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Steel Structures 7 (2007) 119-128 www.kssc.or.kr
Cyclic Loading Tests on Composite Joints
with Flush End Plate Connections
SHI Wen-long1*, LI Guo-qiang2, YE Zhi-ming1 and R. Y. Xiao3
1Department of Civil Engineering, Shanghai University, Shanghai, 200072, China2Department of Structure Engineering, Tongji University, Shanghai, 200092, China
3Department of Civil Engineering, University of Wales Swansea, UK
Abstract
The tests on composite joint specimens with flush end plate connections subjected to cyclic loads have been conducted inTongji University. One bare steel joint specimen has also been tested for comparison. Various instrumentations have been usedto measure: beam strains, column strains, rebar strains, connection deformations and deflections of specimens. The testobservations are reported in detail in this paper. The main results are as follows: (1) the moment-rotation relationships of theconnections are obtained from the tests, which demonstrate that the hysteretic loops are stable and show good energy dissipationability; (2) the composite joint specimens show large strength resistance and good ductility, and all the rotations of connectionare greater than 0.03rad as required by the FEMA-97; (3) similar failure modes have been identified from the observation ofthe composite specimens, which are found to be concentrated around the joint zone; and (4) the slippage between the concreteslab and steel beam is very small, which shows that between the concrete slab and steel beam the full composition can beobtained by the proper design for the shear connectors.
Keywords: Flush endplate, Composite joint, Low cyclic loading, Joint behavior, Moment-rotational relationship
1. Introduction
It has been convenient to assume full rigid or pinned
connections to simplify analysis for steel frame design.
However, for the sake of cost and construction, a great
number of connections have been designed as semi-rigid
ones. Composite slab and semi-rigid connection constitute
a new type of semi-rigid composite connection. Composite
action of connection is achieved through longitudinal
reinforcement and headed shear studs. A great deal of
experiments and earthquake calamities have shown that
semi-rigid composite connections have excellent mechanical
and aseismic performance. In practical engineering, the
using of semi-rigid composite connections can reduce
steel consumption and expedite construction. In the last
twenty years, a lot of tests (Silva and Simoes, 2001; Sun
and Li, 2004; Laszlo Dunai, 2004; B. M. Broderick and
A. W. Thomson, 2005) and theoretical studies on the bare
steel and composite joints were carried out (Tsuji Bunzo,
2001; Changbin Joh and Wai-Fah, 2001; Rene Maquoi
and Jean-Pierre Jaspart, 2002). The previous experimental
research on composite connections was carried out under
symmetrical and monotonic loading (Xiao and Nethercot,
1994; Anderson and Najafi, 1994). There has been
limited research work conducted on composite joints
under non-symmetrical loading and cyclic loading to
quantify the hysteretic characteristics and the effects of
unbalanced connection moments on the joint. In China,
some semi-rigid bare steel and composite joints (Guo,
2003; Yang, 2004; Gao, 2002), bare steel (Guan, 2003)
and composite frames (Wang, 2005) with semi-rigid
connections have been tested under static loads, cyclic
loads (Guo, 2002) and fire (Lou, 2005) since 1992.
In this paper, one bare steel joint and two composite
joints were tested under cyclic loading. Special attention
has been paid to: (1) stiffness, moment resistance, rotational
capacity of composite joints; (2) hysteretic behavior of
composite joints; (3) effect of stiffeners on behavior of
joints; (4) moment-rotation relationship of composite
joins and damage mode; (4) difference of performance
between the bare steel and composite joints.
2. Configurations of Specimens
Under the action of lateral loading, typical moment-
resisting frame structures may be simplified for analysis
purposes into a series of two-dimensional sub-frames
with interior joints as shown in Fig. 1, where the moment
inflection points are assumed at the middle of beam spans
and column heights, allowing sub assemblages with interior
joints to be isolated for evaluating their performances.
*Corresponding authorTel: +86-21-65985318; Fax: +86-21-65983431E-mail: [email protected]
120 SHI Wen-long et al.
2.1. Specimens description
One bare steel joint and two composite joint specimens
denoted as SJ1 and CJ3, CJ4, respectively, were tested.
