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International Journal of Civil Engineering and Technology (IJCIET) Volume 9, Issue 4, April 2018, pp. 1039–1048, Article ID: IJCIET_09_04_117
Available online at http://www.iaeme.com/ijciet/issues.asp?JType=IJCIET&VType=9&IType=4
ISSN Print: 0976-6308 and ISSN Online: 0976-6316
© IAEME Publication Scopus Indexed
BEHAVIOUR OF COMPOSITE SLAB BEAM
WITHOUT SHEAR CONNECTOR
Alphonsa Antony
Assistant Professor,
Department of Civil Engineering,
Jeppiaar Engineering College, Chennai, India
Nivin Joy
Assistant Professor,
Department of Mechanical Engineering,
Sathyabama Institute of Science & Technology,
Chennai, India
ABSTRACT
The floor-to-floor height is considered as a significant aspect due to limited city
areas as the number of high-rise buildings increases. To reduce the floor-to-floor
height, a newly developed composite slab was proposed and experimentally explored.
This project deals with the study of behavior of composite slabs without shear
connector. The principal disadvantage of shear connector lies with the placement of the
transversal bottom slab reinforcement, which is often very difficult. In the proposed
composite beam the top flange of I-section takes the role of shear connector. The
behavior of composite slabs with different depths of I Section inside the slab is found
out by using two sections of steel. Based on the results Load Deflection curve was
plotted. CAD Modeling is done using Solidworks Software and Finite Element Analysis
is done using ABAQUS software.
Key words: Composite Slab, Shear Connector, I-Section, Load Deflection Curve, Finite
Element Analysis.
Cite this Article: Alphonsa Antony and Nivin Joy, Behaviour of Composite Slab Beam
Without Shear Connector, International Journal of Civil Engineering and Technology,
9(4), 2018, pp. 1039–1048.
http://www.iaeme.com/ijciet/issues.asp?JType=IJCIET&VType=9&IType=4
1. INTRODUCTION
Around 1926 the use of steel–concrete composite construction began due to the increasing
demands of long span floors but with shallow floor depth. A large number of composite floor
sections were proposed and had been successfully used in the building construction industry.
The composite construction results in a shallower beam depth and consequently smaller floor-
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to floor height. Reinforced concrete slab, hot-rolled steel beam, and shear connector are the
main components of a composite member. That is a composite member consist of a T -beam
formed by a reinforced concrete slab, a steel joist and mechanical shear connectors between
them. The ability to combine well the advantages of both steel and concrete results in the
popularity of this form of construction. When compared to the contribution of the slab and joist
separately composite beams exhibit enhanced strength and stiffness. The shear connectors
perform the horizontal shear resistance and vertical interlocking between slab made of concrete
and steel beams to generate a composite section that acts as a single unit. Composite members
are constructed keeping in mind that the structural steel shapes and the concrete act together to
resist axial compression and or bending. Different types of shear connectors are studs, channels,
stiffened angles, and flat bars. Through the steel deck studs are welded into the structural steel
framing in the building construction markets. A new composite section system was introduced
to the building construction industry in the late twentieth century which uses the cold-formed
steel beam as a substitute for the hot-rolled steel beam to provide a lighter weight of structural
system.
For framed buildings, bridges, and stadia, steel–concrete composite construction is a very
efficient structural method because of several well-established advantages that it provides
compared to other structural types. Structures are safe, robust, and economic due to the optimal
combination of the individual properties of structural steel and concrete. Because of the
increased speed of construction and flexibility that they offer, steel–concrete composite beams
are an ideal solution for building floors or bridge decks. In municipal buildings and bridge
structures due to the excellent performance in terms of higher loading capacities and larger
flexural stiffness. In the preliminary design phase more and more newly-built high-speed
railway bridges also give preference to composite beams just because of their excellent
mechanical and economic performance. Stiffness and high strength properties together with a
low weight, good corrosion resistance, enhanced fatigue life, low thermal expansion, low
machining cost are some of the interesting features of composite structures that impel their use
in different industrial devices.
