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Finite element analysis on steel–concrete–steel sandwich beams
Transcript of Finite element analysis on steel–concrete–steel sandwich beams
ORIGINAL ARTICLE
Finite element analysis on steel–concrete–steel sandwichbeams
Jia-Bao Yan
Received: 25 September 2013 / Accepted: 28 January 2014
� RILEM 2014
Abstract Steel–concrete–steel (SCS) sandwich
composite structure with J-hook connectors has been
developed and exhibited versatile potential applica-
tions in the building and offshore constructions. In this
structure, J-hook connectors were used to bond the
steel face plates and concrete as integrity. In this
paper, finite element model (FEM) by general finite
element program ABAQUS was developed to analyze
the nonlinear structural behavior of the developed SCS
sandwich beam structures with J-hook connectors
under quasi-static loading. In this FEM, the novel
J-hook connectors were simplified and simulated by
cylindrical studs linked by the nonlinear spring
element. The validations of the FEM cover from the
component to structure level. Firstly, the simulations
of the FEM on the longitudinal shear-slip and axial
tension–elongation behaviors of the J-hook connectors
were firstly validated against the push- and pull- out
tests. Then, the FE analysis (FEA) on the structural
behaviors of the SCS sandwich beams was validated
against those from the beam in the references.
Through these verifications, the accuracy of the FEA
on the nonlinear structural behaviors of the SCS
sandwich beam with J-hook connectors was
confirmed.
Keywords Finite element � Steel–concrete–
steel � Sandwich beam � Push-out � Ultimate
strength � Ultra-lightweight concrete � J-hook
1 Introduction
Steel–concrete–steel (SCS) sandwich composite struc-
tures consisting of two steel face plates and a
sandwiched concrete core becomes popular in recent
three decades due to their excellent cost to strength
performance. In SCS sandwich composite structures,
cohesive material e.g. epoxy or mechanical shear
connectors were common measures to bond the steel
and concrete together. Compared with the cohesive
materials, mechanical shear connectors exhibited
advantage in provision of transverse shear resistance
[1]. Many types of connectors have been developed for
SCS sandwich composite structures e.g. angle connec-
tors, C channel connectors, friction welded connectors
in ‘bi-steel’ structure, overlapped headed studs in
‘double skin’ structure, corrugated strip connectors,
and J-hook connectors as shown in Fig. 1 [2]. SCS
sandwich composite structures with J-hook connectors
(see Fig. 2) have advantages of no limitation on the
thickness of the structure, allowing prefabrication in the
factory, easy fabrication, saving site construction time
and formwork of concrete casting, relative high strength
under static, impact and fatigue loadings [3–5]. This
type of SCS sandwich composite structure exhibited
J.-B. Yan (&)
Department of Civil and Environmental Engineering,
National University of Singapore, E1A-07-03,
1 Engineering Drive 2, Singapore 117576, Singapore
e-mail: [email protected]
Materials and Structures
DOI 10.1617/s11527-014-0261-3
versatile potential applications as the submerged tun-
nels, shear walls and floors in the high rise building,
bridge and offshore deck, protection structures, oil
storage tank, ship hulls, nuclear plant towers, and ice
walls in the arctic offshore structure [6].
Since the SCS sandwich composite structures with
J-hook connectors was developed, experimental studies
and analysis on this type of structures have been carried
out to obtain more information on their structural
performances [3–5]. Among the analysis methods,
numerical method especially the finite element (FE)
method is a very useful mean. Though there was less
information on FE analysis (FEA) on J-hook connec-
tors, there were still some related works on other forms
of SCS sandwich structure. A two-dimensional FE
model was developed for bi-steel beams [7]. However,
this FE model was two-dimensional that limited the
simulation of the connector–concrete interaction that
usually was three-dimensional (3D) and significantly
influenced the shear strength of the connector. Another
simplified FE model was developed for the ‘double
skin’ structure with overlapped headed shear studs [8].
In this model, the concrete core with headed shear studs
was simplified to a homogeneous anisotropic material
(a) Angle connector (b) C channel connector (c) overlapped headed stud
(d) Friction welded connector (e) Corrugated-strip connector (f) J-hook connector
Fig. 1 Sandwich composite structure with different shear connectors
(a) SCS sandwich beam with J-hook connector
(b) Curved SCS sandwich structure with J-hook
Fig. 2 SCS sandwich
structure with J-hook
connectors
Materials and Structures
with enhanced shear strength contributed by the
connectors. This simplification significantly reduces
the difficulty of modeling the overlapped shear con-
nectors in the concrete core and reduces the total
amounts of the elements. However, this simplified FE
model cannot simulate the structural behavior of the
connectors in the SCS sandwich beam structure.
Nonlinear spring elements were also used in the FE
model to replace the headed stud connectors and
connect the concrete slab and I-beam in steel–concrete
composite structure [9]. However, this simplification
could not reflect the interaction between the connector
and the concrete, and underestimates the transverse
shear strength of the structure. In SCS sandwich
composite structure with J-hook connectors, the con-
nectors that work in pairs and interlock each other are
used to transfer longitudinal shear force, resist trans-
verse shear force, and prevent local buckling of the steel
face plates. Since their roles in SCS sandwich structures
are such important, it is of importance to capture their
structural behaviors in the FEA. From the above
literature review, all these developed FE models have
limitations on properly simulate the concrete–connector
interactions [7–9]. Moreover, the complex geometry of
the J-hook connectors also brings challenges to the FEA
of the SCS sandwich beams.
In this paper, a 3D FE model by general commercial
FE program ABAQUS was developed to simulate the
structural behavior of the SCS sandwich beam under
quasi-static loading. In this FE model, as the basic
component of the SCS sandwich structure, structural
behaviors of one pair of interlocked J-hook connectors
were firstly simulated. FE simulations on these basic
structural behaviors of the J-hook connectors i.e. the
longitudinal shear-slip and axial tension–elongation
behaviors were first evaluated by the push-out tests and
tensile tests on a pair of J-hook connectors. Followed,
from the structure level, the accuracy of the FE model
was checked through validations against twenty beam
tests. Through these validations, the accuracy of the FEA
was confirmed. These works in this report extend the
studies and provide useful analysis method on the SCS
sandwich composite beams with J-hook connectors.
2 Finite element model
This finite element model includes (1) modeling the
basic component of the SCS sandwich structure with
J-hook connectors that will be validated by the push-
out tests and tensile tests on a pair of J-hook
connectors, and (2) modeling the SCS sandwich beam
with J-hook connectors.
The ABAQUS CAE and standard type of implicit
solver were used for model building and FEA solution.
2.1 Description on the basic behaviors
of the J-hook connector
J-hook connectors in the SCS sandwich structure play
essential roles such as transferring longitudinal shear
force at the steel–concrete interface, providing trans-
verse shear force through linking the shear cracks in
the concrete, and preventing uplifting and local
buckling of the steel face plates (see Fig. 3). There-
fore, the FE model should properly capture these
structural behaviors. The first characteristic structural
behavior is the longitudinal shear behavior. Generally,
push-out tests are used to obtain the ultimate shear
strength and shear-slip behaviors of the J-hook con-
nectors [6]. The second structural characteristic of the
J-hook connectors is the axial tension behavior. This
behavior can be obtained through direct tensile test. In
this study, the push-out tests and tensile tests carried
out by the authors were used to validate the FE model.
