Strengthening of small concrete columns by natural fiber ...
Transcript of Strengthening of small concrete columns by natural fiber ...
Ref. code: 25595722040218TUO
STRENGTHENING OF SMALL CONCRETE COLUMNS
BY NATURAL FIBER REINFORCED POLYMERS
COMPOSITES (HEMP FRP AND SISAL FRP)
BY
ARISSAMAN SANGTHONGTONG
A THESIS SUBMITTED IN PARTIALFULFILLMENT OF THE
REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE
(ENGINEERING AND TECHNOLOGY)
SIRINDHORN INTERNATIONAL INSTITUTE OF TECHNOLOGY
THAMMASAT UNIVERSITY
ACADEMIC YEAR 2016
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STRENGTHENING OF SMALL CONCRETE COLUMNS
BY NATURAL FIBER REINFORCED POLYMERS
COMPOSITES (HEMP FRP AND SISAL FRP)
BY
ARISSAMAN SANGTHONGTONG
A THESIS SUBMITTED IN PARTIAL FULFILLMENT OF THE
REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE
(ENGINEERING AND TECHNOLOGY)
SIRINDHORN INTERNATIONAL INSTITUTE OF TECHNOLOGY
THAMMASAT UNIVERSITY
ACADEMIC YEAR 2016
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Abstract
STRENGTHENING OF SMALL CONCRETE COLUMNS BY NATURAL FIBER
REINFORCED POLYMERS COMPOSITES (HEMP FRP AND SISAL FRP)
by
ARISSAMAN SANGTHONGTONG
Bachelor of Engineering (Civil Engineering and Technology), King Mongkut’s
University of Technology North Bangkok, 2014
Master of Science (Engineering and Technology), SIIT Thammasat University, 2016
During the last decade, the use of fiber reinforced polymer (FRP)
composites has been successfully promoted for external confinement of reinforced
concrete (RC) columns all over the world. This technique is considered superior to
conventional concrete and steel jacketing methods in terms of confinement strength,
post-retrofit ductility, sectional areas, weight, corrosion resistance, ease of
application, and overall project costs. The existing research on FRP confined concrete
column is mainly concentrated on the use of artificial fibers such as carbon, glass,
aramid, PET and PEN. This research presents results of an experimental study on the
behavior of axially loaded concrete columns that have been strengthened with natural
fiber reinforced polymer (CFRP) composites. Both hemp and sisal natural fibers were
investigated. Six series, forming a total of 90 specimens, were subjected to axial
compression. All the test specimens were loaded to failure in axial compression and
investigated in both axial and transverse directions. The parameters considered are the
shape of cross section shape (i.e. circular, square and rectangular); the size of column;
the number of fiber wrap layers (i.e., two and four layers) and the fiber material such
as hemp and sisal. The experimental results clearly demonstrate that the CFRP
confinement enhances the compressive strength and the ductility of concrete columns.
The ultimate strength and the ductility of the NFRP confined concrete increase with
increasing number of confining layers. The efficiency of NFRP confinement is very
sensitive to the column cross section geometry. When column sizes increase there is a
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reduction in ultimate stress both for NSFRP and NHFRP strengthened specimens. The
NHFRP strengthening is more efficient than NSFRP
Keywords: Compressive behavior, hemp, strengthening, deformability, Hemp Fiber,
Sisal Fiber, Reinforced polymer (FRP)
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Acknowledgements
The author would like to express his appreciation of gratitude to his
advisor, Prof. Dr. Amorn Pimanmas, for his valuable suggestions, constructive
criticism, discussion and persistent supervision. The sincere appreciation is also
extended to Assoc. Prof. Dr. Winyu Rattanapitikorn and Asst. Prof. Dr. Suniti Suparp
for their serving as members of the examination committee. The sincere thanks are
also Dr. Qudeer Hussain for his helps and suggestions.
In addition, the author would like to thanks are also extended to Asian
Institute of Technology (AIT) for supporting test facilities.
Finally, I must express my very profound gratitude to my parents and to
my friend for providing me with unfailing support and continuous encouragement
throughout my years of study and through the process of researching and writing this
thesis. This accomplishment would not have been possible without them. Thank you.
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Table of Contents
Chapter Title Page
Signature Page i
Abstract ii
Acknowledgements iv
Table of Contents v
List of Table viii
List of Figures ix
1 Introduction 1
1.1 General 1
1.2 Significant of Study 2
1.3 Statement of Problems 2
1.4 Purpose of Study 2
2 Literature Review 3
2.1 Introduction 3
2.2 Cylinder Concrete columns with CFRP 3
2.3 Square Concrete columns with CFRP 5
2.4 Cylinder and Square Concrete columns with CFRP 8
2.5 Cylinder, Square and Rectangular Concrete columns
with CFRP 11
2.6 Cylinder and square concrete columns with aramid FRP 14
2.7 Properties of Natural Fiber 16
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3 Tentative Designed-Method 19
3.1 Proposal Research program 19
3.2 Experimental Program 19
3.3 Strengthening Scheme 22
3.4 Loading setup 22
4 Specimens Preparation 23
4.1 Fiber Strengthening 23
4.2 Epoxy Resin 25
4.3 Concrete Preparation 26
4.4 Casting 28
4.5 Corners Preparation 29
4.6 Strengthening 30
4.7 Capping 31
4.8 Test set up 32
4.8.1 Strain gauge 32
4.8.2 Load setup 32
5 Conclusions and Recommendations 35
5.1 Analysis Failure Modes 35
5.1.1 Circular specimens 35
5.1.2 Square and Rectangular specimens 36
5.2 Load Capacity of Concrete Columns 36
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5.2.1 Circular column specimens 37
5.2.1.1 Circular 1 (50x100) 37
5.2.1.2 Circular 2 (100x200) 37
5.2.1.3 Circular 3 (150x300) 38
5.2.2 Square column specimens 41
5.2.2.1 Square 1 (50x50x100) 41
5.2.2.2 Square 2 (100x100x200) 42
5.2.2.3 Square 3 (150x150x300) 42
5.2.3 Rectangular column specimens 46
5.2.3.1 Rectangular 1 (50x100x100) 46
5.2.3.2 Rectangular 2 (100x150x200) 46
5.2.3.3 Rectangular 3 (150x225x300) 47
5.3 Effect of Fiber thickness 50
5.4 Effect of Fiber material 54
5.5 Effect of Section shape 54
5.6 Effect of Size 54
References 61
Appendices 64
Appendix A 65
Appendix B 80
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List of Tables
Tables Page
2.1 Properties of Hemp Fiber 16
2.2 Properties of natural and synthetic fibers 17
3.1 Properties of specimens 20
4.1 Mechanical properties of sisal FRP composites using epoxy resin 24
4.2 Mechanical properties of hemp FRP composites using epoxy resin 25
4.3 Mechanical properties of epoxy resin 27
4.4 Concrete mix composition (per cubic meter) 17
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List of Figures
Figures Page
2.1 Test and Instrumentation Configurations 4
2.2 Example of Failure Condition 4
2.3 Test Setup for Columns with Eccentric Loadings 5
2.4 (a) Creep testing machine and (b) Compression test machine 6
2.5 Specimen dimensions 6
2.6 Axial stress versus CFRP strain and axial strain for
small wrapped prisms 7
2.7 Axial stress versus CFRP strain and axial strain for
medium wrapped prisms 7
2.8 Axial stress versus CFRP strain and axial strain for
large wrapped prisms 8
2.9 (a) Effect of size on peak axial stress
(b) Effect of size on peak axial strain 8
2.10 Stress strain curves of normal strength for CFRP confined specimens 9
2.11 Stress strain curves of high strength forCFRP confined specimens 10
2.12 Failed unconfined and confined square specimens 11
2.13 Failed unconfined and confined cylindrical specimens 11
2.14 Cross section types and strengthening of tested columns 12
2.15 Obtained stress-strain curves for confined circular, square
and rectangular columns 13
2.16 Compressive strength and ultimate strains value for
the tested concrete column 14
2.17 Geometric characteristic of specimens (mm) 15
2.18 Types of axial stress-strain curves 15
2.19 Failure modes of confined specimens 16
2.20 Hemp fiber in concrete 17
2.21 (a) Tensile fracture sample of sisal FRP
(b) Sisal fabric reinforced RC beam 18
3.1 Details of test specimen (units in mm) 21
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3.2 Loading setup 22
4.1 (a) Sisal Fiber (b) Hemp fiber (c) Sisal fabric (d) Hemp fabric 23
4.2 Epoxy resin 26
4.3 Preparation of concrete mixing 27
4.4 Slump test 28
4.5 Concretes casting in the molds 28
4.6 Column specimens 29
4.7 Square and rectangular cross section columns 30
4.8 Strengthening of specimens 31
4.9 Column specimens after capping 31
4.10 Strain gauge on Column specimens 32
4.11 Strain gages setup 33
4.12 Loading set 34
4.13 Column specimens on UTM 34
5.1 Axial stress – axial deformation curves of circular columns 38
5.2 Axial stress – axial deformation curves of square columns 43
5.3 Axial stress – axial deformation curves of rectangular columns 47
5.4 Comparison of normalized stress (Effect of fiber thickness) 51
5.5 Comparison of normalized stress (Effect of fiber material) 55
5.6 Comparison of normalized stress (Effect of section shape) 58
5.7 Comparison of normalized stress (Effect of size) 59
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Chapter 1
Introduction
1.1 General
The need for strengthening or retrofitting reinforced concrete (RC) and pre-
stressed concrete (PC) structures is becoming more apparent, particularly when there
is an increase in load requirements, a change in use, a degradation problem, or some
design/construction defects. Increase in load is mainly because of natural disasters
such as earthquake. At present, earthquakes are occurring all over the world. These
earthquakes are occurring at a higher rate than ever before and pose a much greater
risk to people living nearby. The structures which were designed prior to development
of modern seismic codes maybe destroyed during any earthquake event. Potential
solutions range from replacement of the structures to strengthening with a variety of
techniques. The use of Fiber reinforced polymer (FRP) materials for structural repair
presents several advantages and had been recently investigated all over the world.