2. EXPERIMENTAL PROCEDURE
2.1. Material Properties
A nominal mix was designed according to IS: 10262-1982 for M30 grade of concrete.
2.1. Test Specimen
A total of 6 full-scale composite slab specimens are built and tested in accordance with the
Eurocode 4 - Part 1.1 to determine (1) the structural behavior and (2) the load carrying capacity.
Experimental program includes flexural test on 2 sets of slab specimens subjected to varying I
sections. That is for 1 set ISMB 200 is used (PES1a, PES 1b, PES 1c) and for another set
ISMB300 is used (PES2a, PES 2b, PES 2c). For each set of 3 specimens, first specimen is made
up of inserting 80 mm of I section inside the concrete slab, second specimen is made up of
inserting 100 mm of I section inside the concrete slab and the third specimen is made up of
inserting 120 mm of I section inside the concrete slab.
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2.2. Specimen Designation
Table 1 Specimen Designation
Specimen
Designatio
n
Description I Section
Used
Depth of
Insertion Drawing
PES 1a Partially Encased Slab 1a ISMB 200 80 mm
PES 1b Partially Encased Slab 1b ISMB 200 100 mm
PES 1c Partially Encased Slab 1c ISMB 200 120 mm
PES 2a Partially Encased Slab 2a ISMB 300 80 mm
PES 2b Partially Encased Slab 2b ISMB 300 100 mm
PES 2c Partially Encased Slab 2c ISMB 300 120 mm
2.1. Testing of Composite Slabs
The beams are tested under a one-point load by gradually increasing the load and the relevant
deflection is noted for each load case. 25kN load is increased gradually and corresponding
deflection is noted and finally, the collapse load is found out.
The slabs are placed on a loading frame in which the proving ring and the hydraulic jack
are also placed. A Hydraulic Jack capacity of 500 kN is used for load application. The dial
gauges are placed along the slab diagonally. In the testing setup three dial gauges are used. Dial
2 is placed in the center just beneath the point of load application. Dial 1 and Dial 3 are placed
on the opposite edges. Thus, when the load is applied gradually, the corresponding deflection
is also noted from the dial gauges.
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Figure 1 Testing Setup of PES 1a
3. FINITE ELEMENT MODEL
A three-dimensional FE model was developed by using the general-purpose program ABAQUS
to investigate the bending behavior of composite slab partially encased with I section.
Geometric and material non-linear behaviors were considered in the model. The materials used
were concrete and I section. The compressive strength of the concrete was fck =30 MPa. The
modulus of elasticity for concrete, Ec, can be calculated based on ACI building code:
Ec = 57000 √fc
which results in Ec = 25.2 GPa. The modulus of elasticity for steel was Es = 200 GPa.
Concrete was modeled using 3D deformable solid 8-point elements (C3D8R). The 4-node
general-purpose shell element S4R with reduced integration was employed in steel beam
component. The steel reinforcement was simulated using stringers, which were defined using
3D truss elements (T3D2). The self-weight and test load were simulated using a two-step
loading process to more accurately represent the loading conditions. Dynamic analysis is
carried out. The self-weight was applied using ‘‘gravity load’’ while the test load was applied
as pressure load, which were solved using a general dynamic analysis. The boundary conditions
were pinned at all its four sides. A typical FE mesh is shown in Fig.2. The mesh shape is HEX.
Figure 2 Finite Element Model
4. TEST RESULTS AND DISCUSSION
4.1. General Observations and Failure Mode
For the beam PES 1a, PES 1b, PES 1cthe first crack appear near the internal support when the
load increased to 57%, 63%, 66% of peak load respectively. In case of PES 2a, PES 2b, PES
2c first crack occurs when the load is increased to 65 %, 71%,78% of peak load respectively.
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The concrete slab near the midspan crushed and the bottom flange near the internal support
buckled at the ultimate failure state.
