stress to the cohesive
strength kT / mT ) are employed in this study. To restrict the inherent mesh dependence, the
penalty stiffness is used to modify the bilinear softening law, as shown in Fig. 1. The cohesive
strength mT is the softening stress at which the separation reaches mw and damage initiates.
The fracture energy FG is the work required to create and fully separate a unit surface area of
a cohesive element and is given by the area under the softening law, i.e.,
( )∫=cw
F wwTG0
d (2)
where T is an effective traction, w is an effective separation, and cw is the critical crack
opening beyond which the traction becomes zero and the cohesive element fails completely.
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Mechanical Behaviours of Advanced Materials and Structures at All Scales
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The effective traction and the effective separation can be defined as
222
sn TTT −+= η and 222
sn www η+= (3)
where nT and sT are the cohesive tractions in the normal and tangential directions,
respectively, nw and sw are the normal and tangential opening displacements across the
cohesive surfaces, respectively, and η is the tension-shear coupling constant representing the
effect of the mixed mode (Zhang et al., 2007).
The softening law in Fig. 1 has two stages. In stage O-A, the cohesive element deforms
elastically. Damage initiates at the critical point A. Note that mw should be much smaller than
kw so that the penalty stiffness can be sufficiently large. During stage A-B-C, the separation
of the cohesive element increases, and the cohesive element is softened, i.e., damage evolves.
The softening stress can be formulated as
( )
( )( ) k c
for (A B);
for w w w (B C).
m k
m m k
k
k k
k
c k
T T wT w w w
wT
T w wT
w w
−− < ≤ →
=
− − < ≤ → −
(4)
Same with Song et al. (2006), the tension-shear coupling constant η is taken as 1, i.e., the
quadratic strain criterion is employed for damage initiation and evolution in the cohesive
elements.
Fig. 1 - Softening law with a penalty stiffness to restrict mesh dependence.
MIXED-MODE FRACTURE SIMULATION OF PRE-CRACKED PLAIN
CONCRETE BEAMS
Here, the four-point, single-edge notched shear beams tested by Arrea and Ingraffea (1982)
are studied. Their testing results, especially load versus crack mouth sliding displacement
(CMSD) curves, have become a benchmark for mixed-mode crack propagation analysis. The
geometry and boundary conditions of the series B beams in their test are shown in Fig. 2. The
analytical configuration adopted has a span of 914 mm, a depth of 308.5 mm, a thickness of
Separation w
SofteningStressT
Gf
GF
O
(wm, T
m)
B (wk, T
k)
Penalty stiffness
A
C (wc, 0)
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores,
152 mm, and a pre-crack length
prevailed. The specimen is discretized into the volumetric and cohesive elements. Uniform
linear cross-triangular meshes
the experiments, displacement control
Fig. 2 - An analytical configuration
A linear elastic constitutive law
constitutive parameters in Arrea and Ingraffea
Poisson’s ratio of 0.18, and compressive strength of 45.5 MPa, which
the present simulations. The fracture behavior predicted by the cohesive cr
heavily on the cohesive strength and the fracture energy employed
et al., 2008). Generally, although
by the work-of-fracture method,
measuring the mode-II fracture energy
crack model, the tensile strength has generally been taken as the cohesive strength
and Ortiz, 1996; Ruiz et al., 2001;
intrinsic cohesive crack model, t
example, from a direct tensile test
tensile tests of concrete are difficult to perform and the results always scatter extensively.
Generally, the result of a splitting
(Guinea et al., 1994). In line with prior studies employing the intrinsic cohesive crack model
for concrete (Roesler et al., 2007
taken here to be its mode-I cohesive strength
employing the extrinsic cohesive crack model for concrete, the tensile strength of
is also taken here to be its mixed
Neither the fracture energy FG
(1982). A wide range of values were used for
listed in Table 1, where mIIT
=3.7 MPa, which are the same as
taken to be the same as FIG
Unless otherwise stated, the
shear stress when shear failure occurs
compressive strength cuf was measured to be 45.5
internal friction angle φ can be
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1727-
crack length 0a of 82 mm. It is assumed that the condition of plain strain
s discretized into the volumetric and cohesive elements. Uniform
triangular meshes (3 mm in size) are used in the potential fractured zone.
the experiments, displacement control is used in the simulations.