These FRP composites are usually comprised of uni-directional or bi-directional
carbon, glass, and aramid fiber with suitable epoxy resin. Other types of FRP are
sprayed FRP, in which chopped glass or carbon fibers are sprayed on the surface of
concrete structures. The resulted material is randomly distributed fibers with resin,
which can be used for strengthening purpose. The main advantages of these FRP
materials are due to their light weight, high strength and stiffness, resistance to
corrosion, flexibility, and ease of application. However these conventional FRP are
usually chemical based which are hazardous to the environment. In addition these
FRP are relatively expensive.
In contrast to the conventional chemical based FRPs, recently a new method
of strengthening “Natural Fiber Reinforced Polymer (NFRP)” has been studied.
Natural fibers are usually made from plant leaves which are environment friendly and
low price compared with chemical based FRPs. The additional advantages of natural
fibers are high toughness and acceptable engineering properties. The present research
work is aimed to investigate the potential use of different natural fibers such as Sisal
and Hemp fibers for seismic strengthening or rehabilitation of the concrete structures.
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1.2 Significant of Study
A detail review of exiting literature shows that few research efforts are
available to enhance strength and ductility of reinforced concrete member by using
natural fibers. Further these available studies were mostly conducted on small scale
reinforced concrete columns using sisal and hemp fibers. However no research
activity is found on potential use of natural fibers such as Hemp and Sisal for seismic
strengthening of RC large scale columns. The present study will provide a better
understanding about Natural Fiber Reinforced Polymer Composites.
1.3 Statement of Problems
During severe earthquake, the structure is likely to undergo inelastic
deformation and has to depend on the ductility and energy absorption capacity to
avoid collapse. Such buildings designed for gravity loading need to be strengthened to
increase strength, stiffness and ductility. In this study, the effect of NFRP composites
on strength and ductility of low rise buildings (1-2 stories) will be investigated in
detail.
1.4 Purpose of Study
The main objective of this study is to investigate the potential use of natural
fiber such as hemp fiber and sisal fiber to enhance strength and ductility of reinforced
concrete members. The research parameters included will be concrete columns such
as shape of concrete columns there are three shapes as cylinder, rectangular and
square, the size of concrete columns there are three sizes as small, medium and large
and the number of FRP layers (2 and 4 layers). All specimens were tested by axial
compressive load. These concrete columns will be strengthened using natural fibers
with epoxy resin.
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Chapter 2
Literature review
2.1 Introduction
In the past, Fiber reinforced polymer (FRP) composite have been successfully
applied to retrofit and strengthen RC members. Several composite jacketing systems
have been developed and validated in research. Many researchers are being developed
in different research centers, in order to study the behavior of concrete strengthened
with FRP. These studies mainly focused to investigate different retrofitting methods
to enhance the flexural strength, ductility and shear strength of reinforced concrete
columns confined with glass and carbon fibers. The parameters considered were
number of composite layers, the compressive strength of the unconfined concrete and
the cross-section shape.
2.2 Cylinder Concrete columns with CFRP
Y. Xiao and H. Wu [1] studied axial compression test results of 27 concrete
cylinders confined (diameter of 152 mm and a height of 305 mm) by carbon fiber.
The main parameters are unconfined concrete strength and thickness (1 to 3 layers) of
carbon fiber composite jackets. The concrete strengths were 27.6 MPa, 37.9 MPa and
48.2 MPa for lower, medium and higher strength concrete, respectively. All the
specimens were tested using a high-stiffness, high-capacity compression testing
machine. The result showed that the strength and ductility of concrete can be achieved
by carbon fiber composite jacketing. The efficiency performance is higher for lower
concrete strength than high concrete strength. The stress-strain performances of
confined concrete with carbon fiber after exceeding unconfined concrete strength
exhibit an approximately bilinear behavior which can be formulated by empirical
equations from the tests.
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Fig.2.1 Test and Instrumentation Configurations
The final failure corresponding to the rupture of the carbon fiber jacket was very
explosive. For concrete cylinders confined by carbon and E-glass, the typical failure is
shown in Fig.2.2
Fig.2.2 Example of Failure Condition
J.F. Berthet and all [2] studied the influences of the confinement level and mechanical
properties of the jacket sand the compressive strength of concrete. Five different
concretes have been tested and two level of jackets. The behaviors of different
confined specimens were compared to evaluate the influence of the jacket properties
on the stress–strain response. This result has shown that the ultimate strengths and
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strains increase with the enhancement of the number of composite layers and bilinear
behavior of confined concrete. The curvature of the transition zone and the slope of
the pseudo-plastic branch depend on the jacket stiffness. The failures of the specimens
occurred before the shell fibers reached their ultimate strain capacities at the middle
high of column.
2.3 Square Concrete columns with CFRP
Azadeh Parvin and Wei Wang [3] proposed FRP (Carbon fiber) confined
square concrete columns under axial compressive loading with small eccentricities.
FRP coupon test was conducted to estimate the tensile strength, the modulus of
elasticity. This research investigates the effect of strain gradient and FRP thickness
(one and two layers). Additionally, control specimens without FRP jackets were
tested for comparison. When the axial load was added until the columns failed, the
unconfined concrete failed by crushing of the concrete on the side with larger
compression near the column mid-height. For one and two layers, the jacket was
separated from concrete surface.
Fig.2.3 Test Setup for Columns with Eccentric Loadings
Dian Jie Zhang and all [4] proposed the results of experimental and theoretical
investigations on the stress and strain of short square concrete columns confined by
fiber reinforced polymer (FRP) after creep by the creep testing. The specimen was
placed on the machine and first compressed to 30% of the theoretical ultimate load
which was recorded by the vibrating string strain gauge.
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Fig.2.4 (a) Creep testing machine and (b) Compression test machine.
The results shown the creep does not have an effect on the stress strain curves but that
increases the elastic modulus and slightly decreases the compressive strength of
square concrete columns. The comparison between the model predictions and the
experimental results showed good agreement.
Mark J. Masia and all [5] were investigating the carbon fiber reinforced polymer
(CFRP) wrapping to strengthen plain concrete prisms. The prisms of three different
square cross-sectional sizes (100 mm×100 mm× 300 mm, 125 mm×125 mm×375
mm, 150 mm×150 mm×450 mm) were tested under axial load in compression until
failure occurred. The axial stiffness for each prism was calculated base on the
procedure for determining the elastic modulus E of concrete (AS 1012.17).
Fig.2.5 Specimen dimensions.
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When the prism cross-sectional size was increased for a fixed corner radius, the
effectiveness of confinement was reduced. The effect of size was as significant as its
effect on the increase in strength has shown in Fig.2.6-2.8 for small, medium and
large column, respectively. Thus, significant increases in strength and ductility were
achieved by wrapping. The initial failure occurred when the brittle CFRP wrapping
suddenly ruptured at a corner. At these locations, the measured strains were found
higher than other positions.
Fig.2.6 Axial stress versus CFRP strain and axial strain for
small wrapped prisms.