Figure 3 Failure pattern of PES1a Figure 4 Failure pattern of PES1b
Figure 5 Failure pattern of PES1c Figure 6 Failure pattern of PES2a
Figure 7 Failure pattern of PES2b Figure 8 Failure pattern of PES2c
4.2. Load Deflection Behaviour
The beams which are tested under two-point loading by gradually increasing the load will
deflect and the corresponding value of deflection is noted for the gradual increase in load.
Finally, the collapse load is found out. The ultimate load of PES1a, PES1b, PES1c, PES2a,
PES2b, PES2c is found to be 350kN, 275 kN,150 kN,475 kN,350 kN,175 kN respectively.
Figure 9 Load Deflection Behaviour of PES1a
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Figure 10 Load Deflection Behaviour of PES1b
Figure 11 Load Deflection Behaviour of PES1c
Figure 12 Load Deflection Behaviour of PES2a
Figure 13 Load Deflection Behaviour of PES2b
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Figure 14 Load Deflection Behaviour of PES2c
4.3. Analytical Results
For PES1a the failure first starts near the I section and then distribute to the bottom corner of
the composite slab. The displacement is maximum at the center and it gradually decreases as it
moves from the center. The stress is maximum near the top flange of ISMB 200 and surrounding
portion of it and will be minimum near the edges of the slab. The stress is maximum at the
center of ISMB 200. For PES1b the failure begins near the bottom corner of the partially
encased slab. The stress is maximum at the web of ISMB 200 and then to the top flange of the
I section.it will be minimum near the edges of the slab. For PES1c also the failure begins near
the bottom corner of the partially encased slab. The displacement is maximum near the web of
the I section and decreases gradually and minimum displacement is occurred near the corner.
The stress is maximum at the top flange of ISMB 200. For PES2a the failure begins just above
the top flange of the partially encased slab. The displacement is maximum at the center of the
composite slab and decreases gradually and minimum displacement is occurred near the corner.
The intensity of the stress will be less when compared to partially encased slab with 80 mm of
ISMB 200 inside. For PES2b the failure begins at the bottom corner of the partially encased
slab. The stress is maximum at the center of ISMB 300. The intensity will be less when
compared to PES 1b. For PES2c failure will be more at bottom corner. The stress is maximum
at the top flange of ISMB 300 and then to the web of the I section it will be minimum near the
edges of the slab.
Figure 14 Failure pattern in FE Model of PES1a Figure 15 Failure pattern in FE Model of PES1b
Figure 16 Failure pattern in FE Model of PES1c Figure 17 Failure pattern in FE Model of PES2a
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Figure 18 Failure pattern in FE Model of PES2b Figure 19 Failure pattern in FE Model of PES2c
4.4. Comparison Between FE Model and Experimental Data
The Ultimate Load carrying capacity of PES 1a obtained from FE MODEL IS 420 kN and that
from the experimental data is 350 kN. Thus there is a difference of 70 kN between the analytical
and experimental data.In case of PES1b, PES1c, PES2a, PES2b PES2c there is a difference in
load carrying capacity of 55 Kn, 30kN, 95kN, 70kN, 35kN respectively between the analytical
and experimental data.
Figure 20 Comparison Between FE Model and Experimental Data of PES1a
Figure 21 Comparison Between FE Model and Experimental Data of PES1b
Figure 22 Comparison Between FE Model and Experimental Data of PES1c
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Figure 23 Comparison Between FE Model and Experimental Data of PES2a
Figure 24 Comparison Between FE Model and Experimental Data of PES2b
Figure 25 Comparison Between FE Model and Experimental Data of PES2c
5. CONCLUSION
From the results it is found that, of all the 6 specimens, partially encased slab with 80 mm of
ISMB 300 inside the slab carries the most ultimate load of 475 kN compared to other composite
slab specimens. Hence it is inferred that the said slab can be preferred most. Compared to slabs
with ISMB 200 insertions, slabs with ISMB 300 insertions are able to carry more load. It is also
found that when applying point load, the amount of deflection is more at the center of the
composite slab.
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