Two beams H300 × 150 × 6 × 10 of 1.6 m long were
connected to a column H200 × 200 × 8 × 12 to form a
cruciform specimen as shown in Fig. 2. The beams were
connected to the column flanges by means of 10 mm
thick end plate and M20 Grade 10.9 bolts, as shown in
Fig. 2b. All standard steel members and end plates are
made of Q345 steel. A common form of metal decking
floor system, which comprises a concrete slab supported
by profiled metal decking sitting on steel beams, was
adopted for all composite specimens. The beam-to-slab
connections are connected by welded-through shear
connectors. Longitudinal reinforcement bars pass across
the column line continuously. The longitudinal reinforcement
consisted of Φ10@120 bars, while the transverse reinforcement
consisted of Φ6@200 bars. The reinforcement ratio is
0.8%, which is defined as the reinforcement area divided
by the concrete area above the ribs of the metal sheeting.
The common used 0.8 mm thick profiled steel sheeting
DP688 was chosen as bottom shuttering for the specimens.
The profiled steel sheeting was filled with cast-in-place
normal weight concrete with design strength of 30 N/
mm2. The composite slabs were 1,200 mm wide and
140 mm thick. Spaces between column flanges at the slab
level were solidly cast with concrete. CJ3 was similar to
CJ4 except that the panel zone was stiffened with
transverse plate welded to the column web.
2.2. Specimen design and fabrication
All specimens were fabricated in the Structural
Laboratory at the Tongji University. The bare steel
components were firstly assembled in situ. The profiled
metal decking was then placed on the steel beams and
shear studs were installed by welding. After the joint
Figure 1. Location of specimen.
Figure 2. Specimen of composite joint.
Cyclic Loading Tests on Composite Joints with Flush End Plate Connections 121
assembly, formwork was set up with the metal decking as
bottom shuttering, plywood as side shuttering. Concrete
casting work was then carried out. The casting of cubes
and cylinders for material tests was done at the same
time. The cube and cylinder samples and the slab were
cured under the same conditions.
3. Instrument Arrangement
Strains in the reinforcement and on the steel beam and
column were measured using strain gauges. The
arrangement of strain gauges is shown in Fig. 3. After
assembly of the test specimens, all the instruments were
mounted on the specimens. Inclinometers were used to
measure the rotation of the column and the relative
rotation of the beam so as to provide full information
from which the moment-rotation relationship could be
derived. The arrangement of inclinometers is shown in
Fig. 4. Displacement transducers were used to measure
the deflection of the specimens on the bottom flange of
the beam and also to monitor slippage between steel
beam and slab. The relative rotation of the beam to
column can also be obtained from the deflection values
within the calibrated horizontal length of the beam. The
arrangement of LVDT is shown in Fig. 5.
4. Loading Procedure
The experimental set-up included a supporting frame
and a loading system is shown in Fig. 6 and Fig. 7. The
lateral loading was applied to the specimen at the top of
the supporting frame by a computer-controlled hydraulic
actuator with a maximum load capacity of ±1000 kN and
available stroke of ±200 mm. The specimens were loaded
until failure or when the maximum stroke of the actuator
was reached.
Figure 3. Arrangement of strain gauges.
Figure 4. Arrangement of inclinometers.
Figure 5. Arrangement of LVDT.
Figure 6. Test set-up.
Figure 7. Photo of test set-up.
122 SHI Wen-long et al.
5. Material Tests
5.1. Steel coupons
Material for tensile test coupons was cut from the
flanges and webs of the steel beams and columns. Values
of yield strength and ultimate strength for steel members
are listed in Table 1.
5.2. Reinforcement bars
Test specimens were cut from the 6 mm and 10 mm
diameter rebars. The test results are listed in Table 2.
5.3. Concrete
Concrete work was carried out inside the laboratory
with the specimen in the test position. Samples of
concrete to be used for monitoring the concrete strength
were cast at the same time to cast for composite joint
specimens. The compressive and tensile strengths of all
the samples are summarized in Table 3.
