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Article

Strength Profile Pattern of FRP-Reinforced Concrete Structures: A Performance Analysis through Finite Element Analysis and Empirical Modeling Technique

1
Department of Civil Engineering, University of Engineering and Technology, Taxila 47080, Pakistan
2
Department of Civil Engineering, Pakistan Institute of Engineering and Technology, Multan 66000, Pakistan
3
National Center for Environmental Technology (NCET), Life Science and Environment Research Institute (LSERI), King Abdulaziz City for Science and Technology (KACST), Riyadh 11442, Saudi Arabia
4
Department of Electrical Engineering, Bahauddin Zakariya University, Multan 66000, Pakistan
5
School of Aerospace, Mechanical and Mechatronic Engineering, The University of Sydney, Camperdown 2006, Australia
*
Author to whom correspondence should be addressed.
Polymers 2021, 13(8), 1265; https://doi.org/10.3390/polym13081265
Submission received: 15 March 2021 / Revised: 5 April 2021 / Accepted: 6 April 2021 / Published: 13 April 2021

Abstract

:
Limited research work is available in the literature for the theoretical estimates of axial compressive strength of columns reinforced with fiber reinforced polymer (FRP) rebars. In the present work, an experimental database of 278 FRP-reinforced concrete (RC) compression members was established from the literature to recommend an empirical model that can accurately predict the axial strength (AS) of GFRP-RC specimens. An initial assessment of 13 different previously anticipated empirical models was executed to achieve a general form of the AS model. Finally, a new empirical equation for forecasting the AS of GFRP-RC short columns was proposed using the curve fitting and regression analysis technique. The performance of the proposed empirical model over the previous experimental database represented its higher accuracy as related to that of other models. For the further justification of the anticipated model, a numerical model of GFRP-RC columns was simulated using ABAQUS and a wide parametric study of 600 GFRP-RC samples was executed to generate a numerical database and investigate the influence of various parameters using numerical and empirical models. The comparison between theoretical and numerical predictions with R2 = 0.77 indicted that the anticipated empirical model is accurate enough to apprehend the AS of FRP-RC specimens.

