International Journal of Civil Engineering
https://doi.org/10.1007/s40999-018-0336-6
RESEARCH PAPER
Predicting the Shear Behavior of Reinforced Concrete Beams Using
Non-linear Fracture Mechanics
Vahid Broujerdian1
· Hossein Karimpour1 · Sobhan Alavikia1
Received: 11 September 2017 / Revised: 23 May 2018 / Accepted: 31 May 2018
© Iran University of Science and Technology 2018
Abstract
This paper deals with the challenging problem of predicting the load carrying capacity of reinforced concrete shear-critical
beams. To simulate the cracking behavior of concrete, the discrete crack approach based upon non-linear fracture mechanics
is used. An algorithm with two pathways of implementation has been proposed so as to implement fictitious crack model
to analyze reinforced concrete beams using finite-element method. The merit of the proposed algorithm is its capability to
recognize and to incorporate them in the analysis procedure. The proposed method is capable of predicting simultaneous
multiple shear cracks, load-deformation behavior, and ultimate shear capacity of reinforced concrete beam. The obtained
results show a good compliance with the available experimental benchmark studies on reinforced concrete beams failed
in shear. As one of the important aspects of shear capacity is the size effect issue, some large-scaled test beams have been
numerically simulated using the proposed algorithm and the results have been compared with that of ACI 318-11 building
code as well as the well-known modified compression field theory (MCFT). The comparison corroborated the robustness of
the proposed algorithm in detecting the well-known shear-scaling phenomenon. In the same time, the comparison emphasized on the weakness of the current codes of practice to overestimate the shear capacity of large-scaled beams owing to
not taking the size effect into account.
Keywords Reinforced concrete · Beam · Shear · Fictitious crack model · Finite element
1 Introduction
Diagonal cracking and shear behavior of reinforced concrete
has been one of the conspicuous challenges which has been
dealt with researchers since last century [1, 2]. Although
several experimental as well as analytical models have been
developed so far, there is not any generally confirmed and
comprehensive model capable of relating the shear behavior
to the main known factors. As a result, the current codes
of practice concerning shear design of reinforced concrete
[3–6] are merely empirical relations based on very simple
physical models calibrated by some test results. On the other
* Vahid Broujerdian
broujerdian@iust.ac.ir
Hossein Karimpour
karimpour_h@alumni.iust.ac.ir
Sobhan Alavikia
s_alavikia@alumni.iust.ac.ir
1
Department of Civil Engineering, Iran University of Science
and Technology, Tehran, P.O. Box 16765-163, Iran
hand, studies show that safety factors are not integrated for
different parameters [7, 8].
Using the classic theories of solid mechanics, some
aspects of concrete behavior are neither justifiable nor predictable. In fact, the classic solid mechanics cannot justify
failures that occur in stresses far below the ultimate strength
of a concrete structure [9–11]. ACI 318 code of practice
[3], in its simple relation, specifies the√shear capacity of
reinforced concrete beams as Vc = 0.17 f � c bw d , in which
f ′ c is the compressive strength of concrete in MPa, d and bw
are the effective depth and the width of the beam, respectively, in mm, and Vc is in Newton. This equation is obtained
based on ASCE-ACI 326 data bank [12] that only includes
small beams with average depth of 340 mm. According to
the above-mentioned equation, the average shear strength
of concrete, vc = Vc ∕bw d , is independent of size. However,
experimental observations including experiments conducted
in Tokyo University [13] and Toronto University [14–16]
demonstrate that the consideration of size effect in codes
of practice is indispensable. In addition, recent surveys on
some structure failures have shown that the size effect is one
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International Journal of Civil Engineering
of the main contributory factors in failure [8]. A newer data
bank including 398 data published by ACI445 Committee
[17] clearly shows that in some cases, shear provisions of
ACI code are not on the safe side.
One of the leading cause of fracture and failure of structures is the presence of initial defects and cracks and their
propagation. Defective construction, environmental factors,
and applied loads may give rise to cracks with different size
and shape. Cracks show different behaviors under different loading conditions. Some of these cracks propagate
and bring about disastrous failure of structures. Fracture
mechanics is the knowledge of examination of crack formation in solids, calculation of fractured structure response
to applied loads, and prediction of structure behavior considering the propagation of initial cracks. Development of
fracture mechanics in the last century has clarified that accurate analysis of many concrete structures entails the use of
fracture mechanics principles.