An analytical configuration for a four-point single-edge notched shear beam
constitutive law is applied to the concrete itself. The available material
parameters in Arrea and Ingraffea (1982) include Young’s modulus of 24.8 GPa,
Poisson’s ratio of 0.18, and compressive strength of 45.5 MPa, which are
The fracture behavior predicted by the cohesive cr
heavily on the cohesive strength and the fracture energy employed (Roesler et al., 2007; Park
although the mode-I fracture energy FIG of concrete
fracture method, proposed by RILEM TC 50-FMC (1985)
II fracture energy FIIG is still under the way. In the extrinsic cohesive
crack model, the tensile strength has generally been taken as the cohesive strength
2001; Yu and Ruiz, 2006; Yu et al., 2008). Theoretically, in the
intrinsic cohesive crack model, the cohesive strength is unknown and should be calibrated, for
example, from a direct tensile test (Cornec et al., 2003; Guo et al., 2010, 2012c)
tensile tests of concrete are difficult to perform and the results always scatter extensively.
splitting-tension test can provide an estimate of the tensile strength
In line with prior studies employing the intrinsic cohesive crack model
et al., 2007; Guo et al., 2012b), the tensile strength of concrete,
I cohesive strength mIT . Furthermore, in line with prior studies
ic cohesive crack model for concrete, the tensile strength of
mixed-mode cohesive strength mT .
F nor the tensile strength tf was reported in Arrea and Ingraffea
. A wide range of values were used for the series B beams by different analysts, as
is the mode-II cohesive strength. Here, FIG
ame as those in Galvez et al. (2002a, 2002b), are
such that the total fracture energy is FG =Unless otherwise stated, the mode-II cohesive strength is evaluated as the critical internal
shear stress when shear failure occurs in a simple compression, i.e., c =
was measured to be 45.5 MPa (Arrea and Ingraffea
can be taken as 030 , and thus, 7.19=c MPa. The
s assumed that the condition of plain strain
s discretized into the volumetric and cohesive elements. Uniform
used in the potential fractured zone. As in
edge notched shear beam.
The available material
Young’s modulus of 24.8 GPa,
are also employed in
The fracture behavior predicted by the cohesive crack model depends
(Roesler et al., 2007; Park
of concrete can be measured
(1985), an approach to
In the extrinsic cohesive
crack model, the tensile strength has generally been taken as the cohesive strength (Camacho
Theoretically, in the
ohesive strength is unknown and should be calibrated, for
al., 2010, 2012c). Direct
tensile tests of concrete are difficult to perform and the results always scatter extensively.
test can provide an estimate of the tensile strength
In line with prior studies employing the intrinsic cohesive crack model
, the tensile strength of concrete, tf , is
n line with prior studies
ic cohesive crack model for concrete, the tensile strength of concrete tf ,
was reported in Arrea and Ingraffea
series B beams by different analysts, as
FI =107 N/m and tf
are used, and FIIG is
FIFIIFI GGG 2=+= .
the critical internal
φφ cossincuf . The
Arrea and Ingraffea, 1982), and the
The mode-I cohesive
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Mechanical Behaviours of Advanced Materials and Structures at All Scales
-1728-
strength mIT and the mode-II cohesive strength mIIT are used in the penalty and damage
initiation parts in Fig. 1 while the mixed-mode cohesive strength mT is used in the damage
evolution part in Fig. 1.
Table 1 Available approaches to simulate experiments in Arrea and Ingraffea (1982) and the fracture energy GF
and tensile strength tf employed.
Reference Approach Fracture energy FG (N/m) Tensile strength
tf (MPa)
Rots & De Borst (1987) Smeared crack model 75 2.7
Xie & Gerstle (1995) Energy-based extrinsic
cohesive crack model
150 4.0
Saleh & Aliabadi (1995) Boundary element
model
100 2.8
Cendon et al. (2000) LEFM + spring model 125 4.0
Galvez et al. (2002a,
2002b)
LEFM + intrinsic
cohesive crack model FIG =107 3.7
Yang & Deeks (2007) Scaled boundary FEM
+ extrinsic cohesive
crack model + LEFM-
based re-meshing
FIG =100 N/m, FIIG =0.1
FIG
=10 N/m mIT =
tf =3.0 MPa,
0.13/ == tmII fT MPa
Yu et al. (2008) Extrinsic cohesive
crack model
99.4 2.8
The present authors Intrinsic cohesive crack
model FIG =107 N/m,
FIIG =FIG
=107 N/m mIT =
tf =3.7 MPa, mIIT
=c=19.7 MPa
As a feature and also a limitation due to its basic assumption, in the cohesive crack model,
crack path is confined to bulk-element boundaries, which are not necessarily coincident with
the actual crack path. Fig. 3 shows a typical crack path in the present simulation with an
energy ratio of 2.0 and a stress ratio of 0.25. It can be found that the main crack propagation
included two line segments, namely, the first one starting from the pre-crack tip and oriented 045 and the second one kinked 045 and pointing upward. The crack path is very close to that
in Oliver et al. (2002) via the strong discontinuity approach. There is an obvious local mixed
mode when the crack propagates from the pre-crack, as the kink between the pre-crack and
the first line segment shows. Upon careful observation of the kink region between the two line
segments, multiple micro-cracks initiate there and actually formed a transitional region. The
deviation of the crack path having two kinked line segments from the actual crack path being
a smooth curve has a potential effect on energy release rate and the associated load response.