Graphical Abstract

1. Introduction

The high maintenance costs and limited-service life of conventional steel reinforcement in aggressive and corrosive environments have spurred the interest of modern research in advanced composite materials such as fiber-reinforced polymers (FRPs). The higher tensile strength, lower density, lighter weight, lower maintenance costs, higher resistance to corrosion, lower conductance to temperatures, and high resistance to chemical environments are the main advantages of FRPs [1,2,3,4,5]. These days, the construction industry is focusing on the replacement of corrosive steel reinforcement with the FRP rebars and confinements due to their superiorities over steel rebars to minimize the effects of corrosion in aggressive and corrosive environments [6,7,8,9]. Most of the concrete bridges in the United States and Canada employed the FRP reinforcement as a partial or total replacement of steel rebars [10]. Although, the use of FRPs in the construction industry has been increased still no design guidelines have been added in North American codes for such reinforcement. Furthermore, the use of FRP rebars as longitudinal compressive reinforcements has been prevented in Canadian codes [11,12] due to the limited research and advancement in this area. This may also be associated with the uncertain performance of FRP rebars in compression and limited experimental data.
During the last few decades, for providing the flexural and shear reinforcements, the employment of FRP rebars in reinforced concrete members is increasing [13,14]. Some investigations have been carried out to examine the performance of FRP rebars as longitudinal and transverse reinforcements in compressive and flexural members which depicted a better response of FRP rebars in these members [15,16,17,18,19,20,21]. As the axial compressive performance of FRP rebars is lower than that of steel rebars, therefore, some investigations have been carried out to determine the strength reduction coefficients for FRP rebars to secure the most optimum results under compressive loads [22,23,24,25]. But there is still a need for refining these coefficients using an experimental database consisting of various sample points. The previously suggested models for the axial strength of columns reinforced with FRP rebars have deficiencies such as they were suggested based on small data points, the axial contribution of FRP rebars was not included in the axial compressive performance and bending performance and the compressive and tensile properties of FRP rebars were assumed to be the same. The axial strength (AS) is significantly improved by improving the lateral confinement of the concrete core but the steel reinforcement performs better than FRP reinforcement in compressive members after increasing the lateral confinement of the core [26,27,28]. The predictions are underestimated by neglecting the axial influence of FRP bars in columns while the predictions portray a close agreement with the experimental outcomes by considering the influences of AS and axial stiffness of FRP rebars [17,29,30,31].
Mohamed et al. [32] examined the behavior of fourteen (14) sand-coated FRP-reinforced columns confined with FRP ties/spirals under axial compressive load. Using smaller ratios of transverse reinforcement (0.7%), damage of the specimens happened due to buckling of longitudinal rebars. Similarly, using moderate ratios of transverse FRP confinement (1.5% and 2.7%), the damage of specimens happened due to the damage of spirals and the crushing of the core. Afifi et al. [33] anticipated an equation for GFRP-confined concrete based on the criterion of Willam-Warnke. This model was adjusted utilizing the regression analysis method on the experimental testing outcomes for envisaging the ultimate AS and corresponding axial strain of GFRP-RC columns. Twelve (12) circular GFRP-RC columns (with 205 mm diameter and 800 mm height) were studied by Hadi et al. [34] under various loading circumstances. The testing results depicted that the bending moment capacity and AS of GFRP-RC compression members were less than their identical steel-RC columns. Additionally, ignoring the influence of GFRP bars in the loading strength of columns origins an extensive discrepancy between the testing measurements and analytical predictions. Karim et al. [35] proposed a model for forecasting the axial load-deflection performance of GFRP-RC columns confined with GFRP spirals. Moreover, the effect of spiral-pitch and external GFRP sheets was also investigated. There was observed a two-peak axial loading performance of GFRP-RC columns confined with sheets; the first peak represented the axial capacity of concrete cross-section and the second represented the axial capacity of FRP-confined concrete core.
As concerned with the finite element analysis (FEA) of FRP-reinforced compressive members, a large of studies could be found in the literature that investigates the structural performance of such members using FEA under various conditions [5,19,20,30,36,37,38,39,40,41]. From these studies, it was detected that the projected FEA models captured the structural behavior of FRP-reinforced concrete compressive members precisely. The finite element models (FEM) represent all the shortages of the empirical models. In comparison with the experimental work, finite element simulation saves time and cost by generating computational models that can correctly capture the complex damage behavior of composites [42]. As FEA consumes huge time during the simulations that can be minimized by making some assumptions but these assumptions should be in such a way that they should not affect the accuracy of the models and give close estimations with the experimental outcomes at the same time. One should keep a balance between the analysis time, complexity of the models, size of the elements, and different types of elements in the models. Thus, FEA having a strong background knowledge is a very important and effective tool for the analysis of the structural engineering problems related to composites [43].

Scope and Significance

It was observed from the literature review that there is a lack of studies on predicting the axial compressive strength of FRP-reinforced columns confined with FRP composites. Due to insufficient research data in this area, various international guidelines do not endorse the usage of such reinforcement in concrete columns. Therefore, detailed research is required in this area to provide some design guidelines for the structural performance of FRP-reinforced members under compressive loads. The main aims of the present investigation are: (a) To suggest a novel theoretical model for apprehending the axial compressive strength of FRP-reinforced concrete compressive elements based on various testing outcomes collected from the previous works; (b) to suggest a novel FEA model for accurately apprehending the compressive performance of such members with a minimum time; and (c) a detailed parametric investigation of GFRP-reinforced elements to observe the influence of various geometric and material variables of such members. To propose a novel theoretical model, an evaluation of the previous model over the constructed database has been performed to select the most suitable form. To perform FEM, a modified concrete damage plastic (CDP) model [30] is used for the simulations of the complex performance of concrete and the FRP bars are considered as a linear elastic material. The FEM has been proposed for the validation and comparison purposes of the newly anticipated theoretical model. The experimental results for the calibration and validation of FEA models have been taken from the literature [29]. Besides, widespread parametric training was accomplished using the anticipated FEM and empirical model to generate the results for the validation and comparison of the proposed models. A close agreement was observed between the predictions of the proposed empirical equation and FEM. The currently proposed empirical model has superiority over the previously suggested models for predicting the axial strength of GFRP-reinforced columns because it has been proposed over the large experimental dataset giving more accuracy and considering a large number of parameters of specimens. Furthermore, it is simpler and easier for practical applications. This research work is helpful for the analysis of GFRP-reinforced columns for the concrete construction industry.