One of the branches of fracture mechanics employing
some simplifications based on ignoring the crack tip plasticity is Linear Elastic Fracture Mechanics, LEFM, established by Griffith based on his experiments on glass fibers
[18]. During 1960–1970, several researches showed that
the classic LEFM is not capable of analyzing usual sized
concrete structures [19]. Non-functionality of LEFM has
been illuminated by the examination of Fracture Process
Zone (FPZ). FPZ is a zone with micro cracks that includes
ligaments still transferring stress. Researches have indicated
that if softening behavior of material is considered, fracture
mechanics can be a powerful tool for analysis of propagation of distributed cracks as well as localization of them in
concrete [20–22].
Several models have been proposed so far to predict
cracking behavior of concrete based on non-linear fracture
mechanics. To employ these models for prediction of actual
response of structures, making use of numerical methods
such as FEM is inevitable. There are two main approaches
for crack modeling via finite element, namely, smeared
crack and discrete crack. In the former approach, the cracked
element is considered continuous, while its governing constitutive law is changed to account for the effects of cracks
[23–25]. Although this approach is convenient, its main
shortcomings are non-objectivity and mesh-sensitivity of the
results. Furthermore, it cannot provide details such as crack
mouth opening displacement or crack path [20]. However,
in the latter approach, crack is considered as a geometrical
discontinuity [26]. Consequently, re-meshing after each step
of crack propagation is needed. In discrete crack approach,
the fracture process zone characteristics such as shape and
cohesive forces are considered as boundary conditions of
the problem. Since the analytical method in this type of
modeling is close to the physical condition of concrete, this
method named Fictitious Crack Model (FCM) is the most
accurate method for analysis of concrete.
After all, one of the intact areas in the discrete crack
approach is the lack of multi-crack analysis based on FCM
[27–29]. In this paper, an attempt in this ground is presented.
Utilizing the ABAQUS software [30], a semi-automatic
algorithm is proposed for this end. The presented method
provides responses that are precise enough in comparison
with benchmark problems. The algorithm enhances analysis
to simulate multiple cracks, diagonal cracks, and size effect
phenomenon.
2 Theoretical Background
As it is known, the existence of FPZ, with a considerable
size in concrete, ahead of structural macro cracks introduces a significant non-linearity in its behavior. The simplest description of what is happening in FPZ developed
by Hillerborg et al. in 1976 named Fictitious Crack Model,
FCM [31]. They proposed a tension-softening law based on
Cohesive Crack Model, CCM, of Dugdale and Barenblatt
[32, 33] to analyze a plain concrete beam (Fig. 1).
Indeed, FCM lumps all the FPZ into the crack line and
formulates it in the form of a softening stress–displacement
law. Since this analytical approach is focusing on real physical
Fig. 1 Fictitious crack model: a real crack in concrete, b fictitious crack, c tension-softening relation
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International Journal of Civil Engineering
conditions of concrete, the method is considered as one of the
most accurate methods of concrete crack analysis. In addition,
Hillerborg and his colleagues provided a numerical approach
for crack analysis of a concrete beam under pure bending with
only one single crack that can only be induced in the mid-span.
Their proposed algorithm is summarized as follows:
1. analysis of beam;
2. locating crack extension based on the analysis;
3. applying cohesive forces on the sides of crack (based on
tension-softening relation);
4. stress analysis with new boundary conditions;
5. repeat steps until structural failure.
In reality, it is rare to confront a reinforced concrete element
with only one single crack. In real problems, there exist multiple cracks at the same time with different reactions to applied
loads: propagation, arrest, and closure. Therefore, considering all of the states that can occur upon loading, analysis of a
multiple-crack problem could be very complicated. The gap of
research in this area confirms this fact. This paper is aiming at
introduction of a method to overcome this difficulty.