Fig.2.7 Axial stress versus CFRP strain and axial strain for
medium wrapped prisms.
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Fig.2.8 Axial stress versus CFRP strain and axial strain for
large wrapped prisms.
Fig.2.9 (a) Effect of size on peak axial stress (b) Effect of size on peak axial strain
2.4 Cylinder and Square Concrete columns with CFRP
R.Benzaid and all [6] proposed the behavior of axially loaded short reinforced
concrete (RC) columns that have been strengthened with carbon fiber-reinforced
polymer (CFRP). Total of 48 specimens are circular and square RC columns and
unconfined concrete were subjected to axial compression. The parameters considered
are the shape of cross section shape, the number of CFPR layers (1 and 3 layers), the
concrete strength (high and normal strength) and plain concrete (PC) and reinforce
concrete (RC) columns. For all RC specimens the diameter of longitudinal and
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transverse reinforcing steel bars were respectively 12 mm and 8 mm. The longitudinal
steel ratio was constant for all specimens and equal to 2.25%.The experimental results
demonstrate that the ultimate strength and the ductility of the CFRP confined concrete
increase with increasing number of confining layers. The increase in strength and
ductility is more significant for lower strength concrete. The efficiency of the CFRP
confinement is higher for circular than for square sections, as expected. The increase
of ultimate strength of sharp edged sections is low as shown Fig.2.10
(a) Cylinder of PC column series (b) Cylinder of RC column series
(c) Square of PC column series (d) Square of RC column series
Fig.2.10 Stress strain curves of normal strength for CFRP confined specimens
The CFRP confinement on low-strength concrete specimens produced higher results
in terms of strength and strains than for high-strength concrete as shown Fig.2.11
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(a) Cylinder of PC column series (b) Cylinder of RC column series
(c) Square of PC column series (d) Square of RC column series
Fig.2.11 Stress strain curves of high strength for CFRP confined specimens
The failure of CFRP wrapped specimens occurred in a sudden and explosive manner.
For cylindrical specimens, the fiber rupture started mainly in the central zone, but
square specimens failed near a corner, because of the high stress concentration. CFRP
strengthened specimens showed a typical bi-linear trend with a transition zone.
Yousef A. Al-Salloum and all [7] reported the influence of the radius of the cross-
sectional corners (edges) of about 1/6, 1/4, and 1/3on the strength of small scale
square concrete column specimens confined with FRP composite laminates and
cylinder column. These specimens were tested in uniaxial compression. All columns
were instrumented with strain gauges at mid-height of unconfined and confined
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specimens to measure lateral strains. To measure axial strain, each specimen was
fitted with LVDTs. The load was applied at a loading rate of 4 kN/s. The best
performance was that of the circular specimens. The performances of square
specimens are directly related to the radius of the cross-section edges. The failure of
the square columns always starts at one of the corners while the failure of cylinder
column started at the middle height. In addition, analytical model is presented to
predict the strength of FRP-confined. There are excellent agreements with the
measured ones.
Fig.2.12 Failed unconfined and confined square specimens
Fig.2.13 Failed unconfined and confined cylindrical specimens
2.5 Cylinder, Square and Rectangular Concrete columns with CFRP
I.A. E. M. Shehata and all [8] investigated the gain in strength and ductility of
concrete columns confined by CFRP. Total of 54 short column specimens with
circular column, square column and rectangular column and with the ratio of
specimens height/short size length of the section equal to 2, were tested. The number
of CFRP sheet layers applied to the models was one or two layers. The results of an
experimental program were studied on the behavior of short concrete column. These
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obtained experimental strengths and ultimate strains are compared with the equations
to estimate the confined concrete strength under a constant rate of compressive axial
load (0.22 MPa/s) until their failure.
Fig.2.14 Cross section types and strengthening of tested columns.
The obtained results as shown in Fig.2.15 can be clearly noticed that both the stress
and strain at failure for the confined columns were higher than those for the
unconfined ones and the highest values were obtained for confined circular columns
with 2 CFRP layers. The strengths and ultimate strains were increased when the
number of sheet layers increased. The failure modes for all confined columns with 1
layer have a mid height of the column and one-fourth to midway of the height with 2
layers. For the square and rectangular columns, the failure occurred at one of the
columns corners.
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Fig.2.15 Obtained stress-strain curves for confined circular, square
and rectangular columns.
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Fig.2.16 Compressive strength and ultimate strains value for
the tested concrete column
2.6 Cylinder and square concrete columns with aramid FRP.
Yuan-feng Wang and Han-liang Wu [9] studied concrete short columns
confined with aramid FRP (AFRP). In this study, 99 confined concrete short columns
wrapped with circular and square cross sections were tested under axial compressive
loading and the effect of size and concrete strength was studied. The height to width
ratio or diameter was constantly equal to 3. In each group of circular specimens, there
were three different scaling dimensions 70×210 mm for the small cylinders, 105×315
mm for the medium one, and 194×582 mm for the large one. In each group of square
specimens, the sizes were 70×210 mm for the small square column, 100×300 mm for
the medium column and 150×450 mm for the large column. The geometric
characteristic of the specimens is shown in Fig.2.17
Fig.2.17 Geometric characteristic of specimens (mm)
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The experimental nominal axial stress-strain curves of the confined specimens are
characterized by three types as in Fig.2.18. The curves are bilinear by two key points
are the kink or transitional point (TP) and the end or ultimate point on the curve (UP).
For the specimen with a higher confinement ratio (confinement pressure per strength
of unconfined concrete), the shape will be the first type where the specimen can reach
the load until point TP and increased to point UP. The third type curve was for the
specimen with a smaller confinement ratio and they failed at the ultimate point.
(a) Type I (b) Type II (C) Type III
Fig.2.18 Types of axial stress-strain curves
For the failure mode, the AFRP ruptured either at the mid height or at the end of the
circular specimens. For the square specimens, stress concentrations in the regions
close to the corners led to the rupture of the AFRP sheets as shown in Fig. 2.19.
Fig.2.19 Failure modes of confined specimens
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2.7 Properties of Natural Fiber
Zhijian Li and all [10] studied the mechanical and physical properties of hemp
fiber reinforced concrete (HFRC). The results of the physical and mechanical
properties of HFRC showed that fiber factors (fiber content) have a significant
relationship with the mechanical and physical properties of cementations materials.
The properties of hemp fiber are shown in Table 2.1.
Table2.1 Properties of Hemp Fiber.
Properties Values
Specific gravity (g/mm3)
Fiber Content (%)
1.5
30 – 40
Width (µm) 23.15+ 17.60
Water absorption (%) 85-100
Tensile strength (MPa) 900
Modulus of elasticity (GPa) 34
Natural fibers are a high tensile strength and they have a low modulus of elasticity. F.
P. TORGAL and all [11] proposed that their tensile performance compares favorably
to synthetic fibers. Tensile strength and modulus of elasticity of hemp fiber is highest.
Table2.2 Properties of natural and synthetic fibers
Properties Specific gravity
(kg/m3)
Water
absorption (%)
Tensile
strength (MPa)
Modulus of
elasticity (GPa)
Sisal 11370 110 347-378 15.2
Coconut 1177 93.8 95-118 2.8
Bamboo 1158 145 73-505 10-40
Hemp 1500 85-105 900 34
Banana 1031 407 384 20-51
Polypropylene 913 - 250 2.0
I. Merta and all [12] reported the fracture energy of concrete reinforced with natural
fibers of hemp, elephant grass, and wheat straw, there are contained in concrete
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with0.19% of fibers by weight and of 40 mm of length were uniaxially tested with the
wedge splitting test (WST) method .The hemp fiber as reinforcement produces the
enhancement of the concrete fracture energy up to 70% compared to unreinforced
concrete and up to 2% and 5% for straw and elephant grass fiber, respectively. The
beneficial effect of hemp fiber is believed to be the result of the fiber high tensile
strength.
Fig.2.20 Hemp fiber in concrete
M.Ramesh and all [13] investigated the mechanical properties such as tensile and
flexural properties of hybrid glass fiber-sisal/jute reinforced epoxy composites. The
sisal/GFRP composite samples possess good tensile strength and can withstand the
strength up to 68.55 MPa. The jute/GFRP composite specimen is holding the
maximum flexural load of 1.03KN, slightly higher than the sisal/GFRP composite
sample. Whereas, Tara Sena and all [14] investigated the mechanical characterization
of the FRP and strengthening effects provided by the bonding of sisal FRP to beams
over bonding of carbon FRP and glass FRP. For the sisal FRP, it increased the
flexural strength as well as the tensile strength. The sisal FRP composite exhibited a
tensile strength of 223.367 N/mm2, which was 24% of the tensile strength of CFRP
(923.056 N/mm2) and 33% of the tensile strength of GFRP (678.571 N/mm
2). The RC
beam strengthened by SFRC showed highest amount of ductility and delayed the
formation of cracks without rupture failure. This result showed that the reinforcement
of woven sisal fiber reinforced polymer composites created a new alternate material.