Table 1. Measured tensile strengths of steel
No.Yield strength
(N/mm2)Tensile strength
(N/mm2)Yield strain
(%)Elastic modulus(×105 N/mm2)
Extensibility(%)
BW-1 383.9 564.5 0.195 1.97 28.40
BW-2 387.4 559.9 0.190 2.04 32.54
BW-3 401.1 563.5 0.196 2.05 35.46
BF-1 435.8 509.3 0.206 2.12 29.88
BF-2 402.2 495.4 0.199 2.02 29.78
BF-3 431.9 509.2 0.196 2.20 31.19
EP-1 391.9 498.4 0.190 2.06 29.93
EP-2 436.2 507.6 0.209 2.09 29.89
EP-3 428.1 502.9 0.193 2.22 31.34
CW-1 406.3 505.9 0.189 2.15 30.54
CW-2 405.6 489.9 0.167 2.43 31.79
CW-3 397.7 480.5 0.214 1.86 33.40
CF-1 417.0 500.5 0.216 1.93 30.33
CF-2 414.5 497.7 0.192 2.16 30.58
CF-3 397.6 496.9 0.192 2.07 30.26
Average 0409.15 0512.14 0.200 2.09 31.02
Table 2. Measured tensile strengths of rebar
No. Diameter/mmYield strength
(N/mm2)Tensile strength
(N/mm2)Yield strain
(%)Elastic modular(×105 N/mm2)
Extensibility(%)
GJ1-1 6.77 296.97 436.1 0.140 2.12 28.28
GJ1-2 6.59 318.50 443.3 0.157 2.03 30.88
GJ1-3 6.64 310.31 436.1 0.165 1.87 29.98
Average 6.67 308.59 0438.50 0.154 2.01 29.71
GJ2-1 9.92 462.70 607.7 0.248 2.02 33.02
GJ2-2 10.160 433.50 575.2 0.236 1.85 31.94
GJ2-3 10.070 444.10 581.6 0.248 1.90 29.54
Average 10.050 446.77 0588.17 0.244 1.92 31.50
Table 3. Measured strengths of concrete
No. Size of samples (mm) Cube strength (N/mm2) Average
H1-1 150×150×150 40.89
41.48H1-2 150×150×150 40.89
H1-3 150×150×150 42.67
No. Size of samples (mm) Elastic modular (N/mm2) Average
H2-1 100×100×300 40000
41429H2-2 100×100×300 40000
H2-3 100×100×300 42857
Cyclic Loading Tests on Composite Joints with Flush End Plate Connections 123
6. Test Phenomenon
6.1. Specimen SJ1
SJ1 is a bare steel joint specimen used as a benchmark
for comparison with other composite joint specimens. A
gap between end plate and column flange was observed
when the displacement of top of column reached ±25 mm
(Fig. 8a). The obvious shearing deformation was observed
in the panel zone when the displacement reached ±60 mm
(Fig. 8b). The specimen was loaded until the maximum
stroke of the actuator was reached. No local buckling was
observed on the steel components and the lateral load was
keeping on going up.
6.2. Specimen CJ3
The first cracking was observed on the right slab when
the displacement of the top of column reached 25 mm.
The crack started from the tip of column flange and
extended towards the edge. The lateral load was then
unloaded to zero and the cracks on right slab closed
completely. A reversed loading was then applied, and the
first cracking was also observed on the left slab. With the
increasing in loads, the appeared cracks extended and
widened gradually (Fig. 9a). When the displacement
reached 80 mm, a wide gap between slab and column
flange (Fig. 9b) was observed. When the displacement
reached 120mm, the state of composite slab vicinity to
the column is shown in Fig. 9b and Fig. 9c. It is noted
that the slab around the column is badly damaged. A
large shear distortion was observed in the column panel
zone (Fig. 9d). When the displacement reached 160 mm,
the debonding of the concrete from the metal decking and
the inclined cracks starting from the ribs are visible, as
illustrated in Fig. 9e. The former was due to the flexural
deflection of the beam, while the latter was caused by the
shear and bending action in the slab. When the
displacement reached 200 mm, the damage of concrete
slab continued and the crushed concrete was dropped off
from the gap between the slab and column flange. A wide
gap was observed between end plate and column flange
Figure 8. Test photo of SJ1.
Figure 9. Test photos of CJ3.
124 SHI Wen-long et al.
(Fig. 9f). After the test, the concrete slab vicinity to the
column was cut and examined. It was found that the
concrete at the back of column flange was completely
crushed.
6.3. Specimen CJ4
The first cracking was observed on the right slab when
the displacement of the top of column reached 25 mm in
pull way. The lateral load was then unloaded to zero and
the cracks on right slab closed completely. A reversed
loading was then applied, and the first cracking was also
observed on the left slab. With the increasing in loads, the
appeared cracks were extended and widened gradually.
When the displacement reached 80 mm, a wide gap
between slab and column flange (Fig. 10a) was observed.