2.2 Modeling of J-hook connector
For a pair of interlocked J-hook connectors, it is very
difficult to make a full geometry simulation due to
their complex geometry. A full geometry simulation
will lead to mesh and contact simulation difficulties
that probably terminate the FEA prematurely devel-
oped. Moreover, it will also lead to a great deal of
elements that proves to be time costing and reduce the
computing efficiency. In this paper, a pair of J-hook
connectors was simplified to two cylindrical stud
connectors linked by a nonlinear spring element as
shown in Fig. 4. A small gap of 5 mm is reserved
between these two cylindrical studs for facilitating the
modeling of spring element. The tension–elongation
behavior of the J-hook connectors obtained from the
tensile tests was used to define tension–elongation
behavior of the nonlinear spring element. The defini-
tion of the tension–elongation relationship of spring
cannot be realized through editing the Unicode in the
input program with the values of the tension–elonga-
tion relationship.
Materials and Structures
In the longitudinal direction, the cylindrical studs
were built with the same diameter and similar
embedding depth as the real J-hook connectors in the
SCS sandwich beams. From the Eurocode 4 [10], it
can be well known that the shear strength of the
connectors are determined by the following
PJ ¼ min 0:8fu
pd2
4cv
; 0:29ad2ffiffiffiffiffiffiffiffiffiffi
fckEc
p
=cv
� �
; ð1Þ
where d is the diameter of the stud shank, fu is the
ultimate tensile strength of the stud (B500 MPa), fck is
the characteristic cylinder strength of concrete, Ec is
the secant modulus of concrete, a = 0.2(hs/d ? 1) for
3 B hs/d B 4 or a = 1.0 for hs/d C 4; hs = overall
height of the stud. The recommended value for the
partial safety factor cv is 1.25.
From Eq. 1, it can be seen that the shear strength of
the connectors were determined by both material
properties and geometry that include the diameter and
height of the stud. Therefore, in many FE models as
aforementioned [7–9], the simplifications may not
properly capture this structural behavior and cannot
correctly estimate the connector’s shear strength. In
this paper, the simplified method can simulate the
(a)
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J-
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ook
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ear
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ding
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uck
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caluckl
sver
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rse she
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ear res
C
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istaance
T
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Fig. 3 Functions of the J-hook connectors in SCS sandwich structure
Materials and Structures
closest geometry to shear connectors in terms of height
and diameter compared with other developed FE
models.
In the axial direction of the connector, the axial
tension–elongation behaviors from the direct tensile
tests were used to define the nonlinear spring element.
Thus, this characteristic of the J-hook connectors was
simulated.
2.3 Description of finite element model
In order to simulate the SCS sandwich beam structure
with J-hook connectors from the component to
structure level, the FE model includes the simulation
on the push-out and tensile tests, and the simulation on
the SCS sandwich beam.
2.3.1 FE model for the push-out test
In the push-out test, the main components were steel
face plates, shear connector, concrete core, and load
cell as shown in Fig. 5. All these components were
modeled by the 3D eight-node continuum element
(C3D8R). For a pair of interlocked J-hook connectors,
nonlinear spring element is used to simplify its
complex geometry as shown in Fig. 5. Considering
the symmetry of the structure and loading, only half of
the specimen was built in the FE model. At the
conjunction between the connectors and the steel face
plates and contacting locations between the connector
and concrete core, fine mesh sizes were used to make a
better simulation as shown in Fig. 5.
2.3.2 Finite element model for the SCS sandwich
beams
Different components of the SCS sandwich beams were
built in the developed FE model, which include steel face
plates, shear connectors attached to the steel plates,
support, load cells, and concrete core (as shown in
Fig. 6). Considering the symmetry of the geometry and
loading patterns, one quarter of the full specimen was
modeled. Three-dimensional eight-node linear contin-
uum element with hourglass control was used for steel
face plates, connectors, and concrete core. Nonlinear
spring elements were also used to simulate the axial
tension–elongation behavior of the interlocked J-hook
connectors in the SCS sandwich beam as shown in Fig. 4.
In order to balance the computing accuracy and
efficiency, different mesh sizes were used for the SCS
sandwich beams at different locations. Considering
the interaction between the steel connectors and
concrete core, fine mesh size was used at the
contacting locations between the connectors and
concrete. Typical mesh sizes for the SCS sandwich
beam were shown in Fig. 6.
2.4 Material modeling of concrete and steel
There are mainly two types of materials were involved
in this FEA i.e. steel and concrete.
NelNonlem
lineent
ear t
sprringg
Fig. 4 Simulation of a pair of interlocked J-hook connectors in
FE model
Steel face plate
Steel face plate
Connector
Load cell
Symmetrical surface
Movement restraint Ux=Uy=Uz=0
Displacement loading
Fig. 5 Finite element model for the push-out test
Materials and Structures
2.4.1 Concrete
In ABAQUS material library, the concrete damage
plasticity model was used for the concrete core
materials in the SCS sandwich composite beams.
The concrete damage model is a continuum, plasticity-
based, damage model. In this model, the assumed two
main failure mechanisms are compressive crushing
and tensile cracking of the concrete. The yield
function proposed by Lubliner et al. [11] and modified
by Lee and Fenves [12] was adopted to account
different evolution of strength under tension and
compression. The isotropic damage and non-associ-
ated potential flow rule was assumed in this model
[13]. Considering the concrete damage material model
with softening behavior and stiffness degradation
often lead to severe convergence difficulties in
implicit analysis programs, in Abaqus/Standard type
of program, the viscoplastic regularization of the
constitutive equations is used to improve the conver-
gence rate in the softening regime.
For concrete damage plasticity model, two failure
mechanisms including tensile cracking and axial
compressive crushing were needed to be defined. In
this FEA, different types of concretes were used i.e.
normal weight concrete (NWC), lightweight concrete
(LWC), and ultra-lightweight cement composite
(ULCC). For the LWC and ULCC, the compression
and tension behaviors of the concrete materials were
obtained through compression and splitting tests on
the concrete cylinders according to ASTM [14, 15].