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Fig.2.21 (a) Tensile fracture sample of sisal FRP (b) Sisal fabric reinforced RC beam
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Chapter 3
Tentative Designed-Method
3.1. Proposal Research program
In order to investigate the efficiency of natural hemp fiber and sisal fiber, the
proposed research work is divided into two parts.
A) Strengthening of concrete columns using hemp fibers. The main objective of this
experimental program is to evaluate the strengthening efficiency of natural hemp
fibers to enhance strength and ductility of concrete columns.
B) Strengthening of concrete columns using sisal fibers. The main objective of this
experimental program is to evaluate the strengthening efficiency of natural sisal fibers
to enhance strength and ductility of concrete columns.
The research parameters included are shape of concrete columns, size of
columns, number of layers and type of natural fibers (i.e. sisal and hemp fiber).
3.2 Experimental Program
The experimental program will be comprised of testing of 90 concrete
columns strengthened using natural fibers. The shapes of concrete columns consisted
of three groups such as cylinder, square and rectangular and they have three sizes for
each group. Each group has 30 specimens for difference in the type of fiber and
number of confinement. In all test conditions, there will be 2 specimens for the same
condition to find average value of the results. Table 3.1 shows the detail of specimens
in this experiment.
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Table3.1 Properties of specimens
Main
Groups
Subgroups
(size – mm) Specimen
NFRP
material
NFRP
thickness
(layers)
Number of
specimens
Circular Circular 1
(50 x 100)
C1-CON - - 2
C1-S-2 Sisal 2 2
C1-S-4 Sisal 4 2
C1-H-2 Hemp 2 2
C1-H-4 Hemp 4 2
Circular 2
(100 x 200)
C2-CON - - 2
C2-S-2 Sisal 2 2
C2-S-4 Sisal 4 2
C2-H-2 Hemp 2 2
C2-H-4 Hemp 4 2
Circular 3
(150 x 300)
C3-CON - - 2
C3-S-2 Sisal 2 2
C3-S-4 Sisal 4 2
C3-H-2 Hemp 2 2
C3-H-4 Hemp 4 2
Square Square 1
(50 x 50 x
100)
S1-CON - - 2
S1-S-2 Sisal 2 2
S1-S-4 Sisal 4 2
S1-H-2 Hemp 2 2
S1-H-4 Hemp 4 2
Square 2
(100 x 100 x
200)
S2-CON - - 2
S2-S-2 Sisal 2 2
S2-S-4 Sisal 4 2
S2-H-2 Hemp 2 2
S2-H-4 Hemp 4 2
Square 3
(150 x 150 x
300)
S3-CON - - 2
S3-S-2 Sisal 2 2
S3-S-4 Sisal 4 2
S3-H-2 Hemp 2 2
S3-H-4 Hemp 4 2
Rectangular Rectangular1
(50 x 100 x
100)
R1-CON - - 2
R1-S-2 Sisal 2 2
R1-S-4 Sisal 4 2
R1-H-2 Hemp 2 2
R1-H-4 Hemp 4 2
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Main
Groups
Subgroups
(size – mm) Specimen
NFRP
material
NFRP
thickness
(layers)
Number of
specimens
Rectangular Rectangular2
(100 x 150 x
200)
R2-CON - - 2
R2-S-2 Sisal 2 2
R2-S-4 Sisal 4 2
R2-H-2 Hemp 2 2
R2-H-4 Hemp 4 2
Rectangular3
(150 x 225 x
300)
R3-CON - - 2
R3-S-2 Sisal 2 2
R3-S-4 Sisal 4 2
R3-H-2 Hemp 2 2
R3-H-4 Hemp 4 2
Fig.3.1 Details of test specimen (units in mm)
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3.3 Strengthening Scheme
The strengthening scheme is designed for the following objectives. To study
the influence of type of confined jacket effect on the strengthening. The results will be
compared in terms of the percentage of effective strength between hemp and sisal
fibers. In addition, the study the influence of number of confined jacket layers as 2
and 4 layers on the strengthening. The results will be compared in terms of the
percentage of effective strength between 2 and 4 layers confinement layers provided
all other conditions remained the same.
3.4 Loading setup
The compressive load was applied at a constant rate of 100 N/minute with a
maximum load capacity of 200 ton and the load was recorded with an automatic data
acquisition system. The axial load, vertical displacement, lateral expansion, and strain
were recorded by a load cell mounted on a hydraulic jack. The specimen was then
loaded under the manual control until failure.
Fig.3.2 Loading setup
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Chapter 4
Specimens Preparation
4.1 Fiber Strengthening
Natural sisal fibers were obtained from farms in Cha Am district, whereas
natural hemp fibers were obtained from farms in Konken district, Thailand. Sisal and
hemp fibers were extracted from the Agava Sisalana and Cannabis plan leaves,
respectively, A thin flat strip of fiber (see Fig 4.1(a) and Fig 4.1(b)) having a constant
rectangular cross section. The average thickness of fabric was 1.5 mm as shown in
figure 4.1 (c) and 4.1 (d).
Fig.4.1 (a) Sisal Fiber
Fig.4.1 (b) Hemp Fiber
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Fig.4.1 (c) Sisal fabric
Fig.4.1 (d) Hemp fabric
The tensile strength of sisal FRP composites were determined by testing the
strip specimens of sisal FRP in accordance with ASTM Standard D638 [28]. The
mechanical properties of sisal FRP composites are given in Table 4.1.
Table4.1 Mechanical properties of sisal FRP composites using epoxy resin
Properties Value Units
Tensile strength 104 MPa
Fracturing strain 0.41 %
Ultimate strain 3.48 %
Modulus of elasticity 3.19 GPa
The tensile strength of sisal FRP composites fiber were determined by testing
the strip specimens of sisal FRP in accordance with ASTM Standard D638 [28]. The
mechanical properties of GCSM composite are given in Table 4.2.
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Table4.2 Mechanical properties of hemp FRP composites using epoxy resin
Properties Value Units
Tensile strength 156 MPa
Fracturing strain 0.505 %
Ultimate strain 2.035 %
Modulus of elasticity 6.414 GPa
4.2 Epoxy Resin
The resin used in the experimental program was “Smart CF-Resin”
manufactured by Smart and Bright Co. Ltd. Thailand. The Smart CF-Resin is two part
high performance epoxy resin. Part A is comprised of epoxy resin and part B is a
hardener. Both parts are mixed together with the mixing ratio of 2:1 (i.e. A:B = 2:1).
The resin can be easily applied using trowel, roller or brush. The mechanical
properties of resin (curing time, tensile strength, tensile modulus and elongation at
break) of the resin as provided by the manufacturer are given in Table 4.3
Table4.3 Mechanical properties of epoxy resin
Properties Smart CF-Resin Unit
Curing time 7-10 Hours
Tensile strength 40-45 MPa
Flexural strength 70-75 MPa
Elongation at break 2.5 %
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Fig.4.2 Epoxy resin
4.3 Concrete Preparation
As the first step for preparation of specimens, the concrete mix was slowly
poured into the forms to prevent segregation. The concrete columns were made using
Type I Portland cement. The concrete mix proportion consists of 272 kg of cement,
221 kg of water, 721 kg of sand and 1,187 kg of aggregates. For the concrete property
tests, the slump test (ASTM C143) [16] is an empirical test that measures the
workability of fresh concrete to check the consistency of freshly made concrete which
is being filled in the molds. The test is carried out using a mould known as a slump
cone in three layers. Each layer is tamped 25 times with a steel rod to ensure
compaction. The third layer is finished off level with the top of the cone. The cone is
carefully lifted up. The decrease in the height of the center of the slumped concrete is
called “slump”. The amount of slump is measured in inches from the bottom of the
straight edge to the top of the slumped concrete. The slump is controlled near 8 cm. If
the slump is over the control range, a new mixing is required.