The debonding of the concrete from the metal decking
was visible (Fig. 10b). After the test, the cracks of
concrete slab are shown in Fig. 10d. The concrete slab
vicinity to the column was cut and examined. It was
found that the concrete at the back of column flange was
completely crushed (Fig. 10f).
7. Test Results and Analysis
In this section, the experimental results of all specimens
under cyclic reversal loading will be described. For
convenience of comparison, the values of the main
parameters, such as cracking moment, yield moment and
corresponding rotation, initial rotational stiffness, damage
modes are listed in Table 4.
7.1. Hysteretic curves of lateral load and corresponding
displacement
The hysteretic curves of lateral load and its displacement
Figure 10. Test photos of CJ4.
Table 4. Experimental results
No. Type of joint Mcr (kN · m) My+ (kN · m) My
− (kN · m) Pu (kN)
SJ1 bare joint / 44.91 -44.91 /
CJ3 composite joint 41.10 78.97 -102.160 64.83
CJ4 composite joint 38.09 82.83 -98.81 60.06
No. Ki+ ( kN · m/mrad) Ki
− ( kN · m/mrad) θy+ (mrad) θy
− ( mrad) Damage modes
SJ1 06.93 0-6.93 42.11 -42.11 Not damaged
CJ3 14.63 -19.51 12.02 -14.69 A, C, E
CJ4 14.88 -17.72 11.25 -13.62 A, C, E
Note: (1) Mcr: cracking moment; (2) My+, θy
+: positive yield moment and corresponding rotation; (3) My−, θy
−: positive yield momentand corresponding rotation; (4) Pu: the maximum lateral force; (5) Ki
+: positive initial rotational stiffness; (6) Ki−: negative initial
rotational stiffness; (7) In the ‘Damage modes’ column: A = reinforcement yielding; B = end plate yielding; C = yielding in shearpanel zone; D = bolt yielding or fracture; E = concrete cracking; F = welding fracture in column web; G = yielding in beam flange.
Cyclic Loading Tests on Composite Joints with Flush End Plate Connections 125
at the top of column (P-∆) are shown in Fig. 11. It can be
seen that the P-∆ hysteretic curves are symmetrical about
centerline of column cross section because of the
symmetry of specimens about centerline of column cross
section. For specimens CJ3 and CJ4, the maximum lateral
force ratio between push and pull is 0.93 and 1.06
respectively.
7.2. Hysteretic curves of moment-rotation of the
connections
The hysteretic curves of moment-rotation for left and
right connections are shown in Fig. 12. It can be seen that
the hysteretic loops are stable and ductile and show good
energy dissipation capacity. The hysteretic curves for left
and right connections are nearly same because of
symmetry of left and right connections. For the specimen
SJ1, the maximum moment is corresponding to the
maximum rotation under positive and negative moment.
It indicated that no strength degradation was achieved for
the specimen SJ1.
The curves for left and right connections are in good
agreement because of the symmetrical construction
details. For the specimens CJ3 and CJ4, pinching, indicated
by the reduction of stiffness, is noted. In composite joints,
pinching is mainly caused by the opening and closure of
the cracks in the concrete slab. The slippage between
steel components and the slippage between the composite
slab and steel beam also contribute to the pinching effect.
For the specimens CJ3 and CJ4, the maximum moment is
not corresponding to the maximum rotation under positive
and negative moment respectively. This phenomenon
indicated that strength degradation was achieved for the
specimens CJ3 and CJ4. In addition, the hysteretic curves
of moment-rotation for specimens CJ3 and CJ4 are the
nearly same as that of specimen SJ1 after these two
composite joint specimens reached their maximum lateral
force. It indicated that the performance of composite
joints is in agreement with that of bare steel joint because
of losing composite action of concrete slab.
Figure 11. Hysteretic curves of P-∆.
Figure 12. Moment-rotation curve of the connections.
Figure 13. Shear force-rotation curve in the column panel zone.
126 SHI Wen-long et al.
7.3. Hysteretic curves of shear force and corresponding
rotation
Under a lateral loading, the connection on one side was
subjected to a hogging moment, while the connection on
the other side was subjected to a sagging moment. In
consequence, the column panel zone bore a large shear
distortion. The hysteretic curves of shear force and
corresponding rotation in the column panel zone for all
three specimens are shown in Fig. 13.
