Strengthening slender reinforced concrete (RC) columns is a challenge because
their sensitivity to overall buckling and the combination of the bending and
compressive stresses. This paper presents experimental study for strengthening twenty
long RC columns using enhanced ferrocement jackets. The column specimens have
slenderness ratio of 17.6 and two different cross-sections (square and rectangular).
The utilized expanded metal mesh layers have different weights, lengths and numbers
for each jacket. The twenty strengthened specimens and four reference non-jacketed
specimens were tested under concentric compression loading. The results
demonstrated the effectiveness of the ferrocement jacket in improving the column
capacity, increasing the stiffness, and reducing the lateral deformation. The
significance of the jackets is more evident for long RC columns with larger crosssection area, and for jackets with larger volume fraction of metal mesh layers at the
middle-third of the column height.
2. Ahmed M. El-Kholy, Mohamed M. Masaoud and Magdy A. Abd El-Aziz
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1. INTRODUCTION
Reinforced concrete (RC) long columns are aesthetic and efficient structural members to
transfer the structure loads to the foundation. Many of the wonderful RC buildings, halls, and
special structures in the world would not be impressive enough without the slender columns.
The RC column is categorized as long if its slenderness ratio λ (the height divided by the
width for rectangular columns and by the diameter for circular columns) exceeds 15 and 12
for rectangular and circular columns, respectively, according to the Egyptian code for design
and construction of concrete structures [1]. The long columns are sensitive to overall
buckling at high compression loads and therefore their capacity is governed by not only the
compressive stress but also the bending stress unlike the short columns. This characteristic of
the long columns has significant impact on the typical jacketing procedure that increases the
column confinement in the transverse direction to improve the concrete core effectiveness in
order to sustain higher compressive stress. The typical composites confinement jacket for RC
columns was investigated through numerous researches unlike the limited researches for
studying the strengthening of slender columns. Nevertheless, the researches for strengthening
long RC columns emphasized important observations such as the strengthening effectiveness
is reduced with the increase of slenderness ratio, strengthening effectiveness is reduced with
the increase of eccentricity of loading (if any), and the confinement jacket is not useful
enough for slender columns. These observations were highlighted by Tarkhan [2], Youcef et
al. [3], Gaidosova and Bilcik [4], and Pan et al. [5]. The composites confinement jacket types
of RC columns are ferrocement jacket [6-8] and Carbon Fiber-Reinforced Polymer CFRP
jacket [8-10]. The most important merit of CFRP jacket is that it does not increase the cross
section area of the column. Nevertheless, it is not popular in the developing countries because
of its high cost. The construction procedure and the cost of ferrocement jacket are appropriate
enough to the construction environment in the developing countries. The metal meshes, either
expanded metal mesh (EMM) or welded wire mesh (WWM) that are used with the cement
mortar to form the ferrocement, is available in the markets of these countries. These metal
meshes could be used not only as external confinement but also used as internal confinement
reinforcement (instead of or combined with ties) as proposed by Razvi and Saatccioglu [11]
and El-Kholy et al. [12].
The significant researches for strengthening slender RC columns (λ>15) are summarized in
the following lines. Tarkhan [2] strengthened six rectangular column specimens (λ=15.8)
with ferrocement jackets comprising EMM with huge steel area (4.7 Kg/m2
) and installed
with different mesh orientations. The reference column specimen and the strengthened six
specimens were tested under axial compression loading and recorded high increment in the
ultimate load of the strengthened columns especially for those comprising EMM oriented in
the vertical direction. Malhorta [13] strengthened six square columns specimens (λ=3, 7
and15) with ferrocement jackets comprising one or two WWM layers. Three reference
specimens and the six strengthened specimens were tested under axial compression loading.
Significant improvements in the ultimate load were recorded for the jacketed specimens. Pan
et al. [5] confined six elliptical modified rectangular column specimens (λ ranges from 4.5 to
17.5) with FRP wraps. The specimens were tested under concentric compression loading to
distinguish between the behavior of the short and slender columns. It was concluded that the
strengthening effectiveness is decreased with the increase of the slenderness ratio. Challenge
full scale testing of eight rectangular column specimens with λ=27 was conducted by
Gajdosova and Bilcik [4]. The axially loaded specimens comprised two references and six
specimens strengthened with CFRP. The results demonstrated that mounting the CFRP strips
longitudinally is effective for strengthening slender RC columns unlike confinement in the
transverse direction. Another challenge of testing six square column specimens (three
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references and three confined with CFRP) with λ=16, 19 and 27 was conducted by Youcef et
al. [3]. The specimens were tested under eccentric compression loading.