The compressive stress–strain curves of the LWC and
ULCC obtained from the compression tests on the
cylinders are shown in Fig. 7. The stress–strain curve
suggested by Carreira and Chu [16] was used to model
the elastic–plastic characteristics of the NWC with
strain softening as the following:
rc ¼fckb ec=eckð Þ
b� 1þ ec=eckð Þb; ð2Þ
where rc is the compressive stress of the concrete, ec is
the compressive strain of the concrete, fck is the
compressive strength of the concrete cylinder, eck is the
compressive strain at fck is the b is a function of secant
modulus of elasticity Ec that can be determined by
b ¼ 1 ec=eckð Þ1� fck= eckEcð Þ : ð3Þ
Other plasticity parameters including dilation angle
of 36�, flow potential eccentricity of 0.6, and ratio of
Steel face plate
Load cell
Support
Concrete core
Holes cut for connector
Support
Connector Steel face plate
Load cell
Steel face plate Symmetrical surface Uz=0
Symmetrical surface Ux=0
Movement Restrained
Displacement Loading
Fig. 6 Finite element model for SCS sandwich beam
Materials and Structures
the biaxial/uniaxial compressive strength ratio of 1.16
were set for this plastic damage model according to the
ABAQUS user manual [13].
For the tension capacity of the core material, linear
elastic tensile behavior is assumed before the cracking
in the concrete develops. The cracked concrete can be
simulated by the nonlinear stress–strain behavior or
fracture energy cracking model. The ultimate tensile
strength of the ULCC was obtained through the
splitting tensile tests on the cylinders. For the fracture
energy parameter, it can be determined by the
following equation in CEB-FIP [17]
Gf ¼ Gf0
fck
10
� �0:7
; ð4Þ
where Gf is the fracture energy, Nmm/mm2, Gf0 varies as
the coarse aggregate of the concrete changes,
Gf0 = 0.025 Nmm/mm2 for the d = 8 mm coarse aggre-
gate, Gf0 = 0.030 Nmm/mm2 for the d = 16 mm,
Gf0 = 0.058 Nmm/mm2 for the d = 32 mm; d is the
diameter of the coarse aggregate in the concrete, mm, fck
is the compressive strength of the concrete cylinder, MPa.
Since ULCC is a new material and there is no test data
available on the fracture energy, a smallest value
Gf0 = 0.0025 Nmm/mm2 is used for ULCC consider-
ing there is no coarse aggregate in it, and Gf =
0.088 Nmm/mm2 is used in the tensile behavior of the
plastic material model for the ULCC. For the NWC used
in the SCS sandwich beams, Gf0 = 0.060 Nmm/mm2
was used for the d = 18 mm coarse aggregate, and
Gf = 0.18 Nmm/mm2 was used. For LWC used in the
sandwich composite beam, Gf = 0.060 Nmm/mm2
was used in the FEA.
2.4.2 Steel
A nonlinear isotropic/kinematic hardening model with
Mises yield surface for the definition of isotropic
yielding in ABAQUS material library was used for
steel material [13]. This stress–strain behavior defined
in this model was bi-linear with strain hardening as
shown in Fig. 8. For the elastic behavior of the steel
material, the elastic Young’s modulus Es and Pois-
son’s ratio were needs to be defined. For the plastic
behavior, the yield strength, ultimate strength and the
corresponding strains were needs to be defined.
For these material properties including the elastic
Young’s modulus, yield strength, ultimate strength
and the corresponding strains were obtained from the
tensile tests on the steel coupons.
The elastic Young’s modulus of 205 GPa and yield
strength 275 MPa were used for the sandwich beams
in the Group A and beam J1 in Group B as shown in
Table 1. For the steel plates in the SCS sandwich beam
in Group B, elastic Young’s modulus of 205 GPa and
yield strength 310 MPa were used for the beams in
Group B except J1 in Table 1. For the J-hook
connectors, the same material properties were used
as the steel plates as listed above.
2.5 Boundary, loading, interactions, and solutions
In the push-out tests, the bottom end of the steel face
plates were restrained against moving in the any
directions as shown in Fig. 5. From this figure, it can
be seen than the rotation restrained in the Y and
Z directions and movements in the X direction were
applied to the symmetrical surface. In the LOAD
menu of the ABAQUS CAE modeling, displacement
controlled type of loading was applied to the load cell.
0
10
20
30St
ress
(M
Pa)
Strain
LWC C300
25
50
75
0 0.001 0.002 0.003 0 0.003 0.006 0.009
Stre
ss (
MP
a)Strain
ULCC C60
Fig. 7 Compressive stress–strain curves of LWC and ULCC
Fig. 8 Stress–strain model for the steel material
Materials and Structures
For the beam tests, symmetrical restraints were
applied to the cross section as shown in Fig. 6. The
support was restrained from moving but free in
rotation. Displacement controlled type of loading
was applied to the SCS sandwich beam through the
load cell by setting the Load Menu in the ABAQUS
library.
The contact between the concrete and steel face
plates in push-out and beam tests is simulated by the
general contact with ‘‘hard formulation’’ in the normal
direction and ‘‘penalty friction formulation’’ in the
tangential direction. The hard formulation in the
‘‘Interaction’’ menu of ABAQUS library means that
the pressure will be transferred once two interacting
surfaces contact whilst no pressure will be transferred
when they are separated. The penalty friction formu-
lation permits relative slip between the two contacting
surfaces and the interacting friction force is
proportional to the defined friction coefficient. This
contact permits the two contacting surface separating
but not allows penetrating each other. Friction coef-
ficient is taken as 0.4 as in the previous FE studies
carried out by Yan [2]. For the push-out tests, the
‘‘hard contact’’ formulation and ‘‘penalty friction
formulation’’ were also used to define the interactions
in normal and tangential directions respectively at the
steel face plate and concrete interface, interface of
concrete and load cell in the push-out tests. ‘‘Hard
contact’’ formulation was used in the normal direction
to the interface between the connectors and the
concrete core and in the tangential direction along
this interface no contact was defined for both push-out
tests and beam tests. For the beam tests, ‘‘hard
contact’’ formulation and ‘‘penalty friction formula-
tion’’ were also used to define the interactions in
normal and tangential directions respectively at the
Table 1 Details of the SCS sandwich beam
Beam tc and tt(mm)
hc
(mm)
B
(mm)
D
(mm)
S
(mm)
Core Vf
(%)
w (kg/
m3)
fck
(MPa)
fy(MPa)
ru
(MPa)
Group A
SCS 80 4.0 80 240 10 80 NWC – 2,350 48.3 275 405
SLSC80 4.0 80 240 10 80 LWC – 1,445 28.5 275 405
SCS 100 4.0 80 200 10 100 NWC – 2,350 48.3 275 405
SLCS100 4.0 80 200 10 100 LWC – 1,445 28.5 275 405
SLFCS100 4.0 80 200 10 100 LWC 1S? 1,450 28.1 275 405
SCS150 4.0 80 300 10 150 NWC – 2,350 48.3 275 405
SLCS150 4.0 80 300 10 150 LWC – 1,445 28.5 275 405
SLCS200 3.9 80 200 16 200 LWC – 1,445 27.4 275 405
SLF200-1 3.9 80 200 16 200 LWC 1P? 1,450 28.7 275 405
SLF200-2 3.9 80 300 16 200 LWC 2P? 1,450 28.2 275 405
SLF300-1 3.9 80 200 16 300 LWC 1P? 1,450 28.0 275 405
Group B
J1 4.0 100 200 12 100 ULCC 0.5 P? 1,441 60.0 275 460
J2-1 6.0 100 200 12 100 ULCC 0.5 P? 1,450 60.0 310 460
J2-2 6.0 100 200 12 100 LWC – 1,324 24.0 310 460
J2-3 6.0 100 200 12 100 HPC – 2,672 160 310 460
J3 12.0 100 200 12 100 ULCC 0.5 P? 1,481 60 310 460
J4 6.0 100 200 12 150 ULCC 0.5 P? 1,521 60 310 460
J5 6.0 100 200 12 200 ULCC 0.5 P? 1,440 60 310 460
J6 6.0 100 200 12 100 ULCC 0.5 P? 1,481 60 310 460
J7 6.0 100 200 12 100 ULCC 0.5 P? 1,482 60 310 460
tc thickness of the steel plate under compression, tt thickness of the steel plate under tension, B width of the beam cross section,
D diameter of the J-hook, S spacing of the connector, w density of the concrete, Vf volume fraction of the fibre in the concrete, fy yield
strength of the steel plate, fck compressive strength of the concrete cylinder, ru ultimate strength of J-hook connector, S? denotes steel
fiber, P? denotes polyvinyl alcohol fiber
Materials and Structures
interface between concrete and steel plate, interface
between load cell and top steel face plate, and interface
between bottom steel face plate and support; ‘‘hard
contact’’ formulation was used in the normal direction
between the connectors and the concrete core and in
the tangential direction no contact was defined.