According to Griffith theory [18, 34], creation and propagation of crack are inevitable processes of energy transfer of body
in equilibrium state. In addition, fracture energy is required for
creation of a new crack to reach minimum potential energy
state. The cohesive fracture energy GF is the external energy
required to fully break a unit surface area of cohesive crack.
Assuming a linear pre-peak tensile behavior for concrete, it
can be shown that GF is equal to the area under the softening
curve (Fig. 1c) [33].
The J integral is usually used to characterize the energy
release associated with crack growth. The J integral is a reliable fracture mechanics parameter for both linear and nonlinear material response [21]. It is a measure of the intensity
of deformation at a notch or crack tip, especially for non-linear
materials. In quasi-static analysis, two-dimensional definition
of J integral is
J = lim ∫ n . H . q dΓ
Γ→0 Γ
(1)
where Γ is a contour starting from the bottom of crack surface to the top surface (Fig. 2). The limit Γ → 0 indicates
that Γ shrinks onto the crack tip; q is a unit vector in the virtual crack extension direction; and n is the outward normal
to Γ. H is defined as
H = WI − 𝝈 .
𝜕u
𝜕x
(2)
where I is second order identity tensor, 𝝈 is stress tensor,
𝜕u∕𝜕x is displacement gradient tensor, and W is the elastic strain energy for elastic behavior. For elastic–plastic
behavior, W is the elastic strain energy density plus plastic
Fig. 2 Contour for evaluation of the J integral
dissipation representing the strain energy in an equivalent
elastic material. This study has been based on LEFM with
additional development to account for non-linearity of concrete as a quasi-brittle material.
3 Methods
The problem at hand is to simulate shear-critical reinforced
concrete beams under 3-point-bending test condition. In
addition to develop load-deformation behavior, it is aimed
at obtaining an acceptable estimation of cracking pattern as
well as mode of failure. Figure 3 illustrates the flowchart of
the proposed algorithm which can solve such problem in
a load-control manner. The main concept of the proposed
algorithm is to increase the applied load incrementally so
as to figure out locations in the beam where the maximum
principal stress reaches the tensile strength of concrete, and
then, the cracks initiate and propagate in critical direction.
Cohesive forces are applied on the crack sides during crack
evolution in each step. The path of crack propagation is
assumed to be normal to the direction of maximum principal stress. The analysis continues up to the maximum load,
where the convergence of the finite-element analysis cannot
be achieved beyond it. According to this semi-automatic
algorithm, analysis part of each step is done by computer
using the ABAQUS software, but increasing crack length
and applying cohesive forces on crack edges in each step are
carried out manually.
To account for cohesive forces, a linear tension-softening
function, as shown in Fig. 4, is used. As seen in this figure, the maximum cohesive stress is the tensile strength of
concrete, ft, corresponding to zero opening of crack mouth,
w = 0, and the minimum value is zero corresponding to critical opening of wc. Thus, cohesive forces are calculated as
)
(
w
𝜎 = ft 1 −
, for 0 ⩽ w ⩽ wc
(3a)
wc
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International Journal of Civil Engineering
In the first method, after numerical analysis in each step
and obtaining the stress distribution in the concrete elements, potential zones for crack initiation are located. To
this aim, the criterion of limiting the maximum principal
stress to the tensile strength of concrete is utilized. Then,
the cracks are propagated manually in the direction normal
to that of the maximum principal stress. To define the crack
extension in this method, there is a special sub-menu in the
ABAQUS software capable of assigning crack property to
any desired line. A seam defines an edge with overlapping
nodes that can separate during an analysis. This crack is
originally closed but can open during an analysis. ABAQUS
places overlapping duplicate nodes along a seam when the
mesh is generated. After creation of seam, crack properties
can be determined using a contour integral analysis.
Now, the equivalent nodal cohesive pair forces are calculated and applied on the nearest mutual nodes on both sides
of the extended crack (Fig. 5).
In the second method, the process of obtaining stress distribution and locating the potential cracks are the same as
that of the first method. However, the way of crack extension
is different. In this method, to augment the crack length, the
cracked elements are physically removed from the model
and the resultant cohesive forces are applied on the crack
sides (Fig. 6).