This paper presents enhanced ferrocement jackets for square and rectangular RC long
columns with slenderness ratio of 17.6. The jackets comprise EMM layers with different
weights, lengths, and numbers to investigate the optimum ferrocement jacket for slender
square and rectangular RC columns.
2. EXPERIMENTAL PLAN
Twenty-four RC long column specimens with height of 2200 mm and slenderness ratio λ of
17.6 were tested under concentric compression loading. The specimens were divided into two
groups according to the cross-section shape. Group1 represents the square cross-section with
dimensions 125×125 mm, whereas group2 specimens have rectangular cross-section with
dimensions 125×190 mm. Every group comprises two (one pair) reference non-jacketed
column specimens and ten (five pairs) jacketed column specimens. The experiment plan and
the configurations of the column specimens are given in Table 1. Except the EMM testing, all
materials and specimens testing was conducted in the concrete research and material
properties laboratory at Fayoum University. EMM testing was conducted in the material
properties laboratory of the American University at Cairo.
Table 1 The experimental plan and details of the RC specimens and ferrocement jackets
Group
Specimen
ID
Crosssection
(mm)
Slendernessratio
Reinforcement Ferrocement jacket (EMM layers and remarks)
vertical
ties
thickness
N°oflayers
volume
fraction%
N°
volumetric
ratio%
1
i
SE
125×125
17.6
4Ø10
5Ø8/m
0.61
---- ---- ---- non-jacketed (reference)
i
SF1N Thin 1 0.30 -----
i
SF11/3 N Thin 1+1/3 0.60 (0.40) 1/3 layer at column center
i
SF1N-D Thin 1 0.30 spiral
i
SF1K Thick 1 0.64 ----
i
SF1/3K Thick 1/3 0.64 (0.21) 1/3 layer at column center
2
i
RE
190×125
17.6
6Ø10
5Ø8/m
0.61
---- ---- ---- non-jacketed (reference)
i
RF1N Thin 1 0.30 -----
i
RF2N Thin 2 0.60 -----
i
RF11/3 N Thin 1+1/3 0.60 (0.40) 1/3 layer at column center
i
RF1K Thick 1 0.64 ----
i
RF1/3 K Thick 1/3 0.64 (0.21) 1/3 layer at column center
i =specimen repetition= 1, 2
x Ø y indicates x bars (or ties) of diameter y mm
/m indicates per longitudinal meter
values in parentheses represent the average value on the total height
3. MATERIAL PROPERTIES
Portland cement type1 (CEM1) of grade 42.5N conforming Egyptian Standards (ES) 4756-
1/2013 [14] was used. Local basalt was used as coarse aggregate. The basalt was well graded
with maximum size of 14 mm, specific gravity of 2.6, crushing strength of 20%, absorption
percentage of 2%, Chlorides content of 0.018%, and Sulphates content of 0.21%. The used
4. Ahmed M. El-Kholy, Mohamed M. Masaoud and Magdy A. Abd El-Aziz
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fine aggregate was natural siliceous sand with fineness modulus of 2.12, specific gravity of
2.5, bulk density of 1650 Kg/m3, percentage of clay and other fine materials of 1.1%,
absorption percentage of 1.9%, Chlorides content of 0.04%, and Sulphates content of 0.31%.
Physical and chemical results of both coarse and fine aggregates conform ES 1109/2008 [15].
High grade (360/520 MPa) tensile steel and mild steel (grade 280/450 MPa) were used for
longitudinal and transverse reinforcements, respectively. Tests conducted on the
reinforcement steels show that they conform ES 262-1/2015 [16] and ES 262-2/2015 [17] for
grades 280/450 and 360/520, respectively. For the utilized thin EMM, the dimensions of the
diamond opening and the strand cross-section were 30×20 and 1.2×0.6 mm, respectively,
whereas the corresponding dimensions of the used thick EMM were 32×16 and 1.5×0.9 mm,
respectively. The thin and thick EMM types weighted 0.48 Kg and 1.00 Kg per square meter,
respectively. The average specific gravity was 6.7 for the two types. Two strands were
excluded from the thick EMM, and were tested under uniaxial tension. The results were
shown in Figure 1. The average yield and ultimate stresses were 148 and 276 MPa. The
concrete compressive strength was 25 MPa after 28 days for standard 150 mm cubes. The
concrete-mix ratios were 350 kg/m3
cement, 175 kg/m3
tap water, 1222 kg/m3
basalt, and 611
Kg/m3
sand. Silica fume was used to produce high strength mortar for the ferrocement jacket.