Abaqus Standard type of implicit solver was used for
the solution. Numerous control parameters are associ-
ated with the convergence criteria in Abaqus/Standard
for the solutions. Usually there are default values set to
optimize the accuracy and efficiency of the solution for
a wide spectrum of nonlinear problems. For the
convergence criteria, solution control parameters can
be used to define tolerances for field equations such as
force and moment. For the contact, the contact stresses
and contact displacements were selected for the field
equations of convergence criteria.
3 Push-out tests, tensile tests and SCS sandwich
beam tests
The push-out tests and SCS sandwich beams tests
carried out by the authors were used in this study for
the validation of the FE model.
3.1 Push-out tests
Twelve push-out tests were used to validate the FE
model. The setup of the push-out tests and the geometry
illustration are shown in Fig. 9. The details of the
specimens are listed in Table 2. In the push-out test, a
pair of interlocked J-hook connectors embedded in the
concrete block was pushed off under the quasi-static
interfacial shear forces as shown in Fig. 9. As shown in
this figure, the displacement controlled type of loading
was applied to the concrete core through the load cell,
and then this load will be taken by a pair of J-hook
connectors. The load obtained from the test will be
equal to two times the shear strength of single J-hook
connectors. Linear varying displacement transducers
(LVDTs) were used record the interfacial slip between
the concrete and the steel face plate. Finally, the shear
force versus slip of each specimen was recorded.
3.2 Tensile tests
Tensile tests on the J-hook connectors were also
carried out to obtain the axial tension–elongation
behavior of the J-hook connectors in different concrete
mixtures. The test setup is shown in Fig. 10. As shown
in this figure, a pair of the interlocked J-hook
connectors was embedded in the concrete that was
confined by a steel tube. This steel tube was used to
simulate the confinement of the neighbor concrete in
the structure. The tensile forces was applied to the
specimen and transferred to the J-hook connectors.
The tensile strength as well as the tension–elongation
behaviors of the J-hook connectors can be obtained
that can be used for the validation of the FE mdoel.
3.3 Quasi-static tests on SCS sandwich beams
The SCS sandwich beams with J-hook connectors
subjected to one- or two- point loading were used in
this paper to check the accuracy of the FEA [14, 15].
The beams in Ref. [15] were designed with a span of
1,000 mm under one-point loading. The geometry and
setup of the beam test is shown in Fig. 11a. LWC that
was made of both coarse and fine aggregates was used as
the main core material. NWC was also used in three
specimens. Steel or polyvinyl alcohol (PVA) fibers were
used in four specimens. The details of these SCS
sandwich beams are illustrated in Table 1 (Group A
beams).
The sandwich beams in Ref. [4] were tested under
one- or two- point loading. SCS sandwich beam J1–J5
were set a span of 500 mm and subjected to one-point
loading at the mid-span; beam J6 and J7 that were tested
under two-point loading were designed with spans of
1,100 and 1,600 mm, respectively (see Fig. 11). All the
beams were designed with the same cross section (with
height of core = 100 mm and width 200 mm). The
ULCC was used as the main core materials. LWC and
high performance concrete were used in beam J2-2 and
J2-3, respectively. The test setup and geometry of the
SCS sandwich beams were shown in Fig. 11. The
material properties and details of the SCS sandwich
beams were listed in Table 1 (Group B beams).
4 Validation of the FE model
4.1 Validation of the FE model against push-out
and tensile test
By the recommended FE model, FE analyses (FEA) on
push-out tests were carried out. The validations of the
Materials and Structures
FEA consist of validation of shear force-slip curves of
the J-hook connectors, ultimate shear strength, and
failure mode.
4.1.1 Shear force-slip curves of push-out test
The shear force-slip curves obtained from FEA were
compared with the experimental ones in Fig. 12. From
these figures, it can be seen that the load-slip curves by
the FEA show good agreements with the experimental
curves in terms of initial elastic stiffness, threshold of
the plastic behavior initializing, and nonlinear load-
slip behaviors. In some specimens, there is still some
mismatch of load-slip curves between the FEA and the
experimental ones at the nonlinear part e.g. load-slip
curves of PU2 and PU3. These discrepancies may be
caused by the splitting of the concrete that cannot well
be simulated in the FE model. For PU2, splitting
failure occurred to the concrete core which prevented
the specimen continuing taking more loads. However,
in the FEA, the specimen failed in the shear off of the
connector, and no splitting failure was observed.
LVDT
Steel face plate
Steel face plate
Load cell
J-
Co
hook
ncrete core
Fig. 9 Push-out test on
specimens with J-hook
connectors
Table 2 Details of push-out test on sandwich specimens with J-hook
Item t (mm) d (mm) hc (mm) hs (mm) B (mm) ru (MPa) fck (MPa) Ec (GPa) w (kg/m3) hc
d
PN1 6 9.9 40 49.9 300 405 48.3 32.5 2,400 4.04
PN2 6 11.8 75 90.5 250 480 47.7 24.0 2,343 6.36
PN3 6 11.7 75 90.5 250 450 34.1 19.5 2,329 6.41
PL1 6 9.9 40 49.9 300 405 28.5 12.7 1,450 4.04
PL2 6 11.7 75 90.5 250 450 51.2 18.0 1,874 6.41
PL3 6 11.7 75 90.5 250 450 51.2 18.0 1,874 6.41
PL4 6 11.7 100 120 250 480 51.2 18.0 1,874 7.50
PLF1 6 9.9 40 49.9 300 405 28.1 12.6 1,460 4.04
PU1 4 11.8 50 61.8 250 464 60.0 16.5 1,490 4.24
PU2 6 11.8 50 61.8 250 464 60.0 16.5 1,440 4.24
PU3 8 11.8 50 61.8 250 464 60.0 16.5 1,440 4.24
PU4 12 11.8 50 61.8 250 464 60.0 16.5 1,440 4.24
PU5 6 11.8 75 86.8 250 464 60.0 16.5 1,440 6.36
PU6 6 11.8 100 111.8 250 464 60.0 16.5 1,440 8.47
Materials and Structures
4.1.2 Ultimate shear strength and failure mode
of push-out test
The ultimate shear strengths of the J-hook connectors
obtained from the FEA are compared with the shear
strengths obtained from the push-out tests in Table 3.