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Table4.4 Concrete mix composition (per cubic meter)
Components Quantity (kg)
Cement 272.00
Water 221.00
Sand 720.00
Gravel 1187.0
Water-to-cement ratio (W/C) 0.65
Fig.4.3 Preparation of concrete mixing
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Fig.4.4 Slump test
4.4 Casting
A ready-mix concrete was used in the molds and the vibrator was used to
vibrate the concrete carefully to prevent voids from forming during concreter filling
.A ready-mix concrete was used in the molds as shown in Fig .4.5. After 28 days of
curing, the compressive strength of concrete is controlled to be20MPa (ASTMC39)
[17] by testing a standard cylinder specimen with diameter of 15cm and height of 30
cm at 28 days for curing time. The concrete specimens were cleaned and completely
dried before the resin was applied.
Fig.4.5 Concretes casting in the molds
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Fig.4.6 Column specimens
4.5 Corners Preparation
Before strengthening, corners of the square and rectangular cross section
columns were rounded off to a radius of about 10, 20, 30 mm for the small, medium
and large columns, respectively (see Fig.4.7) in order to prevent breakage of the
natural fiber sheets due to sharp edges and the concrete surface of all columns was
cleaned and completely dried before applying resin.
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Fig.4.7 Square and rectangular cross section columns
4.6 Strengthening
The natural fibers were applied to the specimens by manual wet lay-up
process. A thin layer of primer epoxy was first applied to the concrete surface. After
the primer epoxy on the concrete surface was cured at the ambient temperature for
several hours the first fiber was carefully placed into the resin with gloved hands and
smooth out any air pockets. After installing the first layer, a second layer of resin was
applied to allow the impregnation of the second layer of the HFRP and SFRP. The
following layer is applied in the same way. Finally, a layer of resin was applied to
complete the operation. [18,19]
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Fig.4.8 Strengthening of specimens
4.7 Capping
Each layer had an overlap of about 100 mm to assure the development of full
composite strength. After strengthening, all column had their ends (top and bottom)
capped with plaster to assure parallel surfaces and uniform load distribution. [10,17]
Fig.4.9 Column specimens after capping
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4.8 Test set up
4.8.1 Strain gauge
The instrumentation is completed by strain gages bonded axially and
transversely at mid-height of specimens. The gages are bonded on the concrete
surface in the case of unconfined columns and on the composite shell for confined
concrete columns.
Fig.4.10 Strain gauge on Column specimens
4.8.2 Load setup
Both ends of all strengthened specimens were additionally wrapped
with two 20 mm wide strips of Glass Fiber Reinforced Polymer (GFRP) sheets to
avoid premature failure of NFRP shells at the ends. The compressive load was applied
a constant rate increasing of 4 kN/s and strains was recorded with an automatic data
acquisition system. All of the specimens were tested under concentric compression
using a testing machine with a maximum load capacity of 1,000 kN at AIT laboratory.
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The axial load, vertical displacement, lateral expansion, and strain were recorded and
measured by a load cell mounted on a hydraulic jack. Deflections were measured at
the bottom of concrete column by electronic LVDT transducers. On the top end of the
specimens were applied by gypsum in order to avoid direct eccentric load during the
test and the steel plate with 12 mm thickness, 150x150mm was applied to avoid the
direct eccentric load. Then, the load is applied at a constant rate of4 kN/s. The
comparison of the readings of the two vertical LVDTs located at the left- and right-
hand sides was implemented. The specimen was loaded under the manual
displacement control manner until failure. All specimens were instrumented by
electrical resistance strain gauges for measuring compressive strain at the mid-height
of the column. [18]
Fig.4.11 Strain gages setup
150x150
L1
L2
Vertical Strain Gages
Horizontal Strain Gages
150x150
LVDT
Steel Frame
Clamping Screw
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Chapter 5
Conclusions and Recommendation
All concrete column specimens were tested under monotonic uniaxial
compression up to failure in a Universal Testing Machine of 1000 kN capacity. The
load was applied at a constant rate of 4 kN/s and the strains were measured at the load
interval of 120 kN by an electronic data logger. Prior to the testing, some
arrangements were made to accurately measure the data and to avoid any possibility
of premature failure. These arrangements included;
1) All NFRP-confined and unconfined specimens were capped with sulfur mortar pad
at both ends to ensure a full contact surface, which results in a uniform distribution of
load over the entire cross sectional area.
2) The sulfur mortar cap was trimmed off over the NFRP jackets to avoid the
possibility of transmitting the axial load onto the fiber shell area.
3) Both ends of all strengthened specimens were additionally wrapped with two 20
mm wide strips of Glass Fiber Reinforced Polymer (GFRP) sheets to avoid premature
failure of NFRP shells at the ends.
4) In addition to the sulfur mortar capping, steel plates of 5 mm thickness were placed
at both ends to ensure the application of load over the confined concrete area and to
avoid any accidental axial load transfer onto the fiber shell especially when the
specimen undergoes a large deformation near the failure. Linear variable differential
transducers (LVDTs) were instrumented to the specimen to record axial deformation
of concrete during loading. To ensure the safety of instruments, all LVDTs were
removed prior to the final failure of specimens.
5.1 Analysis Failure Modes
5.1.1 Circular specimens
All NFRP-confined circular specimens failed by the rupture of
NFRP composite caused by the hoop tension associated with the lateral expansion
(See the Appendix A). The failure of the confined specimens resulted from the rupture
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of NFRP composite was suddenly brittle and characterized by a large explosive
sound. Comparatively, the rupture of NHFRP composite was more explosive and
brittle than NSFRP composite. Prior to the final rupture intermittent snapping sounds
indicating progressive fracturing of fibers could be clearly observed in all confined
circular specimens. The typical failure of SFRP-confined circular specimens is shown
in the Appendix A. The failure is characterized by a fully or partly vertical splitting
rupture of SFRP shells. This failure mode indicates that the hoop tension in the SFRP
shell which is caused by the transverse strain due to the lateral expansion of the
specimen exceeds the composite strength.
5.1.2 Square and Rectangular specimens
The typical failure of NFRP-confined square and rectangular
specimens also occurred due to the rupture of NFRP composites (see the Appendix
A). Similar to the case of circular specimens, the failure of square and rectangular
specimens was sudden and explosive. When the final failure was approaching, some
snapping sounds could be heard too. In almost all square specimens, the rupture of
SFRP shell started near one of the corners of the section due to the stress
concentration except in few specimens where the rupture of SFRP shell occurred at
the column face. The rupture of confining fibers at the corners due to stress
concentration has also been reported for FRP confined square and rectangular
columns [12].
5.2 Load Capacity of Concrete Columns
The axial stress-axial deformations of all circular, square and rectangular
NFRP confined columns under uniaxial monotonic loading are shown in Figures 5.1-
5.3. Average values of tested compressive strength and deformations are given in the
Appendix B. It can be seen that the confinement from NFRP jacketing is effective to
increase the ultimate strength and deformation of circular, square and rectangular
specimens. For all NFRP-confined specimens, the increase in the ultimate stress and
deformation is observed to vary with the increase in NFRP thickness. The test results
are discussed in detail in the following sections.
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5.2.1 Circular column specimens
5.2.1.1 Circular 1 (50x100)
The dimensions of the cylinder specimens in this group were
50 mm in diameter and 100 mm in height. The axial stress and deformation curves of
all specimens are shown in Figure 5.1a and 5.1b. The control specimen failed at the
average peak stress of 15.8 MPa. Among the strengthened specimens, a maximum
increase in the peak stress of 848% over the control specimen was recorded for
specimen C1-H-4, whereas a minimum increase of 556% was measured for specimen
C1-S-2 (see the Appendix B). The remaining column specimens in this group (i.e.,
C1-H-2 and C-S-4) reached peak stresses that were 532 and 785 greater than the
control specimen, respectively. Similar to the load carrying capacity, the axial
deformations of the NFRP-strengthened concrete columns were also increased. A
maximum increase in the axial deformation was 1700%, for specimen C1-S-4.
Column specimens C1-S-2, C1-H-2 and C1-H-4 reached the peak stress at 940%,
590% and 1100% enhanced axial deformations, respectively.
5.2.1.2 Circular 2 (100x200)
The dimensions of the cylinder specimens in this group were
100 mm in diameter and 200 mm in height. The axial stress and deformation curves of
all specimens are shown in Figure 5.1c and 5.1d. The control specimen failed at the
average peak stress of 22.1 MPa. The maximum stress increase of 293% was
measured for the specimen C2-H-4 with 4 layers of NHFRP composite and the
minimum increase in peak stress of 126% was measured for column C2-S-2 with 2
layers of NSFRP composite. The increases in peak stress were 162% and 216% for
column specimens C2-H-2 and C2-H-4, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened columns were also
increased. As shown in Figure 5.1c and 11d, the increases in the axial deformations of
300%, 500%, 200% and 400% were recorded for columns C2-S-2, C2-S-4, C2-H-2
and C2-H-4, respectively.