Fig. 3 - Crack path in the simulation with an energy ratio of 2.0 and a stress ratio of 0.25 when the CMSD is
0.133 mm (a deformation scale factor of 100 is employed for clear illustration).
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1729-
EFFECTS OF THE ENERGY RATIO ON THE LOAD RESPONSE AND
ENERGY TERMS
Bazant and Becq-Giraudon (2002) confirmed a value of 2.5 as the optimal energy ratio, with a
variation of approximate 40% from a database involving 238 test series. Bazant (2002)
reviewed the available research on concrete fracture and found that the energy ratio could be
taken as 2.5 and that the stress ratio varied from 0.15 to 0.33. In this section, three levels of
energy ratio (1.5, 2.0, and 2.5) and a stress ratio of 0.25 are chosen. Load-CMSD curves in the
present simulations, together with the lower and upper bounds of experimental results in
Arrea and Ingraffea (1982), are illustrated in Fig. 4. As the energy ratio increases, the initial
fracture energy decreases, and the concrete is damaged more easily; thus, both the peak load
and the peak-load CMSD decrease. By comparing the simulation results with the
experimental results in Fig. 4, it can be found that the width of the peak region larger than that
in the experimental results. After the peak region, the simulation results are larger than the
experimental ones, due to the difference between the crack path in the simulations and the
actual crack path, as shown in Fig. 3. The maximum energy release rate criterion states that
the actual crack propagates in a direction that maximizes the release of stored energy in the
structure. Therefore, the crack path in the simulation releases stored energy at a slower pace.
Fig. 4 - Simulated load-CMSD curves with three levels of energy ratio and a stress ratio of 0.25, together with
the lower and upper bounds of experimental results.
Energy terms are extracted from the simulations for further analysis. For the specimen here,
the damage dissipation, external work, and strain energy versus the CMSD are illustrated in
Fig. 5. Both the damage dissipation and the external work increase monotonically with the
CMSD, i.e., with the fracture process. As shown in Fig. 5a, the damage dissipation increases
with an increasing energy ratio. After damage initiation, as the energy ratio increases, the
initial fracture energy decreases, i.e., the softening stress in this region also decreases.
Therefore, the concrete is damaged more easily, and a comparatively larger fracture process
zone (FPZ) occurs, leading to larger cumulative damage dissipation. Fig. 5b shows that, after
damage initiation, the external work decreases with the energy ratio because less work is
required to overcome the initial fracture energy for the case of the larger energy ratio. Before
the peak-load occurs, the strain energy increases in a parabolic manner, as shown in Fig. 5c.
After the strain-energy peak, as the FPZ increases, the unloading in the undamaged zone
occurs around the FPZ, which explains why the strain energy decreases when extensive
CMSD (mm)
LoadP(KN)
0 0.02 0.04 0.06 0.080
50
100
150
200
Stress ratio=0.25
Lower bound of exp. resultsUpper bound of exp. results
Energy ratio=1.5Energy ratio=2.0
Energy ratio=2.5
Symposium_17
Mechanical Behaviours of Advanced Materials and Structures at All Scales
-1730-
damage is present.
Fig. 5 - (a) Damage dissipation, (b) external work, and (c) strain energy versus the CMSD with three levels of
energy ratio and a stress ratio of 0.25.
EFFECTS OF THE STRESS RATIO ON THE LOAD RESPONSE AND THE
ENERGY TERMS
In this section, an energy ratio of 2.5 and three levels of stress ratio (0.15, 0.25, and 0.35) are
chosen. The predicted load-CMSD curves are illustrated in Fig. 6. For a specimen with a
median size, when the load is at the peak position, the FPZ around the pre-crack tip is small;
thus, the softening stress at the crack tip is almost defined by the initial linear segment of the
bilinear softening law. Therefore, the peak load is dominated by the initial fracture energy Gf.