The mortar compressive strength was 47 MPa after 28 days for standard 70 mm cubes. The
mortar mix weight-ratios were 2, 0.5 and 0.1 for sand, water and silica fume, respectively,
compared with the cement weight. The specifications of all used materials were consistent
with provisions of the Egyptian code for design and construction of concrete structures (ECP
203/2018) [1].
Figure 1 Elongation of the EMM strand
4. THE PROCESS OF PREPARING AND STRENGTHENING THE
SPECIMENS
The program comprises three phases to prepare, preload and strengthen the column
specimens.
4.1 Phase I "preparing the original column specimens"
4.1.1 Steel reinforcement
Table 1 shows that all the column specimens contain vertical reinforcement (grade 360/520)
of four corner bars with 10 mm diameter. The rectangular columns have additional two
middle bars. Also, all the specimens have typical transverse reinforcement (grade 280/450) of
five square ties (8 mm diameter) per longitudinal meter. The volumetric ratio of the lateral
reinforcement is equal to 0.61% compared with the concrete volume. The ends of the vertical
bars were bent horizontally and two confining ties of 8 mm diameter were added at the end of
each column specimen to secure the specimen ends similar to the configurations adopted by
El-kholy and Dahish [18].
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4.1.2 Wooden forms
Figure 2-a shows the wooden forms that were prepared to cast the specimens. The inner
surfaces of the forms were overlaid by a release agent and then the steel reinforcement cages
were aligned in the forms (Figure 2-b) with clear cover of 15 mm.
4.1.3 Concrete pouring
The components of the concrete (with the ratios given in section 3) were mixed using
electrical mixer. The fresh concrete was poured into the specimens forms (Figure 2-c).
Electrical vibrator was used to consolidate the concrete. The sides of the forms were removed
after 24 hours and the specimens were cured for 28 days using the wet burlap (Figures 2-d, 2-
e and 2-f).
4.2 Phase II "preloading the column specimens"
The twenty-four column specimens were preloaded with concentric compression load equal
to 60% of the ultimate load of the reference specimen in each group. Figure 2-g illustrates the
preloading phase. The reason of the preloading phase is to simulate the practical field. It is
worth mentioning that the twelve specimens of each group are identical in terms of the
dimensions, reinforcement and preloading up to this second phase.
4.3 Phase III "jacketing the column specimens"
4.3.1 Roughening the specimen surfaces and installing EMM layers
Electrical angle grinder with carbon disc was used to partially abrase the side surfaces for ten
specimens of each group to increase their roughness to be ready for jacketing the specimens
with interlocking between the original concrete and the ferrocement jacket. The remaining
two specimens in each group (which are in their original form without grinding) will be
labeled as reference specimens. The EMM layers of the ferrocement jackets were prepared
according to the type, number and length specified in Table 1 for each pair of the five
strengthened specimens pairs in each group. The EMM layer was wrapped around the
roughened surfaces of the columns with adequate overlapping. Electric drill was used to
install fasteners acting as shear connectors between the original concrete and the ferrocement
jacket. Figure 2-h illustrates the EMM layers wrapped and connected around the roughened
surface of the concrete specimens.
4.3.2 Adding the high strength cement mortar
High strength cement mortar was prepared according to the ratios given in section 3.
Powerful adhesive (addibond 65 [19]) was used to produce adhesive slurry for bonding the
fresh mortar to the original concrete. The mortar was added to the roughened specimen using
trowel and adequate pressure to densfiy the mortar in the jacket as shown in Figure 2-i. The
finish of the jacket surface was done using the trowel, lath and the spirit level to ensure the
straightness and the horizontality of the surfaces as shown in Figure 2-j. The final cross-
section of the RC specimens increased 20 mm from the four sides (Figure 2-j). After 24
hours, the twenty strengthened column specimens were cured using wet burlap (as shown in
Figure 2-k) for 28 days.
6. Ahmed M. El-Kholy, Mohamed M. Masaoud and Magdy A. Abd El-Aziz
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Figure 2 The process of preparing, preloading and strengthening the specimens
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5. CONCENTRIC COMPRESSION LOADING (INSTRUMENTATION AND
TEST SETUP)
All the twenty-four specimens were loaded with axial compression (till failure) using 100 kN
capacity loading frame as shown in Figure 3. Two rigid steel plates and clamps were used at
the ends to distribute the load and confine the stressed loading ends of the column specimen.
Three displacement transducers were used to monitor the axial and the lateral deflection in
two perpendicular directions at the column mid-height as illustrated in Figure 3. Two strain
gages were used to monitor the lateral strain on the concrete surface at the mid-height.
