Microsoft Word - numero_56_art_10_3004 K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 123 Experimental and analytical investigations of reinforced concrete beams strengthened by different CFRP sheet schemes Khaled Fawzy, Hilal Hassan, M. Madqour University of Zagazig, Egypt khaled_lashen1@yahoo.com, https://orcid.org/0000-0003-2275-4025 hilalcivil@yahoo.com Madqour42@gmail.com, https://orcid.org/0000-0002-0994-2884 ABSTRACT. The use of reinforced fibre polymers to strengthen and repair structural elements is widely spreading. However, there is lack of knowledge of the actual behavior of strengthened structures with FRP sheets. This paper discusses the experimental results of the flexural strengthening of reinforced concrete (RC) beams by carbon fibre- reinforced polymer (CFRP) sheets bonded by epoxy adhesive to the tensile surface of the beams. Using a four-point bending load system over an effective span of 1800 mm, a total of ten beams with an overall dimension of 150 mm * 200 mm * 2000 mm with different degrees of strengthening schemes were tested. The number of layers, strengthening scheme (side and U-shape bonding) and reinforcement ratio are the major parameters of the experimental study. The research indicates that the flexural strength of the beams was substantially improved as the layers of laminate increased (between 31.80 and 71.50 %) and using U shape in ends that delay or prevent debonding failure. The experimental results compared to that analytically obtained by using ANSYS model showing acceptable agreement with deviations varying no more than 10 % for all specimens. KEYWORDS. Strengthening; Carbon fibre reinforced polymer; Deflection; ANSYS; Ultimate strength; Ductility. Citation: Fawzi., F., Hassan, H., Madqour., M. Experimental and analytical investigations of reinforced concrete beams strengthened by different CFRP sheet schemes, Frattura ed Integrità Strutturale, 56 (2021) 123-136. Received: 31.01.2021 Accepted: 08.03.2021 Published: 01.04.2021 Copyright: © 2021 This is an open access article under the terms of the CC-BY 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited. INTRODUCTION he external bonding of high-strength CFRP to structural concrete components has gained widespread significance in recent years, particularly in rehabilitation works. due to the various benefits of the use of CFRP as reinforcement, such as corrosion resistance, lightweight, and high strength. The need for bridges, buildings, and other structural elements to be rehabilitated or strengthened may occur due to one or a combination of several reasons including but not limited to construction or design deficiencies, increased load carrying demands, damage to the structural components, and seismic rehabilitation. CFRP was commonly used for strengthening reinforced concrete, masonry, and steel structures. Several studies have shown the suitability of CFRP material for structures made up of different materials, stiffness, and T https://youtu.be/6maz7ecY9Nc K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 124 ductility [1-4]. By following the proper technique of retrofitting, CFRP greatly improves the shear and flexure strength of concrete structures compared to the standard concrete structure. The epoxy resin which is the adhesive that allows the bond between the concrete surface and CFRP a key parameter for the control for the ultimate strength because it often fails first. Flexure, shear, and compression cracks can be minimized with the help of CFRP technology in RC beams. The use of CFRP compared to other fibre-reinforced polymer (FRP) materials for retrofitting results from its low density, its resistance to elevated tensile forces, fatigue, and corrosion. Hasnat el al [5] performed research on simply supported RC beams reinforced by CFRP wrap. A CFRP wrap withstood the premature debonding of the cover and acted as a U-clip resulting in an improvement in the capacity of the ultimate moment. Mostafa and Razaqpur [6] carried out an experiment on T-section reinforced concrete beams. The load was applied and the deflection was calculated for each beam. The full post-peak load/softening response of each beam also was obtained. Fu et al. research on the effectiveness of the U-jacket system in preventing or delaying debonding failure has been published. Nine large- range RC beams were studied in their experimental analysis to study and examine the effects of different FRP U-jacket modes on debonding failure. Abid and Al-lami [7] also performed a detailed analysis of previous studies that highlight the strength and durability of concrete beams that have been externally