2. Materials and Methods

Database for Empirical Modeling

Many experimental research investigations have been done in the literature to study the axial performance of GFRP-RC columns. In the present research, a database of 278 FRP-RC columns was created from different research papers. The longitudinal FRP rebars and steel ties, steel spirals, FRP ties, or FRP spirals were employed as the longitudinal and transverse reinforcements in all the specimens in the constructed database. In the database, ten (10) columns were transversely unconfined, seven (7) columns were transversely reinforced with CFRP spirals, one hundred and ten (110) columns were transversely reinforced with GFRP spirals, hundred (100) columns were transversely reinforced with GFRP ties, eighteen (18) columns were transversely reinforced with steel spirals, and thirty-three (33) columns were transversely reinforced with steel ties. Various parameters have been included in the development of the database such as transverse reinforcement ratio ( ρ t ), the elastic modulus of FRP bars ( E f ), concrete compressive strength ( f c ), longitudinal FRP reinforcement ratio ( ρ l ), the ultimate tensile strain of FRP bars ( ε u ), the tensile strength of FRP bars ( f u ), breadth ( B ), width ( H ), and axial loading capacity ( P n ) of specimens. Table 1 reports all the statistics of the parameters of the created database (provided in Appendix A).

3. Evaluation of Previous Models

Thirteen (13) existing models were assessed on the constructed database of GFRP-RC columns for selecting the most appropriate form of the newly proposed model. All the models that have been assessed for proposing the new general form of the model, are reported in Table 2. Three different statistical parameters (root mean squared error (RMSE), coefficient of determination (R2), and the mean absolute error (MAE)) were employed for the assessment of the models as reported by Equations (1)–(3). R2 is the most important parameter for examining the accuracy of a proposed theoretical model, therefore, the assessment of the models has been focused on using this parameter in the present research. The flow chart reported in Figure 1 presents the methodology of this investigation.
R 2 = ( n ( i = 1 n x i y i ) ( i = 1 n x i ) ( i = 1 n y i ) [ n i = 1 n x i 2 ( i = 1 n x i ) 2 ] [ n i = 1 n y i 2 ( i = 1 n y i ) 2 ] ) 2
M A E = 1 n i = 1 n | x i y i |
R M S E = 1 n i = 1 n ( x i y i ) 2
In these expressions, n reports the number of test points, x i reports the AS taken from experiments and y i reports the AS taken from the empirical models. Figure 2 depicts the evaluations of the previous models over the database. These evaluations portray that the best accuracy is given by the Afifi et al. [23] model with the maximum value of R2 i.e., R2 = 0.711. If R2 is close to one (1.0), it will report a good correlation of theoretical estimates with the experimental outcomes. A value close to zero will report a week performance of the theoretical model. Due to the highest performance of the Afifi et al. [23] model, the general shape of the developed model was kept similar to that in this model. This model considers the axial influence of FRP bars by assuming a reduction factor for the tensile strength of FRP rebars. Although including the fractal model concept during the modeling can give more accurate results [53] but the fractal model concept of FRP bars (curvy geometrical figure and initial geometric imperfection) in the present study has been neglected to make the proposed model simple for the practical applications and to avoid the complexity of the model. The general shape of the projected theoretical model is reported by Equation (4).
P n = α 1 ( A g A F R P ) f c + α 2 f F R P A F R P
In this expression, α 1 and α 2 represent the reduction coefficients for the AS of FRP-reinforced compression members due to compressive influence of FRP rebars and confined core, A F R P is the area of FRP rebars, A g is the gross area of the column, f F R P is the tensile strength of FRP rebars. In the present investigation, the curve fitting method in MATLAB has been employed for securing the finest fit with the testing outcomes. The relationship for α 1 as recommended by Ref. [11] can be reported by Equation (5).
α 1 = 0.85 β f c
where β is another constant. Putting this value to Equation (6), the following relationship is obtained:
P n = ( 0.85 β f c ) ( A g A F R P ) f c + α 2 f F R P A F R P
The obtained values from the curve fitting method in MATLAB for the constants α 2 and β were 0.0208 and 0.0029, correspondingly. Finally, the proposed model for the AS of FRP-reinforced members, after incorporating the values of the coefficients, has been reported by Equation (7).
P n = ( 0.85 0.0029 f c ) ( A g A F R P ) f c + 0.0208 f F R P A F R P
where the reduction coefficient for AS of columns due to strength of concrete should be larger than 0.646 i.e., α 1 = 0.85 0.0029 f c 0.646 . Figure 3 depicts that the newly suggested model for the AS of columns reported higher accuracy than the previous models with R2 = 0.73.
Figure 4 reports the sample circulation of the previous testing and predicted AS of FRP-reinforced columns. In range 0–2000 kN, the experimental datapoints were counted to be 189 in the developed database. There were 194 datapoints of the predictions of the suggested model. In the range, 2001–6000 kN, the experimental and theoretical counts were 81 and 86, correspondingly. Similarly, in the range, 6001–10,000 kN, the experimental and theoretical counts were zero and 2, correspondingly. Similarly, in the range, 10,001–16,000 kN, the experimental and theoretical counts were 4 and 2, correspondingly. These comparisons show that the predicted values of the proposed model apprehended the AS of FRP-reinforced columns very well.
Figure 5 reports the normal distribution of testing strengths to prophesied strengths of GFRP-reinforced compressive members from the created database for all models. The data of this figure has been obtained from the normalized predictions of various previous models over the developed database. The newly suggested model reported a deviation of only 5% for the average normalized strengths of the ratios of testing values to theoretical values. ACI-318-08 [44] reported a maximum deviation of 42%. Such errors may be ascribed to the cause that the model anticipated by ACI-318-08 [44] is for the steel rebars. This model has been used in this investigation for only a comparative purpose. Furthermore, the percent average eccentricities for the equations recommended by Afifi et al. [23], Khan et al. [47], CSA S806-12 [11] were 22%, 31%, and 5%, correspondingly.