Fig. 3 Flowchart of the proposed algorithm
4 Results and Discussion
4.1 Benchmark
𝜎 = 0,
for w ⩾ wc .
(3b)
To simulate the compressive behavior of concrete,
Hognestad model [35] has been used. Reinforcing bars
are assumed to have elastic-perfectly plastic behavior. To
implement the proposed algorithm, two different pathways
may be chosen. The main differences between these two
methods lie in the way that cracks are created and propagated and how the cohesive forces are applied. In what
follows, explanations of these methods are described.
Fig. 4 Linear tension-softening
function used in this research
13
To evaluate the proposed algorithm, the results of some
experimental tests on beams conducted by Bresler and
Scordelis [36] are compared with the predictions of the present model. These experiments are of high quality as well
as adequately documented, and have been used as benchmark in several analytical studies. The beams OA1 and A1
of the above-mentioned experimental set are considered
here. Both of them are simply supported under a single concentrated load at the mid-span. Beam OA1 has only longitudinal reinforcement, but A1 has both longitudinal and
International Journal of Civil Engineering
Fig. 5 Illustration of applying cohesive stresses in the first method
Fig. 7 Beam OA1 and A1 setup and details [36]
Fig. 6 Illustration of applying cohesive stresses in the second method
shear reinforcement. To impose the shear failure mode to the
beams, they are reinforced with high ratios of longitudinal
bars. The test setup and details are illustrated in Fig. 7. The
geometrical and mechanical properties of cross section, concrete, and reinforcement are included in Tables 1 and 2. The
maximum aggregate size used in the beams is 20 mm. The
beams were loaded by a monotonic load-control mechanism
at the mid-span.
4.2 Evaluation of the proposed methods
Based on the previously introduced Methods, two-dimensional non-linear finite-element analyses are performed to
study the load-deformation behavior and crack propagation of Bresler–Scordelis beams. FEM mesh is constructed
using smart adaptive meshing of ABAQUS [30] with threenode iso-parametric elements. Longitudinal and transverse
reinforcement are modeled in a discrete manner using wire
element. Tie constraints have been used to define interaction between concrete and reinforcing steel. A tie constraint
allows two regions to be bonded together, even though the
meshes created on the surfaces of the regions are dissimilar
[30]. The models are studied under load-control loading.
Figure 8 shows the comparison of the load–displacement
curves obtained by the proposed methods 1 and 2 with the
results of Bresler–Scordelis experiment. In addition, the
curve predicted by the well-known Modified Compression
Field Theory, MCFT, [37] is shown in this figure. It must
be pointed out that MCFT is a smeared rotating crack model
that underlies the shear design provisions of CSA [5] and
AASHTO [4]. Compression softening and tension stiffening
are considered in MCFT.
As shown in Fig. 8, for the both beams OA1 and A1, the
proposed methods 1 and 2 predict the complete load-deformation curve equally well, and give notably better predictions than that of MCFT [37]. In addition, the accuracy of
the predictions of MCFT deteriorates considerably for the
no-stirrup beam OA1. However, the presented methods have
uniform accuracy for both with and without stirrups cases.
Furthermore, it can be seen that among the proposed methods, the predictions of method 2 for the load-deformation
curve have more accordance with the test results. In Table 3,
the ultimate loads, Pu , calculated by methods 1 and 2, are
compared with those of experimental tests as well as MCFT.
According to Table 3, the proposed methods 1 and 2 yield
the ratio of test-to-predicted ultimate load for beam OA1
as 1.08 and 0.98, respectively, while MCFT has a ratio of
1.34 which shows its lack of accuracy. The corresponding
values for Beam A1 are 1.13, 1.11, and 0.93, respectively.
As shown in Table 3, the strength of A1 is overestimated by
MCFT, while the predictions of the proposed methods are
on the safe side.
In Table 4, the computational results for the mid-span
displacements at peak load, 𝛿0 , of the present study are
compared with those of experimental tests and MCFT [37].