bonded to FRP reinforcement. The study focused on bond behavior, testing approaches, and models used to determine bond strength. Flexure, shear, and fatigue behaviors of multiple reinforcement techniques have been reviewed and discussed in detail. Benaoum el al [2] In this study, 3D-FEM is analyzed in reinforced concrete beams on the basis of a load-deflection reaction analysis. The value of loading magnitude, crack initiation and geometric parameters has been shown. A cracked concrete beam supported by externally bonding CFRP and a concrete beam strengthened by steel bars. However, the debonding process of collapse, structural ductility, and long-term durability are the major challenges facing CFRP due to weak bonding and decreased vapor pressure [8-12]. flexural strength, failure behavior, and structural ductility are the most important parameters to be considered in structural design, especially when the structure is in high earthquake zone. CFRP is a substance that is brittle and collapses suddenly, and has a linear elastic effect up to failure, i.e., its failure strain in tension varies from 2% to 4% [6]. Once the strain of failure has been achieved, CFRP gives no warning signs, it separates suddenly and causes loss of strength. These retrofitted reinforced concrete systems are not ideal because they do not have any sort of early warning before the collapse, resulting in the system collapsing. However, these systems would sustain large loads due to the high strength of the CFRP besides in large deformation/ deflection of the structural member.In this paper the effect of using various layers of CFRP sheets with different U-shape and side bonding schemes is experimentally studied. In addition, a finite element numerical model is performed and the obtained results are compared to the experimental behavior of RC beams in terms of ultimate load, crack patterns, and failure modes. EXPERIMENTAL PROGRAM AND SETUP Test specimens en reinforced concrete beams under a monotonical four-point loading scheme were tested in this research work. All the ten beam specimens have the same cross-section 200 mm height and 150 mm width, and a length of 2000 mm (Fig.1). The beams were simply supported with 1800 mm of clear span. The lower longitudinal reinforcement for beams B00 to B07 was two 10 mm bars. Two 12 mm bars were used for B09, and 16 mm for B08. The upper longitudinal reinforcement of all specimens consisted of two 8 mm bars. The stirrups were 6 mm diameter placed at intervals of 125 mm. The thickness of CFRP laminates was 0.129 mm, while their ultimate strain and elasticity module was 1.55% and 230 GPa, respectively. Figure. 1. Details of the tested beams (in mm). T K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 125 Material properties CFRP: The fibre used in the experimental work is longitudinal, unidirectional wrap of Carbon Fibre (Fig. 2). Tab. 3 displays the main features of the manufactured CFRP strengthening material used for the tests. Epoxy adhesive: The epoxy adhesive consists of two-part; resin (component A) and hardener (component B). Tab. 3 shows a summary of the mechanical and physical characteristics of CFRP impregnation resin used. Concrete and steel: To achieve concrete mix constituents with a strength of 32 N/mm2, the concrete mixture was designed using the ACI method. For each casting process, three standard concrete cubes (150 mm x 150 mm x 150 mm) and three standard concrete cylinders (150 mm x 300 mm) were cast and cured in water for 28 days. The average of compressive strength after 28 days was 32 MPa (Tab. 1). Standard tension tests were performed on steel specimens according to ASTM using MTS 200 tons universal testing machine. Three steel specimens were tested for each bar diameter and the average value was considered. the average steel yield stress was 525 MPa for the longitudinal reinforcement and 400 MPa for the stirrups (Tab. 2). Properties Values found in the laboratory Compressive strength (MPa) 32 Modulus of elasticity (GPa) 30.6 Modulus of rupture (MPa) 3.4 Table 1: Concrete properties. Reinforcement type Yield strength (MPa) Modulus of elasticity (GPa) Tension (10 mm) 525 200 Compression (8mm) 525 200 Shear (6 mm) 400 195 Table 2: Steel properties. Materials Properties Values (GPa) CFRP laminates Modulus of elasticity (GPa) 230 Elongation at ultimate (%) 1.70 Design thickness (mm/ply) 0.129 Tensile strength (MPa) 4000 Density (g/cm3) 1.82 Epoxy (the mix) Modulus of elasticity (GPa) 4.50 Elongation at ultimate (%) Tensile strength (MPa) 0.90 30 Table 3: CFRP laminates and epoxy adhesive properties. Figure 2: CFRP sheet used in this