4. Finite Element Modelling

This section presents the methodology of the FEA of GFRP-RC columns under various loading situations. A total of seven GFRP-RC specimens were defined using a finite element software ABAQUS whose experimental results were taken from the previous research of Elchalakani et al. [29]. The details of all specimen are provided in Table 3. A control model (G150-45) was selected for the calibration purpose of the GFRP-RC columns. During the calibration of the control specimen, various geometric and materials characteristics of the control specimen such as support conditions, the plastic performance of concrete, element sizes, and various element types were studied to gain the results that give the minimum error as compared with the experimental outcomes. The boundary conditions were applied to the control model such that the bottom end of the specimen was controlled in all directions and the top portion of the specimen could freely translate and rotate in all directions. The simulations of GFRP reinforcement and concrete material were done using three-dimensional 8-noded brick and three-dimensional 2-noded truss elements, correspondingly. The bond behavior between the reinforcement and concrete was simulated using the “embedded region” that joins the degrees of freedom (DOF) of the truss sections of FRP bars to the essential DOF of concrete three-dimensional stress elements. The load was applied to the top center of the specimen using the displacement control technique. The geometry and support conditions of the simulated specimens are presented in Figure 6.

4.1. Simulation of Concrete Material

The behavior of concrete is complex due to the various constituents required for its manufacturing. The finite element simulation of this complex-natured material is a challenging task. In the present numerical work, the geometric performance of concrete was defined using three-dimensional brick elements with 8 nodes with reduced integration property (C3D8R). The average compressive strength of concrete material was 32 MPa at 28 days. The elastic behavior of concrete was defined using the equation given by ACI 318-11 [50] as presented by Equation (8).
E c = 4700 f c
The concrete damaged plastic (CDP) model available in ABAQUS was used for the definition of the plastic performance of concrete. This relationship considers the crushing of concrete under compressive loading and the cracking of concrete under tensile loading to accurately predict the plastic behavior of concrete [54,55]. The CDP model divides the plasticity behavior of concrete into three parts: plastic, compressive, and tensile behavior. The plastic performance of concrete material was calibrated for all the parameters of plasticity available in the CDP model of concrete i.e., stress ratio, dilation angle, shape factor, viscosity parameter, and eccentricity of concrete. For the definition of concrete performance under compressive loading, the stress–strain relationship provided by Eurocode 2 [56] was utilized as presented by Figure 7a. The linear elastic behavior of concrete was taken up to 40% of the ultimate strength of concrete [57]. The ultimate strain ( ε c u ) and the strain at ultimate compressive strength of concrete ( ε c ) were calculated using Equation (9) and (10) as recommended by [58]. The compressive stresses ( σ c ) were calculated using the relationship given by Eurocode 2 [56] as presented by Equation (10).
ε c = 0.0014 [ 2 e 0.024 f c e 0.140 f c ]
ε c u   = 0.004 0.0011 [ 1 e 0.0215 f c ]
σ c = f c k η η 2 1 + ( k 2 ) η
where k = 1.05 E c ε c u f c ,   η =   ε c ε c u .
The tensile behavior of concrete in the CDP model was defined using the modified tension stiffening model [59] as shown in Figure 7b. This model considers the behavior of concrete at post failure conditions of concrete such as tension stiffening, strain hardening, and softening and the interactions of FRP reinforcement with the concrete material. The tensile strength of concrete ( f t ) was determined using the model proposed by Ref. [60].
f t = 0.33 f c

4.2. Simulations of FRP Bars