According to this table, the ratios of prediction-to-experimental ultimate displacements for Beam OA1 are 1.03
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International Journal of Civil Engineering
Table 1 Cross-sectional
properties of Bresler–Scordelis
Beams [36]
Table 2 Material properties of
Bresler–Scordelis Beams [36]
Beam no.
b (mm)
h (mm)
d (mm)
L (mm)
Span (mm)
Bott. steel
Top steel
Stirrups
OA1
A1
310
307
556
561
461
466
4100
4100
3660
3660
4 No. 9
4 No. 9
–
2 No. 4
No. 2@ 210
Reinforcement
Concrete
Bar size
No. 2
No. 4
No. 9
Diameter (mm)
Area (mm2)
fy (MPa)
fu (MPa)
Es (MPa)
6.4
32.2
325
430
190,000
12.7
127
345
542
201,000
28.7
645
555
933
218,000
400
350
Load (kN)
300
250
200
150
Experiment
Proposed Method 1
Proposed Method 2
MCFT [37]
100
50
0
0
2
4
6
Displacement (mm)
8
10
(a)
600
500
Load (kN)
400
300
Experiment
Proposed Method 1
Proposed Method 2
MCFT [37]
200
100
2
4
6
8
10 12 14
Displacement (mm)
16
18
fr, MPa
OA1
A1
22.6
24.1
3.97
3.86
2, respectively, and 0.78 for MCFT. Thus, the predictions
of the present methods for ductility are more conservative
than that of MCFT.
Based on the foregoing results and discussion, it could
be concluded that the proposed algorithm for implementing
FCM in finite-element modeling yields acceptable results for
predicting non-linear load–displacement behavior of shearcritical beams. Furthermore, the proposed method 2 is more
accurate than method 1, at least for the studied samples. Of
course, more corroborative study is needed to make a more
reliable comparison.
To delineate the fracture mode of the beams, the calculated shapes of OA1 and A1 along with their estimated crack
patterns are illustrated in Fig. 9. In addition, for the sake of
comparison, their experimental crack patterns are shown in
Fig. 9. As the crack patterns of Bresler and Scordelis [36]
were not available, their replicates by Vecchio and Shim [37]
are used here, denoted by VS-OA1 and VS-A1. According
to Fig. 9, the predicted cracking patterns and failure modes
of the beams are in a good agreement with the experimental
ones.
20
(b)
Fig. 8 Comparison of experimental and predicted load-deformation
curves: a beam OA1, b beam A1
and 0.96 for methods 1 and 2, respectively, while the ratio
obtained by MCFT is 0.83. The corresponding values for
Beam A1 are 1.18 and 1.08 for the proposed methods 1 and
13
f′c, MPa
4.3 Verification of Proposed Algorithm
in Examination of Size Effect
0
0
Beam no
After the validation of the proposed algorithm, it can be
employed for analyzing large-scaled beams, and predicting shear strength of them. As the fictitious crack model
preserve fracture energy criterion, the proposed model is
expected to capture the size effect on shear strength of reinforced concrete beams [9–11, 27]. To examine the proposed
model in this respect, the large-scale test beams of Collins
and Kuchma [16] have been simulated by method 2, which
is already shown that it is generally better than method 1.
Details and test setup of these beams are depicted in Fig. 10.
International Journal of Civil Engineering
Table 3 Ultimate load obtained
by the present study, MCFT
[37], and the tests [36]
Table 4 Mid-span deflection at
peak load by the present study,
MCFT [37], and the tests [34]
Beam number
Pu (kN)
Pu-test/Pu-calc
Test [36]
MCFT [37]
Method 1
Method 2
MCFT [37]
Method 1
Method 2
OA1
A1
335
468
250
500
311
415
343
423
1.34
0.93
1.08
1.13
0.98
1.11
Beam number
𝛿0 (mm)
OA1
A1
𝛿0-test ∕𝛿0-calc
Test [36]
MCFT [37]
Method 1
Method 2
MCFT [37]
Method 1
Method 2
6.7
14.1
8
18.0
6.5
12.0
7.0
13.1
0.83
0.78
1.03
1.18
0.96
1.08
Fig. 9 Comparison of cracking patterns and failure modes: a experimental VS-OA1 [37], b calculated OA1, c experimental VS-A1 [37], d calculated A1 (D-T: diagonal tension, V-C: shear compression)
Fig. 10 Details and test setup of
large-scaled beams of Collins
and Kuchma [16]
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International Journal of Civil Engineering
The predicted load-deformation curves of the present
study are shown in Fig. 11. The test shear capacity and the
calculated shear capacity of the beams according to ACI
318-11 [3] and MCFT [16] are also shown in this figure. As
it can be seen in Fig. 11, shear capacities calculated based on
ACI provisions are not on the safe side owing to the exclusion of size effect from ACI relation. As MCFT includes
size effect in its relation, its predictions for large beams are
on the safe side. However, its accuracy is low. On the other
hand, the proposed model completely captures the dependence of shear strength on the size effect. In Table 5, the ultimate loads, Pu, of the proposed method 2 are compared with
those of experimental tests [16], MCFT [16] and ACI [3].