study. K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 126 Strengthening and instrumentation Concrete was poured into the moulds in three layers by using the vibrator to eliminate the appearance of voids. To achieve a smooth surface, the extra concrete was removed. At ambient temperature for 24 hours, the beams, cubes, and cylinders were coated with plastic sheets, then separated from the moulds and numbered. The curing process for the beams was carried out by using a wet sackcloth for 28 days, while the concrete cubes and cylinders were submerged in clean water. the surface of the concrete beams was cleaned to remove the weak strip of dry cement paste and then the dust was removed by air nozzle to achieve perfect bonding. The bonding onto the concrete surface of one or more layers of CFRP was carried out according to the following procedure. Firstly, concrete surfaces were covered with a continuously thick adhesive layer for even surface impregnation, the fabric was cut at the desired size, the adhesive penetrates completely into the fabric's open spaces by using flexible roller. Subsequently, the second layer of adhesive was immediately applied to create a uniform layer of bonded surface reinforcement on top of the fabric. The second adhesive layer was applied in the direction of the fibres with a trowel without excessive pressure and movements. The process was repeated as additional layers of fabric in Fig. 3. Figure 3: beam after the installation of CFRP. Beam strengthening included different layers of CFRP and different schemes reported as in Tab. 4. The beams were subjected to a monotonic load up to failure using a 200 kN hydraulic jack. By Using linear variable displacement transducers LVDT, the deflection of all specimens was measured at the mid span as in Fig. 4. Figure 4: Test Set-up. K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 127 Table 4. Strengthening scheme. Deflection and failure modes The mechanisms of failure can be categorized in global failure and local failure [13-15].  global failure involves compression failure of concrete in bending before or after yielding of steel, rupture of FRP layer in tension, and shear failure of concrete. Beam No. Strengthening schemes Type of strengthening B 00 Control beam B 01 One layer with length 1700 mm B 02 two layers with length 1700 & 1400 mm B 03 three layers with length 1700 & 1400 & 1100 mm B 04 One layer and on sides above bottom edge by 20 mm with length 1700 mm B 05 One layer and 6 U shapes B 06 two layers and 6 U shape B 07 Three layers and 6-U shape B 08 One layer with length 1700 mm with lower longitudinal reinforcement 16 mm diameter B 09 One layer with length 1700 mm with lower longitudinal reinforcement 12 mm diameter K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 128  local failure is characterized in some places with high interfacial peeling or shear stresses, which may cause the debonding of the composite layer from the concrete beam. Various failure modes, controlled by the mechanical properties of the materials and the strengthening configuration was founded in the tested specimens. EXPERIMENTAL RESULTS Control beam he reference beam B00 had a yield load of 39.9 kN and a maximum load of 51.20 kN. The beam failure began with the yield of steel, then very high ductility values were observed, steel tension failure was observed at mid-span. The ultimate deflection was 32.01 mm (see also Tab. 5). One layer strengthening of beams Beam B01 was strengthened with a single layer parallel to the bottom surface of the beam. The beam reinforcement reached its yield at a load of 59.70 kN and supported a maximum load of 69.44 kN with strength gain of 135 % compared with the control beam, while its deflection at failure reached 27.72 mm. Beam B01 showed higher initial stiffness. At mid-span, flexure cracks started, followed by debonding of the CFRP as in Fig. 8. Specimen B04 with strengthened with one layer on the soffit of the specimen and on sides. The ultimate load was 75.66 kN with a strength increase of 148%. The final failure occurred by rupture of CFRP in the lower chord and then on sides of the beam after concrete crushing in compression at mid-span at a deflection of 31.74 mm. Beam B05 had one sheet with a width of 100 mm attached on the bottom chord and 6 U shape sheets with a width of 50 mm wrapped on the bottom and on the sides to prevent CFRP debonding. The ultimate load was 73.76 kN with a strength increase of 144%. The failure was ductile because the deflection at failure was approximately twice the deflection at the yield of steel reinforcement. At the mid-span, flexure cracks occurred, followed