The geometric definitions of reinforcing bars were accomplished using 3-D truss sections having two nodes with three DOF at each node (T3D2). The definition of elastic performance of FRP bars was carried out using two variables i.e., Poisson’s ratio and Young’s modulus that were taken as 0.25 [37] and 50 GPa, correspondingly [29]. FRP bars show sudden failure with rupture after yielding strength. Therefore, the plastic performance of GFRP bars was assumed as linear elastic up to failure without the application of any damaging criterion [38]. The tensile strengths of longitudinal and transverse GFRP bars were considered as 1200 MPa and 784 MPa, correspondingly [29]. Figure 8 represents the simulated behavior of GFRP longitudinal and transverse bars in ABAQUS.

4.3. Calibration of FEM

One of the GFRP-RC columns (G150-45) was selected for calibration purposes. The numerical results of the load-deflection curve of the control model were compared with the experimental results from Ref. [29]. After calibrating the control model, it was used for the analysis of the other six specimens to further authenticate the accuracy of the anticipated finite element model. The control model was calibrated for different element types of GFRP and concrete material, mesh sizes, the eccentricity of concrete, shape factor, viscosity parameter, stress ratio, and dilation angle of concrete.
Various element types of concrete material and FRP reinforcement were evaluated to examine the effect of their variation on the load-deflection behavior of control finite element specimens. The 3-D stress elements available in the ABAQUS library for concrete material include hexahedral (C3D8R & C3D20R), tetrahedral (C3D4H & C3D10H), and triangular (C3D6H & C3D15H) elements that were studied during the calibration process. Similarly, the FRP reinforcing bars were studied for different truss (T3D2R & T3D3R) and beam (B31H & B32H) elements. It was observed that C3D8R and T3D2R gave the best results for concrete and reinforcement, correspondingly as presented in Figure 9 which displays the load-deflection response of the control column.
The effect of increasing or decreasing the mesh size was also studied. The finite element models are always meshed size-dependent. This may be due to the phenomenon of strain localization that causes the unloading of some elements in the model. The studied mesh sizes were 15, 20, 25, 30, 40, and 50 mm. The best results were obtained while using a mesh size of 20 mm throughout the specimen. Figure 10a presents the load-deflection response of the control model by using different values of mesh size of the specimen.
The dilation angle of concrete, which represents the internal frictional angle, should range between 30° and 45° [61,62,63,64,65,66]. In the present investigation, the studied values of dilation angle were 30°, 33°, 35°, 38°, 40°, 43°, and 45°, correspondingly. The effect of variation of the dilation angle was not significant for the load-deflection response of the control specimen as reported in Figure 10b. However, the dilation angle of 35° gave a close agreement of numerical outcomes of the load-deflection curve with the experimental measurements.
The sensitivity of the viscosity parameter of concrete on the axial performance of the GFRP-RC column was also investigated. Various values of viscosity parameter used for the adjustment were 0.0068, 0.0058, 0.0048, 0.0038, 0.0028, and 0.0018. The effect of the viscosity parameter on the load-deflection response of the control model is presented in Figure 10c. There was an increase of 20.41% in the axial capacity of the specimen when the viscosity parameter was improved from 0.0018 to 0.0068. However, a close correlation with the experimental results was observed while using a viscosity parameter of 0.0058.
The effect of the shape factor for the yielding surface of the concrete on the load-deflection performance of the control model is presented in Figure 10d. With the increase or decrease of shape factor from 2/3, the ultimate load of the specimen decreases. Thus, the best approximation for the testing load-deflection behavior of the GFRP-RC control model was observed at a value of 2/3. Similarly, the effects of stress ratio and eccentricity of concrete were also examined. The results indicated that these two parameters have no significant effect on the axial performance of GFRP-RC specimens. Therefore, the default values i.e., 1.16 and 0.1 were used for these parameters, correspondingly.