From this table, it can be observed that the average
test-to-prediction ratio of the ultimate shear strength
for the fourteen push-out tests is 1.00 with a coefficient
of variance (COV) of 0.05. This implies ultimate shear
strengths of the J-hook connectors attained from the
FEA agree well with the experimental results. In
Eurocode 4, Eq. 1 was used to predict the shear
strength of the connectors. The predictions by Eq. 1
In-filled concrete
Steel plate
J-hook
T
T
Steel plate
Steel tube
e
T
T
Fig. 10 Tensile test on a pair of interlocked J-hook connectors
(a) Test setup and details of sandwich beams in group A
(b) Test setup and details of sandwich beams in group B
P
A
A
A-A
t t
tc
P
P
B
B
B-B
B
B
CL
P
B
B
J1-5 J6
t t
tc
Fig. 11 Test setup and details of the SCS sandwich beams
Materials and Structures
are given in Table 3. From this table, it can be also
seen that the Eq. 1 offers about 20 % average
underestimations on shear strength of the J-hook
connectors. Both Eq. 1 and FEA exhibit close COV of
the predictions on these fourteen push-out tests.
Unfortunately, FEA method shows advantages of
describing both the linear and nonlinear shear-slip
behaviors over the analytical model.
There were two types of failure modes that were
observed from the push-out test i.e. shank shear failure
(SS) and concrete cracking failure (CC) [6]. The
predicted failure modes by the FE model were
compared with the failure modes observed from the
push-out tests in Table 3. From this table, it can be
found that the FEA predicts about 80 % correct failure
modes compared with the observed failure modes
during the test. The 20 % error predictions on failure
mode may be caused due to the concrete splitting of
the specimens that might be caused by the even
distribution of the shear loads on the concrete core
(c)(b)(a)
0
20
40
60
80
Loa
d (k
N)
Slip (mm)
PN1 TestPN1 FE
0
30
60
90
120
Loa
d (k
N)
Slip (mm)
PN2 TestPN2 FE
0
20
40
60
0 2 4 6 8 10 0 2 4 6 8 0 2 4 6 8
Loa
d (k
N)
Slip (mm)
PL1 TestPL1 FE
(f)(e)(d)
(i)(h)(g)
(l)(k)(j)
0
40
80
120
Loa
d (k
N)
Slip (mm)
PL2 TestPL3 TestPL2-3 FE
0
40
80
120
Loa
d (k
N)
Slip (mm)
PL4 TestPL4 FE
0
20
40
60
Loa
d (k
N)
Slip (mm)
PLF1 TestPLF1 FE
0
25
50
75
100
Loa
d (k
N)
Slip (mm)
PU1 Test
PU1 FE0
25
50
75
100
Loa
d (k
N)
Slip (mm)
PU2 TestPU2 FE
0
25
50
75
100
Loa
d (k
N)
Slip (mm)
PU3 TestPU3 FE
25
50
75
100
Loa
d (k
N)
Slip (mm)
PU4 Test
PU4 FE0
30
60
90
120
Loa
d (k
N)
Slip (mm)
PU5 Test
PU5 FE0
30
60
90
120
0 2 4 6 8 0 3 6 9 12 0 4 8 12
0 2 4 6 8 0 2 4 6 0 2 4 6
00 2 4 6 0 3 6 9 0 4 8 12
Loa
d (k
N)
Slip (mm)
PU6 TestPU6 FE
Fig. 12 Comparisons of
shear-slip curve between the
tests and FEA
Materials and Structures
material during the tests. Figure 13 shows the com-
parisons of the SS and CC failure modes between the
FEA and the experimental failure mode. The principle
plastic strain contours of the FEA were used to assist
judging of the failure in these two materials. Once the
lower limit of the cracking strain for the steel or
concrete were set, the cracking developed in the
elements can be judged if the strains in these elements
exceed this limit. For the limit of the steel cracking
strain herein is set as 0.30, and this value for the
concrete is set as 0.035. From Fig. 13, it can be seen
that these two failure modes can be well simulated by
the FE model.
4.1.3 Tension–elongation behavior of the tensile test
The other important characteristic behavior of the
J-hook connector is the axial tension versus elongation
behavior. The experimental tension–elongation behav-
iors of the J-hook connectors are compared with the
FEA in Fig. 14 (The details of the tensile tests are listed
in Table 4). From this figure, it can be seen that the
introduced spring element can capture the tension–
elongation behavior of the J-hook connectors in the
sandwich structure.
4.2 Validation of the FE model against SCS
sandwich beam test
By the recommended FE model, FE analyses were
carried out on the SCS sandwich beams under quasi-
static loading.
4.2.1 Deformed shape
The deformed shape of the SCS sandwich beams
under one- or two- point loading obtained from the
tests were compared with the deformed shape of the
sandwich beam obtained from the FEA at the same
loading levels in Fig. 15. From these figures, it can be
seen that developed FE model is capable of describing
the deformations of the sandwich beam with J-hook
connectors though there are some mismatches. These
differences may be caused by the soft support
problem.
4.2.2 Ultimate strength and failure mode
The ultimate strength and failure modes by the FEA
were compared with those by experimental results in
Table 5. From this table, it can be seen that the
Table 3 Comparisons of the ultimate shear strength of the J-hook connectors
No. Item PTest (kN) Test failure mode PFE (kN) FE failure mode PTest
PFEPa by Eq. 1 (kN) PTest/Pa
1 PN1 31.0 SS 31.6 SS 0.98 24.9 1.24
2 PN2 47.2 SS 50.4 SS 0.94 42.0 1.12
3 PN3 36.4 CC 37.5 CC 0.97 32.4 1.12
4 PL1 20.9 CC 21.1 CC 0.99 17.1 1.22
5 PL2 41.4 CC 42.3 SS 0.98 38.1 1.09
6 PL3 45.5 SS 42.3 SS 1.08 38.1 1.19
7 PL4 48.3 SS 49.1 SS 0.98 38.1 1.27
8 PLF1 22.6 SS 23.0 SS 0.98 16.9 1.34
9 PU1 46.8 SS 45.7 SS 0.98 40.2 1.16
10 PU2 42.1 CC 45.6 SS 1.09 40.2 1.05
11 PU3 44.2 CC 46.7 SS 1.06 40.2 1.10
12 PU4 48.6 SS 48.2 SS 0.99 40.2 1.21
13 PU5 51.2 SS 53.8 SS 1.05 40.2 1.27
14 PU6 51.7 SS 50.6 SS 0.98 40.2 1.29
Mean 1.00 1.19
Cov 0.05 0.07
SS shank shear failure, CC concrete cracking
Materials and Structures
predicted ultimate strength by FEA agree well with the
experimental ultimate strengths with an average test-
to-prediction ratio 0.99 and a COV 0.06. With regards
to the failure mode, it can be seen that the FE model
can offer 95 % correct predictions except on beam
SCS100. Nevertheless, the FE model shows advanta-
ges on observing the connector shear failure (CSF)
that was usually difficult to observe due to the
connectors were invisible in the embedded concrete.