by CFRP sheet rupture at the bottom chord. Figure 5: load-deflection curve for one-layer beams. Two and three layers strengthening of beams Beam B02 was reinforced with two layers of CFRP. The strengthening was applied on the bottom of the beam with unequal lengths (1700 mm and 1400 mm). The yield load was 62.72 kN and the ultimate load was 75.10 kN, which represents a gain in strength of 147 %. The beam failure was sudden and brittle due to the rupture of the reinforcing composite material. The beam failure was sudden and brittle in form of rupture of the reinforcing composite material. Several flexural cracks occurred T 0 10 20 30 40 50 60 70 80 0 10 20 30 40 50 60 70 80 L o ad ( k N ) Mid-span deflection (mm) B00 B01 B04 B05 K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 129 in the central span of the beam before the composite material failed. The maximum deflection at failure was 27.58 mm as in (Fig. 8). The strengthening of beam B06 was similar to Beam B05, except for the number of layers, which is two rather than one. The rupture started with the CFRP wrapped sheets and then the CFRP bottom chord, at the final load of 87.85 kN and the ultimate deflection of 36.96 mm. Beam B03 was strengthened with 3 layers of CFRP, and the failure occurred in the concrete compression zone, followed by the rupture of CFRP. The maximum load was 79.39 kN, which is higher than B00 by 155%, and the maximum deflection was 23.33 mm. specimen B06 with two strengthening layers and 6 U-shape sheets had a maximum load of 87.85 kN with a strength gain of 172 % compared with B00. At mid-span, more cracks started, followed by debonding of the CFRP (Fig. 8). beam B07 with three layers and 6U-shape sheets showed that had a maximum load of 88.78 kN with approximately 2% strength gain compared with B06, the deflection was 30.97. Figure 6: Comparison of the load vs. mid-span deflection of: (a) beams strengthened by two layers CFRP, (b) beams strengthened by three layers CFRP. Different reinforcement strengthening of beams Specimens B08 and B09 were strengthened by one layer of CFRP with different reinforcement ratio. Their ultimate loads increased by 43 % and 16 % compared with B01, respectively. For B08 large shear cracks with almost 45° from supports. The beam failed completely at the load of 99.08 kN due to failure in the shear region. But for B09, the failure occurs firstly in concrete compression zone, then rupture of the CFRP sheet at a load of 80.38 kN as in Fig. 8. Ductility characteristics In the seismic regions, ductility is a significant parameter for the design of concrete structures. The ductility can be evalua- ted in terms of energy or deflection. For comparison purposes, Thomsen et al. [16] use ductility depended on the concept of energy, µE, described as the ratio of the system's energy at failure, Eu, to that of the first steel yield, Ey. The concept of deformation is based on the deflection ductility index (displacement at failure divided by displacement at yield) while the energy ductility is measured as the ratio of the area under the load deflection curve at ultimate failure to the area under the 0 10 20 30 40 50 60 70 80 0 10 20 30 40 50 60 70 Lo a d  ( k N ) Mid‐span deflection (mm)  B00 B02 B06 0 10 20 30 40 50 60 70 80 90 0 10 20 30 40 50 60 70 Lo a d  ( k N ) Mid‐span deflection (mm)  B00 B03 B07 (a) (b) K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 130 load deflection curve at yielding of tension steel. Oudah and Hash [17] recently published a new definition of ductility, a model based on beam deflection and energy. The ductility indexes can be described as: Deflection ductility: μ∆=∆u/∆y (1) Energy ductility: μE = Eu/Ey (2) Tab. 6 displays the energy and deflection ductility of the prepared RC beams reinforced by using different combinations of CFRP. It was also found that the beam without strengthening displayed greater displacement or ductility relative to concrete beams of different CFRP configurations. Figure 7: load-deflection curve for one layer with different reinforcement. Beam No. At first crack At steel yield At failure Load (kN) Deflection (mm) Load (kN) Deflection Δy (mm) Max Load (kN) Deflection Δu (mm) B 00 11.80 1.98 39.9 8.35 51.20 32.01 B 01 16.73 2.1 59.7 14.10 69.44 27.72 B 02 26.32 6.45 62.72 14.32 75.1 26.13 B 03 25.59 3.45 63.88 14.88 79.39 23.33 B 04 21.88 1.51 60.25 14.51 75.66 31.74 B 05 13.68 1.54 60.15 16.83 73.76 32.96 B 06 17.47 2.56 80.50 25.61 87.85 36.96 B 07 23.99 2.17 71.55 20.44 88.78 30.97 B 08 15.58 1.09 88.8 23.77 99.06 33.76 B 09 12.17 1.46 53.07 14.27 80.38 36.56 Table 5: Tested specimen data. K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 