According to Table 5, the ratio of prediction-to-experimental
ultimate loads has a mean of 1.02 and covariance of 3.6%
for the proposed method 2 while these values for MCFT
600
600
ACI [3]
500
400
MCFT [16]
300
B100
200
100
ACI [3]
500
Test [16]
Load (kN)
Load(kN)
Fig. 11 Comparison of the
proposed method 2 predictions
with ACI [3], MCFT [16], and
the experimental results of
large-scaled test beams [16]
approach are 1.15 and 7.6%, and for ACI they are 0.80 and
7.9%, respectively.
As shown in Table 5, the strength of large beams containing no stirrups is significantly underestimated by ACI.
Among the mentioned test beams, B100B failed in a load
about 70% of the ACI value. The mentioned discrepancy
between real shear behavior of beams and ACI prediction
makes concerns on size effect especially for beams without
shear reinforcement. It must be mentioned that ACI permits
to design beams without stirrups if factored shear is less
than 0.5 Vc. In this regard, footings and slabs are designed
so they do not require stirrups. The difference between predicted values and test results reveals the fact that addition of
small amount of distributed reinforcement over the depth of
the member has remarkable effect on its shear capacity and
impedes sudden failures.
Proposed Method 2
Test [16]
400
MCFT[16]
300
200
B100B
100
proposed method2
0
0
1
2
3
Displacement (mm)
0
4
0
1
2
3
4
Displacement (mm)
500
Test [16]
400
300
200
Test [16]
400
MCFT [16]
300
200
B100D
100
ACI [3]
500
MCFT[16]
Load(KN)
Load (kN)
600
ACI[3]
600
B100L
100
proposed method2
0
Proposed Method 2
0
0
2
4
6
8
0
2
Displacement (mm)
Table 5 Ultimate load obtained
by the present study, MCFT
[16], ACI [3], and the tests [16]
Beam number
B100
B100B
B100D
B100L
Mean
CoV %
13
Pu (kN)
8
4
6
Displacement(mm)
Pu-test/Pu-calc
Test [36]
MCFT [37]
ACI [3]
Method 2
MCFT [37]
ACI [3]
Method 2
468
408
556
448
368
378
528
378
556
578
640
579
442
422
531
446
1.27
1.08
1.05
1.19
1.15
7.6
0.84
0.71
0.87
0.77
0.80
7.9
1.06
0.97
1.05
1.00
1.02
3.6
International Journal of Civil Engineering
5 Conclusions
This study examines diagonal cracking and shear behavior
of reinforced concrete beams subjected to concentric gravity
loads. The motive behind this study is the lack of multi-crack
analysis based on FCM in the literature. Using the ABAQUS
software, the classical finite-element method based on discrete crack approach is utilized for analysis. The behavior
of cracks is simulated based on fictitious crack model or
cohesive crack model. Due to limitations of the software
on direct analysis of multiple diagonal cohesive cracking,
a stepwise semi-automatic approach with two pathways of
implementation is proposed in which the outcomes of both
pathways were coinciding. The comparison of the predictions of the proposed method for reinforced concrete beams
with test results indicates satisfactory accuracy in the evaluation of the load-deformation and cracking pattern of the
beams. In addition, the proposed method demonstrates a
very good accuracy in simulation of the behavior of largescaled beams, and size effect phenomenon.
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