It can be also found that the connectors failed in
vertical shear (VSF) for most of the beam tests as listed
in Table 5. Because, for the beams failed in VSF, the
connectors were under the most critical working state
i.e. under combined shear and tensile loads. It is thus
can be concluded from the comparisons of the ultimate
strengths and failure modes that the developed FE
Test SS failure mode
Back viewFE SS failure mode
(a) Shank shear failure of the connector (SS)
Splitting crack of the FE
Splitting crack observed in the test
(b) Concrete cracking failure mode (CC)
Back View
Fig. 13 Comparison of failure mode between the test and FEA
0
10
20
30
Ten
sion
(kN
)
Elongation (mm)
FE TU1TU2 TU3TU4 TU5
0
10
20
30
0 10 20 30 0 10 20 30
Ten
sion
(kN
)
Elongation (mm)
TN1 TestTN1 FETL1 TestTL1 FE
Fig. 14 Validation of the tension–elongation behavior of the
J-hook connector
Materials and Structures
model is capable of predicting the ultimate load
carrying capacities as well as failure modes of the SCS
sandwich beams with J-hook connectors.
4.2.3 Load–central deflection curves
The load versus central deflection curves of the SCS
sandwich beam by the FEA were compared with the
experimental curves in Fig. 16. From these figures, it
can be seen that most of the predicted load–central
deflection curves resembles well with the test curves in
terms of linear and nonlinear behaviors. However, it
was also observed that the elastic stiffness of the load–
deflection curves by the FEA was somehow smaller
compared with the test curves. These differences in the
elastic stiffness of sandwich beams may be caused by
the soft support of the beam test. Except these
differences of the elastic stiffness, the FEA provides
good agreements on the ultimate strength and nonlin-
ear load–deflection behaviors of the beam.
Table 4 Details of the tensile test specimens
Specimen t (mm) hs (mm) hc (mm) d (mm) Fiber by volume ry (MPa) ru (MPa) fck (MPa) Material type
TN1 6 58.8 100 11.8 – 310 480 47.7
TL1 6 56.3 95 11.8 – 310 465 30.0 LWC
TU1 6 56.3 95 11.8 310 465 65.2
TU2 6 71.3 125 11.8 310 465 65.2
TU3 4 57.3 95 11.8 310 465 65.2
TU4 8 55.3 95 11.8 0.50 % 310 465 65.2 ULCC
TU5 12 53.3 95 11.8 310 465 65.2
TU6 6 60.5 95 16.0 280 405 65.2
NWC denotes normal weight concrete, NWFC denotes normal weight concrete with fibers, LWC denotes light weight concrete, LWFC
denotes light weight concrete with fibers, ULCC denotes ultra-lightweight cement composite
(a) Beam J2-3
0
1
2
3
0 100 200 300 400 500
Def
lect
ion
(mm
)
Distance (mm)
150 kN FE 150 kN Test220 kN FE 220 kN Test270 kN FE 270 kN Test
J2-3
(b) Beam J4 (c) Beam J5
0
2
4
6
8
0 100 200 300 400 500
Def
lect
ion
(mm
)
Distance (mm)
115 kN FE 115 kN Test150 kN FE 150kN Test200 kN FE 200 kN Test
J4
0
0.5
1
1.5D
efle
ctio
n (m
m)
Distance (mm)
50 kN FE 50 kN Test80 kN FE 80 kN Test100 kN FE 100 kN Test
J5
0 100 200 300 400 500
(d) Beam J6
0
4
8
12
0 200 400 600 800 1000
Def
lect
ion
(mm
)
Distance (mm)
50 kN FE 50 kN Test100 kN FE 100 kN Test150 kN FE 150 kN Test
J6
(e) Beam J7
0
4
8
12
0 400 800 1200 1600
Def
lect
ion
(mm
)
Distance (mm)
30 kN Test 30 kN FE60 kN Test 60 kN FE80 kN Test 80 kN FE
J7
Fig. 15 Validation of the deformed shapes of the FE model against test results
Materials and Structures
4.2.4 Cracks in the concrete core
The contours of the cracking in the concrete core by
the FEA were exhibited by plotting the principle strain
contour of the concrete elements. Once achieving the
limit of the cracking strain, the cracks are assumed to
be developed in the concrete. All the elements
exceeded the cracking strain were highlighted and
compared with the cracks that were observed from the
tests in Fig. 17. Through the comparisons of the cracks
developed in the SCS sandwich beam between the
observations in the test and FEA, it can be seen that the
developed FE model can be capable of predicting most
of the cracks developed in the concrete that were
observed in the tests.
4.2.5 Load-end slip behaviors between steel face
plate and concrete core
The load-slip behaviors between the concrete core and
bottom steel face plate given by the FEA were
compared with the corresponding experimental load-
slip curves in Fig. 18. From these figures, it can be
seen that the developed FE model offers reasonable
predictions of the load-slip behavior between the steel
face plate and the concrete core during the working
state with acceptable differences. It was also observed
from the test that sometimes the slip was very difficult
to measure due to the small values especially at the
elastic working stage of the SCS sandwich beam. This
might be one reason that caused the differences of the
load-slip curves between the predictions and the test
results.