Figure 3 Test setup
6. RESULTS
Table 2 shows the average results for the six pairs of each group. The ultimate load, axial
displacement, lateral displacement and energy absorption are listed in Table 2 for every pair.
Also, their increment percentages compared with the reference pair are given in the table.
Figure 4 illustrates the load-axial displacement histories for the two tested groups. Figure 5
shows the percent increment in the ultimate load for jacket specimens compared with the
non-jacketed specimens. Figure 6 illustrates the failure modes and the cracks for the tested
specimens. Figures 7 and 8 show the percentage increment in axial displacement and
percentage decrement in lateral displacement, respectively, for jacketed specimens compared
with non-jacketed specimens. Similarly, Figure 9 shows the strain absorption results.
6.1 Ultimate load
Figure 5 demonstrates that all jacketed specimens sustained higher load capacity (compared
with the reference specimens) except SF1N-D due to the existence of large number of EMM
overlaps in the spiral wrapping that interrupts the jacket continuity. Also, the result of SF1N-
D confirms the low effectiveness of the confinement jacket for slender columns. It could be
argued that the higher cross-section area and the higher minor second moment of inertia of
the rectangular columns (about 1.4 times those of the square specimens) increased the
ultimate load improvement of the rectangular column specimens compared with the square
specimens as evident from the comparison between Figures 5-b and 5-a.
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Table 2 The results of strengthened column specimens compared with reference specimens
±% indicates percentage of increment (+) or decrement (-) in value with respect to non-jacketed specimen
It is noticeable that the strength improvement is minor for square jacketed columns with
thin EMM as shown in Figure 5-a. The two reasons behind this observation are the small
cross-section of the square column specimens and the low volume fraction of the thin EMM.
For the square specimens jacketed with thick EMM and for all the rectangular column
specimens strengthened with either thin or thick EMM, the improvement in the ultimate load
was significant. The average improvements in the strength were 29%, 23% and 44% for the
square specimens jacketed with thick EMM, rectangular specimens jacketed with thin EMM,
and rectangular specimens jacketed with thick EMM, respectively. The capacity
improvement for the thick EMM jacket is approximately twice that for thin EMM. It is worth
mentioning that the volume fraction of thick EMM is also approximately twice that of the
thin layer as Table 1 shows. The improvement percentages for thick layer and one-third thick
layer jackets are close in each studied group. Therefore, one-third thick layer installed at the
middle-third of the column specimen is more reliable (than complete layer) in terms of the
cost and construction time. A glance to Figure 5-b shows that the two thin EMM layer jacket
was slightly more efficient than the one thick EMM layer jacket although the volume fraction
of two thin EMM layers is smaller than that of one thick layer. The reason behind this
observation might be that the number of layers (not only the volume fraction) is an important
parameter to improve the jacket efficiency. However, the ease of construction for the one-
third thick EMM jacket still overrides the small additional gain of using two thin EMM
layers.
6.2 Failure and cracks
The square jacketed column specimens with thin EMM layers and the reference non-jacketed
specimens exhibited clear buckling at the mid-height of the column (level 1) as shown in
Figure 6. It is worth to remind that the improvement in the strength of these jacketed
specimens as concluded and interpreted in section 6.1. The increase of the volume fraction
reduces the deformation, and the failure still occurs in the middle-third of the column (level
2) but might be not in the exact mid-height. Also, using one-third EMM layer jacket reduces
the deformation but moves the failure section out of the middle-third of the specimen. The
failure occurs in the weak two-thirds height where only one EMM layer is installed.
Group
Specimen
ID
Ultimate load Axial displacement Lateral displacement Energy absorption
kN ±% mm ±% mm ±% kN.mm ±%
1
i
SE 441.13 ---- 11.75 ---- 10.50 ---- 2591 ----
i
SF1N 467.47 5.97 11.50 -2.13 9.50 -9.52 2687 3.71
i
SF11/3 N 450.03 2.02 11.25 -4.26 12.00 14.29 2531 -2.32
i
SF1N-D 439.56 -0.36 11.50 -2.13 9.50 -9.52 2527 -2.47
i
SF1K 573.38 29.98 12.00 2.13 8.50 -19.05 3440 32.77
i
SF1/3K 568.15 28.79 11.75 0.00 8.00 -23.80 3337 28.79
2
i
RE 514.81 ---- 12.00 ---- 11.00 ---- 3088 ----
i
RF1N 637.28 23.79 12.25 2.08 6.00 -45.45 3903 26.39
i
RF2N 787.66 53.00 12.25 2.08 1.00 -90.90 4824 56.22
i
RF11/3 N 627.7 21.93 12.50 4.17 3.00 -72.70 3923 27.04
i
RF1K 751.45 45.97 12.75 6.25 1.00 -90.90 4790 55.12
i
RF1/3 K 726.29 41.08 11.75 -2.08 2.75 -75.00 4266 38.15
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6.3 Deformation, stiffness and ductility
Figure 7 shows that the rectangular specimens exhibited insignificant increment in the axial
displacement whereas the square specimens and those with one-third height thick EMM did
not show any gain in the axial displacement.