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5.2.1.3 Circular 3 (150x300)
The dimensions of the cylinder specimens in this group were
150 mm in diameter and 300 mm in height. The axial stress and deformation curves of
all specimens are shown in Figure 5.1e and 5.1f. The control specimen failed at the
average peak stress of 26.9 MPa. Among the strengthened specimens, a maximum
increase in the peak stress of 197% over the control specimen was recorded for
specimen C3-H-4, whereas a minimum increase of 86% was measured for specimen
C3-S-2 (see the Appendix B). The remaining column specimens in this group (i.e.,
C3-H-2 and C3-S-4) reached peak stresses that were 94% and 164% greater than the
control specimen, respectively. Similar to the load carrying capacity, the axial
deformations of the NFRP-strengthened concrete columns were also increased. A
maximum increase in the axial deformation was 395%, for specimen C3-S-4. Column
specimens C3-S-2, C3-H-2 and C3-H-4 reached the peak stress at 155%, 101% and
50% enhanced axial deformations, respectively.
Fig.5.1 (a) Circular 1 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
C1-S-4
C1-S-2
C1-CON
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Fig.5.1 (b) Circular 1 with NHFRP
Fig.5.1 (c) Circular 2 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Axia
l st
ress
(M
Pa)
Axial deformation (mm)
C1-H-4
C1-H-2
C1-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
C2-S-4
C2-S-2
C2-CON
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Fig.5.1 (d) Circular 2 with NHFRP
Fig.5.1 (e) Circular 3 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
C2-H-4
C2-H-2
C2-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
C3-S-4
C3-S-2
C3-CON
Ref. code: 25595722040218TUO
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Fig.5.1 (f) Circular 3 with NHFRP
Fig.5.1 Axial stress – axial deformation curves of circular columns
5.2.2 Square column specimens
5.2.2.1 Square 1 (50x50x100)
The dimensions of the square specimens in this group were
50 mm in width, 50 mm in depth and 100 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.2a and 5.2b. The control
specimen failed at the average peak stress of 12.7 MPa. Among the strengthened
specimens, a maximum increase in the peak stress of 848% over the control specimen
was recorded for specimen S1-H-4, whereas a minimum increase of 421% was
measured for specimen S1-S-2 (see the Appendix B). The remaining column
specimens in this group (i.e., S1-H-2 and S-S-4) reached peak stresses that were 532%
and 652% greater than the control specimen, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened concrete columns were
also increased. A maximum increase in the axial deformation was 1475%, for
specimen S1-S-4. Column specimens S1-S-2, S1-H-2 and S1-H-4 reached the peak
stress at 875%, 590% and 1100% enhanced axial deformations, respectively.
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
C3-H-4
C3-H-2
C3-CON
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5.2.2.2 Square 2 (100x100x200)
The dimensions of the square specimens in this group were
100 mm in width, 100 mm in depth and 200 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.2c and 5.2d. The control
specimen failed at the average peak stress of 17.7 MPa. The maximum stress increase
of 293% was measured for the specimen S2-H-4 with 4 layers of NHFRP composite
and minimum increase in peak stress of 182% was measured for column S2-S-2 with
2 layers of NSFRP composite. The increases in peak stress were 210% and 216% for
column specimens S2-H-2 and S2-H-4, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened columns were also
increased. As shown in Figure 5.2c and 5.2d, the increases in the axial deformations
of 400%, 500%, 200% and 400% were recorded for columns S2-S-2, S2-S-4, S2-H-2
and S2-H-4, respectively
5.2.2.3 Square 3 (150x150x300)
The dimensions of the square specimens in this group were
150 mm in width, 150 mm in depth and 300 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.2e and 5.2f. The control
specimen failed at the average peak stress of 21.5 MPa. Among the strengthened
specimens, a maximum increase in the peak stress of 197% over the control specimen
was recorded for specimen S3-H-4, whereas a minimum increase of 86% was
measured for specimen S3-S-2 (see the Appendix B). The remaining column
specimens in this group (i.e., S3-H-2 and S3-S-4) reached peak stresses that were 94%
and 164% greater than the control specimen, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened concrete columns were
also increased. A maximum increase in the axial deformation was 395%, for specimen
S3-S-4. Column specimens S3-S-2, S3-H-2 and S3-H-4 reached the peak stress at
155%, 118% and 340% enhanced axial deformations, respectively.
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Fig.5.2 (a) Square 1 with NSFRP
Fig.5.2 (b) Square 1 with NHFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S1-S-4
S1-S-2
S1-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S1-H-4
S1-H-2
S1-CON
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Fig.5.2 (c) Square 2 with NSFRP
Fig.5.2 (d) Square 2 with NHFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S2-S-4
S2-S-2
S2-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S2-H-4
S2-H-2
S2-CON
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Fig.5.2 (e) Square 3 with NSFRP
Fig.5.2 (f) Square 3 with NHFRP
Fig.5.2 Axial stress – axial deformation curves of square columns
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S3-S-4
S3-S-2
S3-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
S3-H-4
S3-H-2
S3-CON
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5.2.3 Rectangular column specimens
5.2.3.1 Rectangular 1 (50x100x100)
The dimensions of the rectangular specimens in this group
were 50 mm in width, 100 mm in depth and 100 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.3a and 5.3b. The control
specimen failed at the average peak stress of 11.9 MPa. Among the strengthened
specimens, a maximum increase in the peak stress of 848% over the control specimen
was recorded for specimen R1-H-4, whereas a minimum increase of 556% was
measured for specimen R1-S-2 (see the Appendix B). The remaining column
specimens in this group (i.e., R1-H-2 and R-S-4) reached peak stresses that were 532
and 785 greater than the control specimen, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened concrete columns were
also increased. A maximum increase in the axial deformation was 1507%, for
specimen R1-S-4. Column specimens R1-S-2, R1-H-2 and R1-H-4 reached the peak
stress at 829%, 516% and 971% enhanced axial deformations, respectively.
5.2.3.2 Rectangular 2 (100x150x200)
The dimensions of the rectangular specimens in this group
were 100 mm in width, 150 mm in depth and 200 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.3c and 5.3d. The control
specimen failed at the average peak stress of 16.6 MPa. The maximum stress increase
of 162% was measured for the specimen R2-H-4 with 4 layers of NHFRP composite
and minimum increase in peak stress of 51% was measured for column R2-S-2 with 2
layers of NSFRP composite. The increases in peak stress were 75% and 111% for
column specimens R2-H-2 and R2-H-4, respectively. Similar to the load carrying
capacity, the axial deformations of the NFRP-strengthened columns were also
increased. As shown in Figure 5.3c and 5.3d, the increases in the axial deformations
of 167%, 300%, 100% and 233% were recorded for columns R2-S-2, R2-S-4, R2-H-2
and R2-H-4, respectively.
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5.2.3.3 Rectangular 3 (150x225x300)
The dimensions of the rectangular specimens in this group
were 150 mm in width, 225 mm in depth and 300 mm in height. The axial stress and
deformation curves of all specimens are shown in Figure 5.3e and 5.3f. The control
specimen failed at the average peak stress of 18.8 MPa. Among the strengthened
specimens, a maximum increase in the peak stress of 112% over the control specimen
was recorded for specimen R3-H-4, whereas a minimum increase of 33% was
measured for specimen R3-S-2 (see the Appendix B). The remaining column
specimens in this group (i.e., R3-H-2 and R3-S-4) reached peak stresses that were
39% and 89% greater than the control specimen, respectively. Similar to the load
carrying capacity, the axial deformations of the NFRP-strengthened concrete columns
were also increased. A maximum increase in the axial deformation was 230%, for
specimen R3-S-4. Column specimens R3-S-2, R3-H-2 and R3-H-4 reached the peak
stress at 70%, 45% and 193% enhanced axial deformations, respectively.