7.4. Energy dissipation
The energy dissipation capacity is the factor of utmost
importance when evaluating the performance of a structure
subjected to seismic attacks. Its value is generally
deformation-dependent and serves as an indication of
dissipation energy for the structure through the inelastic
range. The dissipated energy Ji in the ith loading cycle is
defined as the area encircled by the restoring force-
deformation curve. The energy per cycle may be further
separated into two parts, Ji+ for positive loading and Ji
−
for negative loading. Since the asymmetrical characteristics
of a composite connection under sagging and hogging
actions, the moment-rotation response is thus non-
symmetrical. This may lead different values of dissipated
energy for positive and negative loading semi-cycles.
The energy dissipation of all three specimens is shown
in Fig. 14. It can be seen that in the first eight cycles, the
energy dissipation is very small. This indicates that the
specimens are in elastic state. After the eighth cycle, the
energy dissipation of specimens keeps on going up with
the increasing in cycles.
7.5. Skeleton curves
The skeleton curves of P-∆ are shown in Fig. 15. It can
be seen that the composite joint specimens have larger
strength resistance and stiffness than the bare steel joint
specimen does owing to the presence of reinforcement
bars and concrete slab. The composite joint specimens
show the nearly same performance as the bare steel joint
does after reaching maximum lateral force.
7.6. Strain of beams
The strain of left steel beam of specimens SJ1 and CJ4
is shown in Fig. 16. For the specimen SJ1, No. 2 and No.
6 strain gauge readings are much higher than the other
strain gauges’. The maximum data obtained from No. 2
strain gauge is nearly 1000 µε, while that of No. 6 strain
gauge is nearly 2000 µε. The readings of No. 1 and No.
7 strain gauge located on the beam flanges are very small.
Figure 14. Cumulative energy dissipation of specimen.
Figure 15. Skeleton curves of P-∆.
Figure 16. Strain of left beam of specimen SJ1 and CJ4.
Cyclic Loading Tests on Composite Joints with Flush End Plate Connections 127
From the data obtained from these strain gauges, the
follow conclusions can be drawn: (1) For the flush end
plate connection, the strain of beam flanges is very small
because of lack of restriction, especially for the bare steel
joint; (2) The strain of beam web in level of bolts is large
because of strong restriction of bolts; (3) There is a gap
between end plate and column flange because of
pretension of bolts. Thus, the beam flanges begin to bear
load after these gaps disappear when loading. (4) The
steel beam of specimen SJ1 is yielding while the steel
beam of specimen CJ4 is still elastic.
7.7. Slippage between steel beam and concrete slab
The slip between steel beam and concrete slab versus
displacement of the top of column is shown in Fig. 17. It
can be seen that the readings of LVDT7 and LVDT8 keep
on going up with the increasing in the lateral displacement.
There is no obvious difference in readings between
LVDT7 and LVDT8 during the whole test. For the
specimen CJ3, the maximum readings of LVDT7 and
LVDT8 are 0.22 mm and 0.275 mm respectively. The
reading ratio is 0.8. The slippage strain is 159 µε, which
is defined as the difference in reading of LVDT7 and
LVDT8 divided by the spacing between this two LVDT.
For specimen CJ4, the maximum readings of LVDT7 and
LVDT8 are 0.165 mm and 0.146 mm respectively. The
reading ratio is 1.13, while the slippage strain is 55 µε.
8. Conclusions
Through the experimental studies, the concluding remarks
may be summarized as:
(1) The composite joints with flush end plate connection
have good moment resistance and rotational capacity
under cyclic loading. The ultimate rotations of all three
specimens are beyond 0.03rad, as required by the FEMA-
97 for earthquake-resistance.
(2) The cyclic test results indicated that the hysteretic
loops of the connection moment-rotation curves are stable
and plummy, even though pinching in large inelastic
ranges was observed.
(3) The presence of the column web stiffener can increase
the moment capacity and initial rotational stiffness of the
connection, but not very much.
(4) Failures of composite joints are observed to be
concentrated in the nodal zone.
(5) By a proper full shear design, the slippage between
slab and steel beam is so small that these two components
can be assumed to work well together.
Acknowledgment
The studies presented in this paper are sponsored by the
Natural Science Foundation of China through the
Outstanding Youth Project (No. 50225825). The financial
support from NSFC is especially acknowledged.
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