When the energy ratio is fixed, the peak of the load-CMSD curves remains almost the same,
as shown in Fig. 6, and is in agreement with many available numerical simulations, as
reviewed in Bazant (2002). Because the peak of the load-CMSD curve is mainly dominated
by the initial fracture energy and depends less on the stress ratio, the stress ratio of 0.15
recommended by the CEB-FIP Model Code (1993) predicts the same peak load as the other
stress ratios. After the peak, with the FPZ around the pre-crack developing further, the crack
tip displacement (the vector sum of crack tip opening and sliding displacements) is larger than
kw , and thus, the softening stress in the FPZ is larger for a larger stress ratio. As the stress
ratio increases from 0.15 to 0.25, the load level in the post-peak region remains almost
identical; as the stress ratio further increases from 0.25 to 0.35, the load level in the post-peak
region increases significantly.
Fig. 6 - Simulated load-CMSD curves with an energy ratio of 2.5 and three levels of stress ratio.
CMSD (mm)
Damagedissipation(J)
0 0.02 0.04 0.06 0.08 0.10
0.5
1
1.5
Stress ratio=0.25
Energy ratio
1.52.02.5
CMSD (mm)
Externalwork(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
20
Stress ratio=0.25
Energy ratio1.52.02.5
CMSD (mm)
Strainenergy(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Stress ratio=0.25
Energy ratio1.52.02.5
CMSD (mm)
LoadP(KN)
0 0.02 0.04 0.06 0.080
50
100
150
200
Energy ratio=2.5
Stress ratio=0.15Stress ratio=0.25Stress ratio=0.35
a b c
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1731-
Next, the effect of the stress ratio on the energy terms is studied. For the specimen here, the
damage dissipation, the external work, and the strain energy versus the CMSD are illustrated
in Figs. 7. All three energy terms are almost independent of the stress ratio before the peak-
load CMSD. Both the damage dissipation and the external work increase monotonically with
the fracture process. As shown in Fig. 7a, the damage dissipation has negligible dependence
on the stress ratio. Fig. 7b shows that the external work increases with the stress ratio after the
peak-load CMSD because, when extensive damage occurs, more work is required to
overcome the larger softening stress in the case of the larger stress ratio. Before the peak-load
CMSD, the strain energy increases in a parabolic manner, as shown in Fig. 7c. After the peak-
load CMSD, for the case of the stress ratios 0.15 and 0.25, the strain energy decreases because
of the unloading in the undamaged zone; for the stress ratio 0.35, the strain energy remains
constant and then increases.
Fig. 7 - (a) Damage dissipation, (b) external work, and (c) strain energy versus the CMSD with an energy ratio of
2.5 and three levels of stress ratio.
EFFECTS OF THE COHESIVE STRENGTH ON THE LOAD RESPONSE AND THE
ENERGY TERMS
Fig. 8 illustrates the simulated load-CMSD curves with an energy ratio of 2.5, a stress ratio of
0.25, and three levels of the mode-I cohesive strength mIT , i.e., tf80.0 (2.96 MPa), tf90.0
(3.33 MPa), and tf (3.70 MPa). Fig. 8 shows that the peak load increases clearly with mIT
while the increasing rate of the peak load is smaller than that of mIT . Furthermore, the peak-
load CMSD decreases as mIT increases. The associated damage dissipation, the external work,
and the strain energy versus the CMSD are illustrated in Fig. 9. The damage dissipation
increases negligibly with mIT , as shown in Fig. 9a. Fig. 9b shows that the external work
always increases with the CMSD. Fig. 9c shows that the strain energy increases with the
CMSD before the peak-load CMSD and then decreases after the peak-load CMSD due to
unloading in the undamaged zone around the FPZ. Figs. 9b and c show that the external work
and the strain energy increase with mIT .
CMSD (mm)
Damagedissipation(J)
0 0.02 0.04 0.06 0.08 0.10
0.5
1
1.5
Energy ratio=2.5
Stress ratio
0.150.250.35
CMSD (mm)
Externalwork(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.5
Stress ratio
0.150.250.35
CMSD (mm)
Strainenergy(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.5
Stress ratio
0.150.250.35
a b c
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Mechanical Behaviours of Advanced Materials and Structures at All Scales
-1732-
Fig. 8 - Load-CMSD curves with an energy ratio of 2.5, a stress ratio of 0.25, and three levels of mIT .
Fig. 9 - (a) Damage dissipation, (b) external work, and (c) strain energy versus the CMSD with an energy ratio of
2.5, a stress ratio of 0.25, and three levels of mIT .