Figure 4 Load–vertical displacement histories
Figure 5 Percent increment in ultimate load with respect to non-jacketed specimen
Figure 6 The failure modes and crack patterns of tested specimens
Figure 8-a shows that the reduction in lateral deformation was minor for the square
specimens jacketed with thin EMM layer. For square specimens jacketed with thick EMM
(either whole or one-third layer), the reduction was significant (about 20%). On the other
hand, Figure 8-b shows that the reduction in lateral deformation was evident and effective for
all jacketed rectangular column specimens because of their original higher stiffness
(compared with square column specimens). Also, it is noticeable that the reduction in lateral
10. Ahmed M. El-Kholy, Mohamed M. Masaoud and Magdy A. Abd El-Aziz
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displacement for the rectangular specimens jacketed with thick EMM layer (or two thin
layers) was approximately double that of the specimens jacketed with one thin EMM layer.
Based on the preceding discussions of the displacement results, the improvement in
ductility is insignificant for all specimens because there is no noticeable increase in the axial
displacement. However, the improvement in the stiffness of the columns is noticeable in
Figure 4. The more ultimate load is sustained, the more improvement in the stiffness is. The
stiffness improvement was higher for the specimens (square or rectangular) jacketed with two
thin EMM layers or one thick EMM layer, and moderate for the rectangular specimens
jacketed with thin EMM layer.
Figure 7 Percent increment in axial displacement with respect to non-jacketed specimen
Figure 8 Percent decrement in lateral displacement with respect to non-jacketed specimen
Figure 9 Percent increment in energy absorption with respect to non-jacketed specimen
6.4 Energy absorption
Figure 9 shows the increment in the absorbed energy for the jacketed column specimens
compared with reference specimens. The absorbed energy was calculated by estimating the
area under the load-displacement curve. The area was approximated to triangle shape. Figure
4, Figure 7 and Table 2 show that all jacketed column specimens fail at close displacements
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but different ultimate loads. Therefore, the ultimate load increment will govern that of the
energy absorption. There was no increment in the energy absorption for the square column
specimens jacketed with thin EMM layer. The increment became significant (average 29%)
for square and rectangular column specimens jacketed with thick and thin EMM layer. The
improvement in energy absorption was approximately doubled (average 50%) for rectangular
specimens jacketed with two thin or one thick EMM layer.
7. CONCLUSIONS
Twenty RC long columns strengthened with ferrocement jackets and four non-jacketed
reference specimens were tested under axial compression. All the twenty-four specimens are
slender columns with 2200 mm height and slenderness ratio of 17.6. The ferrocement jackets
comprise high strength cement mortar and EMM layers with different weights. The weight of
the used thick mesh is approximately double that of the other used thin EMM. The EMM
layers were used with the complete height of the columns or with only one-third height of the
column specimens or wrapped spirally on the whole column specimen. The following
conclusions are summarized.
1) The square column specimens sustained smaller ultimate load and exhibited more lateral
deformation compared with the rectangular specimens (with the same width) because of their
relative smaller cross-section area and moment of inertia.
2) The jackets of the square column specimens should comprise thick EMM with larger
weight compared with rectangular column (with the same width) in order to obtain significant
increment in the ultimate load and reduction of the lateral deformation.
3) The larger cross-section area of the column (and larger aspect ratio for the same width)
increases the strengthening effectiveness (capacity and stiffness).
4) Spiral EMM ferrocement jacket is not effective for slender columns because it is explicit
confinement jacket with no continuity (of EMM strands) in the vertical direction.
5) Increasing the surface weight of the EMM (volume fraction of EMM compared with the
mortar volume) and also the number of layers increases the strengthening effectiveness (load
capacity and stiffness).
6) The improvement in load capacity is proportional to the volume fraction of the used EMM
layers.
7) The use of one-third height thick EMM layer at the center of the ferrocement jacket is
considered as enhanced reliable jacket because of the low average volume fraction of the one-
third height EMM (economic cost), ease of construction, and close effectiveness (capacity
and stiffness) to the jackets with a complete height thick layer or two thin layers.
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