Fig.5.3 (a) Rectangular 1 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R1-S-4
R1-S-2
R1-CON
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Fig.5.3 (b) Rectangular 1 with NHFRP
Fig.5.3 (c) Rectangular 2 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R1-H-4
R1-H-2
R1-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R2-S-4
R2-S-2
R2-CON
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Fig.5.3 (d) Rectangular 2 with NHFRP
Fig.5.3 (e) Rectangular 3 with NSFRP
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R2-H-4
R2-H-2
R2-CON
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R3-S-4
R3-S-2
R3-CON
Ref. code: 25595722040218TUO
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Fig.5.3 (f) Rectangular 3 with NHFRP
Fig.5.3 Axial stress – axial deformation curves of rectangular columns
5.3 Effect of Fiber thickness
Figure 5.1-5.3 shows the axial stress-axial deformation curves of concrete
columns with different fiber thicknesses and the comparison of normalized ultimate
stress is displayed in Figure 5.4. It can be seen that the ultimate load carrying capacity
of circular, square and rectangular column specimens were elevated with an increase
in NFRP thickness. Both types of NFRP (i.e. NSFRP and NHFRP) led to the increase
in ultimate load carrying capacity with an increase in thickness. Increase in ultimate
load carrying capacity is more highly noticeable in smaller size specimens (i.e.
Circular 1, Square 1 and Rectangular 1) than in larger specimens as shown in Figure
5.4.
0
20
40
60
80
100
120
140
160
0 2 4 6 8 10 12 14 16
Ax
ial
stre
ss (
MP
a)
Axial deformation (mm)
R3-H-4
R3-H-2
R3-CON
Ref. code: 25595722040218TUO
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Fig.5.4 (a)
Fig.5.4 (b)
Fig.5.4 (c)
0
100
200
300
400
500
600
700
800
900
1000
Circular 1
Nor
mal
ized
Str
ess
(MP
a)
C1-CON
C1-S-2
C1-S-4
C1-H-2
C1-H-4
0
100
200
300
400
500
600
700
800
900
1000
Circular 2
Nor
mal
ized
Str
ess
(MP
a)
C2-CON
C2-S-2
C2-S-4
C2-H-2
C2-H-4
0
100
200
300
400
500
600
700
800
900
1000
Circular 3
Nor
mal
ized
Str
ess
(MP
a)
C3-CON
C3-S-2
C3-S-4
C3-H-2
C3-H-4
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Fig.5.4 (d)
Fig.5.4 (e)
Fig.5.4 (f)
0
100
200
300
400
500
600
700
800
900
1000
Square 1
Nor
mal
ized
Str
ess
(MP
a)
S1-CON
S1-S-2
S1-S-4
S1-H-2
S1-H-4
0
100
200
300
400
500
600
700
800
900
1000
Square 2
Nor
mal
ized
Str
ess
(MP
a)
S2-CON
S2-S-2
S2-S-4
S2-H-2
S2-H-4
0
100
200
300
400
500
600
700
800
900
1000
Square 3
Nor
mal
ized
Str
ess
(MP
a)
S3-CON
S3-S-2
S3-S-4
S3-H-2
S3-H-4
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Fig.5.4 (g)
Fig.5.4 (h)
Fig.5.4 (i)
Fig.5.4 Comparison of normalized stress (Effect of fiber thickness)
0
100
200
300
400
500
600
700
800
900
1000
Rectangular 1
Nor
mal
ized
Str
ess
(MP
a)
R1-CON
R1-S-2
R1-S-4
R1-H-2
R1-H-4
0
100
200
300
400
500
600
700
800
900
1000
Rectangular 2
Nor
mal
ized
Str
ess
(MP
a)
R2-CON
R2-S-2
R2-S-4
R2-H-2
R2-H-4
0
100
200
300
400
500
600
700
800
900
1000
Rectangular 3
Nor
mal
ized
Str
ess
(MP
a)
R3-CON
R3-S-2
R3-S-4
R3-H-2
R3-H-4
Ref. code: 25595722040218TUO
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5.4 Effect of Fiber material
In this experimental study, two types of natural fiber composites, namely
natural sisal fiber reinforced polymer (NSFRP) composites and natural hemp fiber
reinforced polymer (NHFRP) composites were studied. To compare the effectiveness
of different strengthening composites, a comparison of comparison of normalized
ultimate stress is displayed in Figure 5.5.As can be seen, the composite NHFRP
demonstrates a consistently superior performance over NSFRP composite for circular,
square and rectangular columns specimens. This is supposedly due to the higher
tensile strength and stiffness of NHFRP compared with NSFRP. This experimental
data indicates that the NHFRP strengthening is more efficient than NSFRP.
5.5 Effect of Section shape
In this study, three different types of cross section shapes (i.e. circular, square
and rectangular) were constructed and strengthened using NFRP composites to
investigate the efficiency of NFRP confinement on the ultimate strength. The
comparison of normalized ultimate stress is displayed in Figure 5.6. It can be seen that
efficiency of NFRP confinement is very sensitive to the column cross section
geometry i.e. circular, square and rectangular for all sizes, it is evident that change in
section shape (from circular to rectangular), regardless of the specimens size, led to
the reduction in load carrying capacity of NFRP strengthened specimens. These
findings are compliant with the results reported in the literature for artificial CFRP
composites [17].
5.6 Effect of Size
In this study, three different sizes for each cross section shape were considered
to investigate the effect of size of NFRP-confined concrete columns. A comparison of
normalized ultimate stress is displayed in Figure 5.7. Similar to the sectional shape,
the efficiency of NFRP confinement is observed to be very sensitive to the column
size. As can be seen, as the column size increases, regardless of the section shape, the
ultimate stress for both NSFRP and NHFRP strengthened specimens was reduced.
Ref. code: 25595722040218TUO
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These findings are complying with the results reported in the literature for artificial
FRP composites [18].
Fig.5.5 (a)
Fig.5.5 (b)
Fig.5.5 (c)
0
200
400
600
800
1000
Circular 1
Nor
mal
ized
Str
ess
(MP
a)
C1-CON
C1-S-2
C1-H-2
C1-S-4
C1-H-4
0
200
400
600
800
1000
Circular 2
Nor
mal
ized
Str
ess
(MP
a)
C2-CON
C2-S-2
C2-H-2
C2-S-4
C2-H-4
0
200
400
600
800
1000
Circular 3
Nor
mal
ized
Str
ess
(MP
a)
C3-CON
C3-S-2
C3-H-2
C3-S-4
C3-H-4
Ref. code: 25595722040218TUO
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Fig.5.5 (d)
Fig.5.5 (e)
Fig.5.5 (f)
0
200
400
600
800
1000
Square 1
Nor
mal
ized
Str
ess
(MP
a)
S1-CON
S1-S-2
S1-H-2
S1-S-4
S1-H-4
0
200
400
600
800
1000
Square 2
Nor
mal
ized
Str
ess
(MP
a)
S2-CON
S2-S-2
S2-H-2
S2-S-4
S2-H-4
0
200
400
600
800
1000
Square 3
Nor
mal
ized
Str
ess
(MP
a)
S3-CON
S3-S-2
S3-H-2
S3-S-4
S3-H-4
Ref. code: 25595722040218TUO
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Fig.5.5 (g)
Fig.5.5 (h)
Fig.5.5 (i)
Fig.5.5 Comparison of normalized stress (Effect of fiber material)
0
200
400
600
800
1000
Rectangular 1
Nor
mal
ized
Str
ess
(MP
a)
R1-CON
R1-S-2
R1-H-2
R1-S-4
R1-H-4
0
200
400
600
800
1000
Rectangular 2
Nor
mal
ized
Str
ess
(MP
a)
R2-CON
R2-S-2
R2-H-2
R2-S-4
R2-H-4
0
200
400
600
800
1000
Rectangular 3
Nor
mal
ized
Str
ess
(MP
a)
R3-CON
R3-S-2
R3-H-2
R3-S-4
R3-H-4
Ref. code: 25595722040218TUO
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Fig.5.6 (a) Size 1
Fig.5.6 (b) Size 2
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Circular Square Rectangular
Control specimen
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Circular Square Rectangular
Control specimen
Ref. code: 25595722040218TUO
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Fig.5.6 (c) Size 3
Fig.5.6 Comparison of normalized stress (Effect of section shape)
Fig.5.7 (a) Circular specimens
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Circular Square Rectangular
Control specimen
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Circular 1 Circular 2 Circular 3
Control specimen
Ref. code: 25595722040218TUO
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Fig.5.7 (b) Square specimens
Fig.5.7 (c) Rectangular specimens
Fig.5.7 Comparison of normalized stress (Effect of size)
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Square 1 Square 2 Square 3
Control specimen
0
100
200
300
400
500
600
700
800
900
1000
1100
1200
S-2L S-4L H-2L H-4L
No
rmal
ized
str
ess
(MP
a)
Fiber material type - Fiber thickness (layers)
Rectangular 1 Rectangular 2 Rectangular 3
Control specimen
Ref. code: 25595722040218TUO
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References
Books and Book Articles
1. Standard Test Method for Tensile Properties of Polymer Matrix Composite
Materials. Designation: D 3039/D 3039M – 00.(1997). International Harmonization of
Composite Materials-Phase I : ASTM Institute for Standards Research.