Fig. 10 illustrates load-CMSD curves with an energy ratio of 2.0, a stress ratio of 0.25, and
three levels of the mode-II cohesive strength mIIT , namely, c50.0 (9.85 MPa), c75.0 (14.775
MPa), and c (19.70 MPa). Fig. 10 shows that the load curves essentially coincide and show
nearly no dependence on mIIT . The associated damage dissipation, the external work, and the
strain energy versus the CMSD are illustrated in Fig. 11. After the peak-load CMSD, the
damage dissipation in the case of c50.0 is larger than that in the case of c75.0 and c by
almost a constant, as shown in Fig. 11a. On careful observation of Fig. 11a, the constant
amount of damage dissipation difference is accumulated during the initiation stage of the
crack propagation from the pre-crack. Figs. 11b and c show that the external work and the
strain energy are essentially independent of the mIIT . These observations are in agreement
with the current understanding that the crack grows mainly in a stable manner in local mode-I
under a global mixed-mode loading, as implied by the MTS criterion (2002), and that a
mixed-mode fracture mechanism dominates at crack initiation, though the specimens finally
fracture in mode-I manner (Ozbolt and Reinhardt, 2002). Furthermore, Figs. 8-11 show that
mIT had much larger effects on the load response and the energy terms than mIIT .
CMSD (mm)
Load(KN)
0 0.02 0.04 0.06 0.080
50
100
150
Energy ratio=2.5Stress ratio=0.25
TmI=0.80f
t
TmI=0.90f
t
TmI=1.00f
t
CMSD (mm)
Damagedissipation(J)
0 0.02 0.04 0.06 0.08 0.10
0.5
1
1.5
Energy ratio=2.5Stress ratio=0.25
TmI=0.80f
tTmI=0.90f
tTmI=1.00f
t
CMSD (mm)
Externalwork(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.5Stress ratio=0.25
TmI=0.80f
tTmI=0.90f
t
TmI=1.00f
t
CMSD (mm)
Strainenergy(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.5Stress ratio=0.25
TmI=0.80f
tTmI=0.90f
tTmI=1.00f
t
a b c
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-1733-
Fig. 10 - Load-CMSD curves with an energy ratio of 2.0, a stress ratio of 0.25, and three levels of mIIT .
Fig. 11 - (a) Damage dissipation, (b) external work, and (c) strain energy versus the CMSD with an energy ratio
of 2.0, a stress ratio of 0.25, and three levels of mIIT .
CONCLUSIONS
In this study, the intrinsic cohesive crack model with a bilinear softening law is employed to
investigate mixed-mode fracture in a plain concrete beam. In contrast to the available
research, the present approach requires neither preliminary results from LEFM simulations
nor a re-meshing procedure or special implementation to prevent crack locking. The
simulations with regular meshes show that the approach can provide a reasonable estimation
of the peak load of the plain concrete structure. The parametric studies illustrate that the
energy ratio in the bilinear softening law have larger effects on the load response and energy
terms than the stress ratio. The simulations also confirm that the crack initiates in a mixed-
mode manner but grows in local mode-I under a global mixed-mode loading and that the
mode-I cohesive strength has much larger effects on the load response and the energy terms
than the mode-II cohesive strength.
ACKNOWLEDGMENTS
X. Guo acknowledges financial support from National Natural Science Foundation of China
(Project nos. 11372214 and 11102128) and Postdoctoral Fellowship from Faculty of
Engineering and UDF-Computational Science and Engineering (CSE) at The University of
Hong Kong.
CMSD (mm)
LoadP(KN)
0 0.02 0.04 0.06 0.080
50
100
150
200
Energy ratio=2.0Stress ratio=0.25
TmII=0.50c
TmII=0.75c
TmII=1.00c
CMSD (mm)
Damagedissipation(J)
0 0.02 0.04 0.06 0.08 0.10
0.5
1
1.5
Energy ratio=2.0Stress ratio=0.25
TmII=0.50c
TmII=0.75c
TmII=1.00c
CMSD (mm)
Externalwork(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.0Stress ratio=0.25
TmII=0.50c
TmII=0.75c
TmII=1.00c
CMSD (mm)
Strainenergy(J)
0 0.02 0.04 0.06 0.08 0.10
5
10
15
Energy ratio=2.0Stress ratio=0.25
TmII=0.50c
TmII=0.75c
TmII=1.00c
a b c
Symposium_17
Mechanical Behaviours of Advanced Materials and Structures at All Scales
-1734-
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