131 Figure 8: Failure mode of the tested beams. Beam No. Ductility Ductility ratios In terms of deflection µ In terms of energy µ In terms of deflection µ In terms of energy µ B 00 3.83 5.96 1 1 B 01 1.97 2.64 0.51 0.44 B 02 1.54 1.92 0.40 0.32 B 03 1.57 2.08 0.41 0.35 B 04 1.68 2.09 0.44 0.35 B 05 1.96 2.66 0.514 0.45 B 06 1.49 1.64 0.39 0.28 B 07 1.51 2.06 0.39 0.34 B 08 1.42 1.49 0.37 0.25 B 09 2.56 3.70 0.67 0.62 Table 6: Ductility index. K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 132 VERIFICATION STUDY he finite element (FE) models were calibrated with the experimental results. The purpose of this comparison is to verify the validity of the analysis and model. As in the (Fig. 10), there is a really very good correlation between the experimental and numerical load-deflection curves for all loading stages. the FE models were able to predict the Load-carrying capacity of RC beams. The validity and reliability of the FE models established to simulate the experimental performance. The concrete is modelled using the form of element SOLID65 [18]. This element has eight nodes with three degrees of freedom at each node; translations in the global reference directions x, y, and z. This element is capable of plastic deformation, cracking and crushing in three orthogonal directions. The nonlinear behavior of geometry and properties of materials for concrete structures was considered in this research according to several sources [2, 19-22], the mechanical properties of concrete, FRP plate and adhesive are selected and are given in Tab. 7. Material Elastic modulus (GPa) Poisson’s ratio Compressive strength (MPa) Yield strength (MPa) Tensile strength (MPa) Concrete 32 0.20 32 3.02 Steel bars 30.6 0.30 500 CFRP 230 0.30 Epoxy 4.50 0.30 Table 7: Mechanical properties of concrete, steel and CFRP reinforcement. Figure 9: (a) Sample representation of developed FE models., (b) different element of the beam modeled. Tab. 8 summarizes the comparison of experimental and numerical results achieved for all specimens studied and demonstrates that the analytical approach discussed here can be used to model strengthened beam behavior in a satisfactory way when there is no premature delamination of the strengthened composite material. The proposed ANSYS [23] model results showed acceptable agreement with the experimental results, with deviations of less than 10 %. T (b) (a) K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 133 0 10 20 30 40 50 60 70 80 0 20 40 60 Lo a d  ( k N ) Mid‐span deflection (mm)  B02 EXP B02 ANSYS BOO EXP BOO ANSYS 0 10 20 30 40 50 60 70 80 0 20 40 60 Lo a d  ( k N ) Mid‐span deflection (mm)  B01 EXP B01 ANSYS B03 EXP B03 ANSYS 0 10 20 30 40 50 60 70 80 90 0 10 20 30 40 50 60 70 Lo a d  ( k N ) Mid‐span deflection (mm)  B07 EXP B07 ANSYS B06 EXP B06 ANSYS 0 10 20 30 40 50 60 70 80 0 20 40 60 Lo a d  ( k N ) Mid‐span deflection (mm)  B04 EXP B05 EXP B04 ANSYS B05 ANSYS K. Fawzy et al, Frattura ed Integrità Strutturale, 56 (2021) 123-136; DOI: 10.3221/IGF-ESIS.56.10 134 Figure 10: comparison between experimental and numerical load - deflection curve for B00 to B09. Beam No. Theoretical (Ansys) Experimental 𝑃 𝑃 Failure mode (Experimental) Load (kN) Deflection Δu (mm) Load (kN) Deflection Δu (mm) B 00 51.39 30 51.20 32.01 1 Concrete crushing B 01 75.21 23.92 69.44 27.72 1.08 debonding of the CFRP B 02 77.67 23.82 75.1 26.13 1.03 Rupture of the CFRP B 03 76.39 23.69 79.39 23.33 0.96 Rupture of the CFRP and Concrete crushing B 04 72.43 31.76 75.66 31.74 1 Rupture of the CFRP and Concrete crushing B 05 78.43 24.79 73.76 32.96 1.06 Rupture of the CFRP B 06 88.03 24.53 87.85 36.96 1 Rupture of the CFRP B 07 86.43 26.48 88.78 30.97 0.97 Rupture of the CFRP B 08 100.15 24.3 99.06 33.76 1.01 Local shear rupture B 09 82.25 22.56 80.38 36.56 1.02 debonding of the CFRP Table 8: Comparison between experimental and theoretical results. CONCLUSIONS he aim of this analysis is to investigate the influence of different parameters on the flexural behavior of repaired concrete beams, such as the number of layers, strengthening scheme (side and U-shape bonding), and reinforcement ratio. Based on these experimental and numerical results, we can deduce the following:  The outcome of the experimental program shows that externally bonded CFRP may be used to support reinforced concrete beams effectively. With the increase in CFRP layers, an increase in stiffness and flexural strength was observed. T 0 20 40 60 80 100 0 10 20 30 40 Lo a d  ( k N ) Mid‐span deflection (mm)  B08 EXP B09 EXP B08 ANSYS B09 ANSYS K. 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