2. Standard Method of Test for Slump of Hydraulic Cement Concrete. AASHTO
Designation: T 119M/T 119-07.ASTM Designation: C 143/C 143M-05a.
3. Standard Test Method for Compressive Strength of Cylindrical Concrete
Specimen. Agencies of the Department of Defense. Designation: C 39/C 39M – 03
Articles
4. Y. Xiao and H. Wu.(2000). Compressive behavior of concrete confined by
carbon fiber composite jackets. Journal of Materials in Civil Engineering, May 2000
(pp.139-146).
5. J.F. Berthet, E. Ferrier and P. Hamelin.(2004).Compressive behavior of
concrete externally confined by composite jackets. Part A: experimental study.
Construction and Building Materials 19, 2005 (pp. 223–232).
6. Azadeh Parvin and Wei Wang. Tests on concrete square columns confined by
composite wraps. The University of Toledo, Toledo, Ohio, U.S.A.
7. Dian Jie Zhang and all. (2010). Compressive behavior of FRP-confined square
concrete columns after creep. School of Civil Engineering, Beijing Jiaotong
University, Beijing.Engineering Structures 32, 2010 (pp. 1957-1963).
8. Mark J. Masia and all. (2003). Size effects in axially loaded square-section
concrete prisms strengthened using carbon fiber reinforced polymer wrapping.
Canada. Journal Civil Engineer 31, 2004 (pp. 1-13).
9. R. Benzaid and all. Experimental investigation of circular and square RC
columns strengthened with CFRP sheets. International Conference on Sustainable
Built Environment Infrastructures in Developing Countries ENSET Oran (Algeria),
October 2009 (pp. 12-1).
Ref. code: 25595722040218TUO
62
10. Yousef A. Al-Salloum. (2006). Influence of edge sharpness on the strength of
square concrete columns confined with FRP composite laminates. Department of
Civil Engineering, King Saud University, Saudi Arabia. Composites: Part B38, 2007
(pp. 640–650).
11. I.A.E.M. Shehata and all.(2001).Strength of short concrete columns confined
with CFRP sheets. Materials and Structures Vol. 35, January-February 2002 (pp. 50-
58).
12. Yuan-feng Wang and Han-liangWu. Size Effect of Concrete Short Columns
Confined with Aramid FRP Jackets. Journal of composite for construction @ ASCE,
July- August 2011 (pp. 535-544).
13. Zhijian Li and all. Properties of hemp fibre reinforced concrete composites
(January 2005). Composites: Part A 37, 2006 (pp. 497–505). School of Engineering
and Technology, Deakin University, Pigdons Road, Geelong, Vic. 3217, Australia.
14. F. P. TORGAL and S .JALALI. Natural fiber reinforced concrete. Woodhead
Publishing Limited, 2011 (pp. 154-167). University of Minho, Portugal.
15. I. Merta, E.K. Tschegg. (2012). Fracture energy of natural fiber reinforced
concrete. Construction and Building Materials 40, 2013 (pp. 991–997). Institute for
Building Construction and Technology, Building Construction and Maintenance,
Faculty of Civil Engineering, University of Technology Vienna, Karlsplatz.
16. M. Ramesh and all. (2012). Mechanical property evaluation of sisal–jute–glass
fiber reinforced polyester composites. Composites: Part B 48, 2013 (pp. 1–9).
17. Tara Sena and H.N. Jagannatha Reddyba.Flexural strengthening of RC beams
using natural sisal and artificial carbon and glass fabric reinforced composite system.
Sustainable Cities and Society 10, 2014 (pp. 195–206).
18. Rochette P and all. Axial testing of rectangular column models confined with
composites. J Compos Construct 2000;4(3 )(pp.129–36)
19. Fang-Yao Yeh and all. Size and shape effect on FRP confinements for
rectangular concrete columns. 13th World Conference on Earthquake Engineering
Vancouver, B.C., Canada, 1-6 August 2004 Paper No. 657
20. Riad Benzaid and all. Circular and Square Concrete Columns Externally
Confined by CFRP Composite: Experimental Investigation and Effective Strength
Models. Fiber Reinforced Polymers - The Technology Applied for Concrete Repair.
Ref. code: 25595722040218TUO
63
21. K.A. Harries and all. (1998). Axial Behavior of Reinforced Concrete Columns
Retrofit with FRPC Jackets. Proc., of 2nd int. Conf. on Compos .in Infrastructure,
(pp. 411-425). University of Ariz., Tucson, Ariz.
22. A.Mirmiran. and all. (1998). Effect of column parameters on FRP-confined
concrete, Journal of Composites for Construction ,November 1998 (pp. 175-185).
23. Silvia Rocca. (2007). Experimental and analytical evaluation of FRP confined
large size reinforced concrete columns. Dissertations Paper 1997. Faculty of the
Graduate School of the University of Missouri-Rolla Doctoral.
24. Thong M. Pham. (2014). Confinement model for FRP confined normal- and
high-strength concrete circular columns. University of Wollongong, Australia.
Faculty of Engineering and Information Sciences-Papers.
25. Ahmed Belaadi and all.(2012). Tensile static and fatigue behavior of sisal
fibers. Materials and Design 46. 2013 (pp. 76–83), from
http://www.sciencedirect.com/science/article/pii/S0261306912006796
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Appendix A
Failure modes
Failure modes of circular specimens
C-CON
C1-2S
Ref. code: 25595722040218TUO
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Appendix B
Summary of test results
Main Groups Subgroups
(size – mm) Specimen
Peak stress
(MPa)
% Increase in
peak stress
Ultimate
deformation (mm)
% Increase in
ultimate deformation
Circular
Circular 1
(50 x 100)
C1-CON 15.8 - 0.5 -
C1-S-2 88.0 456 5.2 940
C1-S-4 140.0 785 9.0 1700
C1-H-2 90.0 469 3.5 590
C1-H-4 150.0 848 6.0 1100
Circular 2
(100 x 200)
C2-CON 22.1 - 2.0 -
C2-S-2 50.0 126 8.0 300
C2-S-4 70.0 216 12.0 500
C2-H-2 58.0 162 6.0 200
C2-H-4 87.0 293 10.0 400
Circular 3
(150 x 300)
C3-CON 26.9 - 2.8 -
C3-S-2 50.0 86 7.0 155
Ref. code: 25595722040218TUO
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Circular Circular 3
(150 x 300)
C3-S-4 71.0 164 13.6 395
C3-H-2 52.3 94 0.0 100
C3-H-4 80.0 197 3.0 199
Square
Square 1
(50 x 50 x 100)
S1-CON 12.7 - 0.4 -
S1-S-2 66.0 421 3.9 875
S1-S-4 95.2 652 6.3 1475
S1-H-2 72.0 469 2.8 590
S1-H-4 120.0 848 4.8 1100
Square 2
(100 x 100 x 200)
S2-CON 17.7 - 1.6 -
S2-S-2 50.0 182 8.0 400
S2-S-4 56.0 216 9.6 500
S2-H-2 46.4 162 4.8 200
S2-H-4 69.6 293 8.0 400
Square 3
(150 x 150 x 300)
S3-CON 21.5 - 2.2 -
S3-S-2 40.0 86 5.6 155
S3-S-4 56.8 164 10.9 395
S3-H-2 41.8 94 4.8 118
S3-H-4 64.0 197 9.7 340
Ref. code: 25595722040218TUO
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Rectangular
Rectangular 1
(50 x 100 x 100)
R1-CON 11.9 - 0.3 -
R1-S-2 44.0 271 2.6 829
R1-S-4 70.0 490 4.5 1507
R1-H-2 45.0 279 1.7 516
R1-H-4 75.0 532 3.0 971
Rectangular 2
(100 x 150 x 200)
R2-CON 16.6 - 1.5 -
R2-S-2 25.0 51 4.0 167
R2-S-4 35.0 111 6.0 300
R2-H-2 29.0 75 3.0 100
R2-H-4 43.5 162 5.0 233
Rectangular 3
(150 x 225 x 300)
R3-CON 18.8 - 2.1 -
R3-S-2 25.0 33 3.5 70
R3-S-4 35.5 89 6.8 230
R3-H-2 26.1 39 3.0 45
R3-H-4 40.0 112 6.1 193