5 Recommended finite element analysis
procedures
To carry out the FEA on the SCS sandwich beam with
J-hook connectors, it is essential to offer proper
simulations of the J-hook connectors at the working
state. This requires the FE model can capture the
longitudinal shear behavior and axial tensile behav-
iors. The longitudinal shear behaviors can be simu-
lated by cylindrical stud with the same diameter and
Table 5 Ultimate strengths
and failure modes of SCS
sandwich beam
BSY bottom steel plate yield,
VSF vertical shear failure in the
concrete core, CF connector
failure, CF connector fail
Beam Pt (kN) Experimental
failure mode
PFE (kN) Predicted
failure mode
PFE/Pt
SCS 80 119.1 BSY 114.8 BSY 0.96
SLSC80 95.6 BSY 84.7 BSY 0.89
SCS 100 86.2 BSY 80.3 VSF 0.93
SLCS100 55.2 VSF 54.9 CF/VSF 0.99
SLFCS100 68.7 VSF 65.1 CF/VSF 0.95
SCS150 66. 7 VSF 62.5 CF/VSF 0.94
SLCS150 45.4 VSF 42.2 CF/VSF 0.93
SLCS200 40.1 VSF 39.2 CF/VSF 0.98
SLF200-1 45.6 VSF 47.1 CF/VSF 1.03
SLF200-2 48.9 VSF 46.4 CF/VSF 0.95
SLF300-1 30.3 VSF 30.4 CF/VSF 1.01
J1 174.7 BSY/VSF 182.7 CF/VSF 1.05
J2-1 221.2 VSF 228.2 CF/VSF 1.03
J2-2 137.2 VSF 135.8 CF/VSF 0.99
J2-3 352.4 VSF 380.1 CF/VSF 1.08
J3 368.3 BSY/VSF 396.4 CF/VSF 1.08
J4 230.4 VSF 201.3 CF/VSF 0.87
J5 146.0 VSF 154.8 CF/VSF 1.06
J6 164.5 BSY/VSF 166.7 BSY/VSF 1.01
J7 121.8 BSY/TSY 122.2 BSY/TSY 1.00
Mean 0.99
Cov 0.06
Materials and Structures
(c)(b)(a)
(f)(e)(d)
(i)(h)(g)
0
25
50
75
100
125
Loa
d (k
N)
Deflection (mm)
SCS80 Test
SCS80 FE0
25
50
75
100
Loa
d (k
N)
Deflection (mm)
SLCS80 TestSLCS80 FE
0
20
40
60
80
100
Loa
d (k
N)
Deflection (mm)
SCS100 TestSCS100 FE
0
20
40
60L
oad
(kN
)
Deflection (mm)
SLF200-2 Test
SLF200-2 FE0
15
30
45
Loa
d (k
N)
Deflection (mm)
SLCS200 TestSLCS200 FE
0
20
40
60
Loa
d (k
N)
Deflection (mm)
SLCS150 TestSLCS150 FE
0
20
40
60
Loa
d (k
N)
Deflection (mm)
SLCS100 Test
SLCS100 FE0
20
40
60
80L
oad
(kN
)
Deflection (mm)
SLFCS100 TestSLFCS100 FE
0
50
100
150
200
0 10 20 30 40 0 10 20 30 40 0 10 20 30 40
0 10 20 30 40 0 10 20 30 40 0 10 20 30 40
0 10 20 30 40 0 10 20 30 40 0 5 10 15
Loa
d (k
N)
Deflection (mm)
J1 TestJ1 FE
(l)(k)(j)
(o)(n)(m)
0
100
200
300
Loa
d (k
N)
Deflection (mm)
J2-1 TestJ2-1 FE
0
50
100
150
Loa
d (k
N)
Deflection (mm)
J2-2 TestJ2-2 FE
0
100
200
300
400
Loa
d (k
N)
Deflection (mm)
J2-3 TestJ2-3 FE
0
50
100
150
200
250
Loa
d (k
N)
Deflection (mm)
J4 TestJ4 FE
0
50
100
150
200
Loa
d (k
N)
Deflection (mm)
J6 TestJ6 FE
0
50
100
150
0 5 10 15 20 0 5 10 15 20 0 10 20 30 40
0 5 10 15 0 10 20 30 40 0 20 40 60 80
Loa
d (k
N)
Deflection (mm)
J7 TestJ7 FE
Fig. 16 Validation of the
load–central deflection
curves of the FE model
against test results
Materials and Structures
(b) FE of J2-2(a) Test of J2-2
(d) FE of J4(c) Test of J4
(f) FE of J5(e) Test of J5
(g) Test of J6
(h) FE of J6
(i) Test of J7
(j) FE of J7 Fig. 17 Validations of the cracks in the concrete of the FE mode
Materials and Structures
height of the J-hook connector. Regarding the axial
tension–elongation behaviors, it needs to be carefully
calibrated through the tensile tests. Thus, tensile tests
on the J-hook connectors in the sandwich specimen
become quite important to this FE model. The
recommended FEA procedure were summarized as
the following.
(1) Carrying out tensile tests on a pair of interlocked
J-hook connectors to obtain the tension–elonga-
tion behaviors. These tension–elongation behav-
iors will be assigned to the spring element that
was used to connect two cylindrical stud con-
nectors in the FE model.
(2) Modeling the steel face plates with the same
geometry and materials as used in the beam tests.
(3) Modeling the cylinder shear stud pairs with the
same diameter, effective height, and materials as
the J-hook connectors that work in pairs. All
these modeled shear stud will share nodes with
the steel face plates.
(4) Using the 3D spring element to link a pair of
shear studs that were attached to the top and
bottom steel face plates. The tension–elongation
behaviors of the J-hook connectors obtained
from the tensile tests in step (1) are assigned to
the spring elements.
(5) Building the concrete cores and defining the
interactions among different interacting parts.
(6) Solutions
6 Discussions of the finite element model
The finite element model developed in this paper not
only can be used for the analysis of SCS sandwich
beams with J-hook connectors, but also can be applied
to the SCS sandwich beams with overlapped headed
shear studs and other forms of interacted connectors.
The key elements in this model are the simulations of
the longitudinal shear-slip behavior and axial tension–
elongation behavior of a pair of interacting connectors
in the SCS sandwich composite beams.
6.1 Validation of the finite element model against
SCS sandwich beams with overlapped headed
shear stud
Another nine SCS sandwich beams with overlapped
headed shear studs in Ref. [2] were also used to
validate this FE model. The details of the specimens
were given in the Table 6.
Following the recommended finite element analysis
procedures in Sect. 5, the FEA were carried out on the
(a) (b) (c)
(d) (e) (f)
0
100
200
300
Loa
d (k
N)
Slip (mm)
J2-1 FE
J2-1 Test0
50
100
150
Loa
d (k
N)
Slip (mm)
J2-3 FE
J2-3 Test0
100
200
300
Loa
d (k
N)
Slip (mm)
J4 FE
J4 Test
0
50
100
150
200
Loa
d (k
N)
Slip (mm)
J6 Test
J6 FE0
50
100
150
Loa
d (k
N)
Slip (mm)
J7 FE
J7 Test0
20
40
60
0 1 2 3 0 0.2 0.4 0.6 0 1 2 3
0 2 4 6 0 1 2 3 0 3 6 9
Loa
d (k
N)
Slip (mm)
SLCS150 Test
SLCS150 FE
Fig. 18 Validations of the
load-slip behaviors of the FE
model
Materials and Structures
SCS sandwich beams with overlapped headed shear
studs.
6.1.1 Simulation of the overlapped headed shear stud
As recommended in step (1) of Sect. 5, three direct
tensile tests on a pair of overlapped headed shear studs
were carried out to obtain the tension–elongation
behavior of the basic component of the SCS sandwich
composite beams with overlapped headed shear stud
(see Fig. 19). From Fig. 19, it can be seen that the FE
model simulates well the tension–elongation behavior
of the basic component of the SCS sandwich beam.
6.1.2 Finite element model of the SCS sandwich beam
with headed shear studs
Following the recommended FEA procedure in Sect.
5, the FE models were built to simulate the different
components of the SCS sandwich beam as shown in
Fig. 20. Similar to the SCS sandwich beam with the
J-hook connectors, the steel face plates, studs, con-
crete core, support and load cell were modeled as
shown in Fig. 21.‘
6.1.3 Validation of the finite element model
The validation of the finite element model was carried
out by comparing the load–central deflection of the
SCS sandwich beams with the experimental load–
central deflection curves in Fig. 22. From these
figures, it can be concluded that the load–central
deflection curves by the FEA agree well with exper-
imental curves. The ultimate strengths and failure
modes of the nine SCS sandwich beams were
compared with the FE predictions in Table 6. From
Fig. 22 and Table 6, it can be concluded that the
developed FE model is capable of describing the
structural performance of the SCS sandwich beam
with overlapped headed shear studs in terms of load–
central deflection curves, ultimate strength and failure
modes of the specimens.
Table 6 Ultimate strength and failure mode of the beam B1–
B9
Beam Test Finite element
analysis
Ratio of
PE/Pu
Failure
mode
Pu
(kN)
Failure
mode
PE
(kN)
B1 VSF,
BSY
212.3 CF, VSF 221.8 1.04
B2 VSF 236.0 CF, VSF 241.0 1.02
B3 VSF,
BSY
378.0 VSF 403.2 1.07
B4 VSF 133.6 VSF 135.1 1.01
B5 VSF 451.3 VSF 462.2 1.02
B6 CF, VSF 233.1 CF, VSF 233.7 1.00
B7 CF, VSF 165.4 CF, VSY 162.6 0.98
B8 VSF,
BSY
174.3 VSF,
BSY
171.7 0.99
B9 FF, BSY 127.8 FF, BSY 121.9 0.95
Mean 1.01
Cov 0.03
BSY bottom steel plate yield, VSF concrete core shear failure,
CF connector shear failure, FF flexural failure, Pu ultimate
strength of the test, PE ultimate strength by finite element
analysis (FEA), Cov coefficient of variance
(a) Tension test on overlapped headed studs (b) Tension-elongation curve
0
10
20
30
40
0 4 8 12
Ten
sion
For
ce (
kN)
Elongation (mm)
T1T2T3FE model
T
T
Concrete
Headed
stud
200 mm
200 mm
100 mm
Fig. 19 Tension–
elongation behavior of
overlapped headed studs
Materials and Structures
Non-linear spring element
Fig. 20 Simulation of the
overlapped headed shear
stud by the spring element
Load cell
Support Steel plate
Steel plate
Stud Concrete core
Fig. 21 FE model for the SCS sandwich beam with overlapped headed shear stud
(a) (b) (c)
(d) (e) (f)
0
100
200
300
P (
kN)
Deflection (mm)
B2 Test
B2 FE0
150
300
450
P (
kN)
Deflection (mm)
B3 TestB3 FE
0
50
100
150
P (
kN)
Deflection (mm)
B4 Test
B4 FE
0
200
400
600
P (
kN)
Deflection (mm)
B5 Test
B5 FE0
50
100
150
200
P (
kN)
Deflection (mm)
B8 FE
B8 Test0
50
100
150
0 5 10 15 20 0 10 20 30 40 0 10 20 30 40
0 5 10 15 20 0 10 20 30 40 0 25 50 75
P (
kN)
Deflection (mm)
B9 Test
B9 FE
Fig. 22 Validation of the
load–deflection curves of FE
model
Materials and Structures
6.2 Discussions
The validations of the FE model on nine SCS
sandwich beams with the overlapped headed shear
studs further confirmed the accuracy of the FE
simulation and the fact that this model can be used
in analysis on SCS sandwich beams with other
interacted shear connectors. One key issue addressed
herein is the proper simulations on the structural
behaviors of the basic component in the structure.
From this point of view, the tensile tests on the
connectors become necessary and important. More-
over, so far there are no design codes that can be
followed to describe the tension–elongation behaviors
of the connectors. This should be further investigated,
and included in the design codes.
Another point needs to be pointed out is that the
spring model also has limitations on modeling the
interaction between the tensile and shear resistance of
the connectors. In the proposed spring model, the
tensile force in the spring can reduce the shear strength
of the connectors. Conversely, the shear resistance
also affects the tensile resistance of the two connectors
by the linking spring. If the steel shank that the spring
was linked to is under high shear, the tensile capacity
of the shank was also reduced even though the tensile
capacity of the spring was not decreased. Therefore,
the model can partially reflect the interaction between
the shear and tension of the connector, but the model
could not completely simulate this interaction.
7 Conclusions
This study presents a three dimensional nonlinear finite
element model for SCS sandwich composite beams with
the J-hook shear connectors and overlapped headed
shear studs. In the FE model, a pair of interlocked J-hook
connectors were simplified by two cylindrical stud
linked by 3D nonlinear spring elements. Through the
validations against the push-out and tensile tests on the
J-hook connectors, the simplified connectors in the FE
model were capable of simulating the shear-slip behav-
ior and axial tension–elongation behavior of the basic
component i.e. a pair of interlocked J-hook connectors
in the SCS sandwich beams. Nevertheless, this simpli-
fication of the interlocked J-hook shear connectors
significantly reduced the total amounts of the elements,
simplified the simulating of the interaction between the
connectors and the concrete core, and avoided the
singular elements used in the FEA. All these advantages
resulted in improving the efficiency of the FEA,
improving the convergence and avoiding the pre-mature
termination of the nonlinear FEA.
Extensive experimental data (20 beam tests) on the
quasi-static tests on the SCS sandwich beams with
J-hook connectors was used to validate the FE model.
Through the validations, it indicates that the developed
FE model was capable of simulating the structural
behavior of the SCS sandwich beams with the J-hook
connectors in terms of ultimate load carrying capacity,
load–central deflection curves, deformed shapes at
different loading levels, relative slip between the steel
face plate the concrete core, and cracks in the concrete
core materials. The errors of the FEA might be caused
by the simulation errors of shear-slip behavior and
tension–elongation behaviors for J-hook connectors,
limited information on the tensile fracture energy of
the ULCC, and ignoring the confining effect of the
concrete to the tensile and shear strength of the J-hook
connectors. The tensile fracture tests on the ULCC
needs to be carried out to provide more information on
the tensile fracture energy of this material.
This developed FE model is not only applied to the
SCS sandwich beams with the J-hook connectors, but
also can be extended to SCS sandwich beams with
other types of interacted connectors. In this paper, nine
SCS sandwich beam with overlapped headed shear
studs were used to confirm the applicability of the FE
model. Through the validation, the FEA agrees well
with the test results. Standard FEA procedures were
recommended. One point needs to be addressed is that
tensile tests are commonly necessary and important for
the new types of connectors used in the SCS sandwich
beam. This is because the necessary information on the
tensile behaviors of them is needed for the FEA.
The FEA extends the studies and offers alternative
nonlinear analysis method on the SCS sandwich
composite beams with J-hook connectors and other
types of interacted connectors.
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