5. Results and Discussion

The load-deflection curve of the control model represents that the percentage discrepancy between the numerical and experiments was 6.23% for the maximum loading capacity and 9.70% for the axial deflection at a maximum loading capacity of GFRP-RC specimen. However, the overall performance of the curve was closely captured by the proposed FEM. The minor discrepancies between the experimental and FEM results may be due to the differences between assumed boundary conditions in numerical simulations and experimental testing. Furthermore, the discrepancies may be associated with the geometric imperfections, differences in the strength of concrete and FRP material, the accuracy of laboratory instruments, manufacturing faults of specimens, and the assumptions made during the simulations.
After the validation of the control model, it was employed for the analysis of all other GFRP-RC columns from Ref. [29]. Table 4 represents the results obtained from the finite element simulations and their discrepancies from the experimental measurements. The average percentage discrepancy of finite element simulations from the experiments was 3.78% for loading capacity and 15.9% for the corresponding deflection at ultimate loading capacity.

Load-Deflection Performance of FEM

The load-deflection curves of concentrically loaded GFRP-RC specimens are presented in Figure 11. The anticipated FEM predicted the axial behavior of concentric specimens with high accuracy in the elastic region of the load-deflection curve. However, the post-buckling behavior of specimens was not exactly traced. This may be due to the assumption of linear elastic performance of GFRP reinforcement up to failure in the simulations. In concentric columns, the GFRP bars are subjected to pure compression and the compressive performance of GFRP bars was taken as similar to the tensile behavior that may also be a reason for the discrepancy of results during the post-peak behavior. The FEM of the GFRP-RC specimen with 75 mm stirrup spacing tested under concentric loading (G75-C) portrayed the percentage faults of 2.56% and 13.92% for the maximum capacity and axial deflection at that capacity, correspondingly. The specimen G150-C showed percentage errors of 1.26% for axial capacity and 17.46% for the corresponding axial deflection. Similarly, the discrepancies for AS and axial deflections were 1.79% and 21.07%, correspondingly. The average differences between the simulations and experimental measurements of concentric GFRP-RCC specimens were 5.21% and 14.70% for peak loading capacity and axial deflection at that loading, correspondingly.
In the case of eccentric GFRP-RC columns, the proposed FEM predicted the axial performance of specimens with high accuracy. Figure 12 represents the finite element and experimental load-deflection curves of the eccentrically loaded GFRP-RC specimens. It can be observed that the FEM of the specimen G75-25 gave a percentage error of 2.34% and 21.36% for the axial ultimate load and equivalent axial deflection, correspondingly. The percent error for specimen G75-35 was 11.84% for axial load and 17.45% for the axial deflection of the columns. The column with 150 mm stirrups spacing tested with an eccentricity of 25 mm (G150-25) presented the discrepancies of 0.41% and 10.28% for axial capacity and corresponding deflection, correspondingly. Similarly, the control specimen G150-45 presented the errors of only 6.23% and 9.70% for load and deflection, correspondingly. All the eccentrically loaded specimens showed an average discrepancy of 5.21% for the peak load and an average discrepancy of 14.70% for the axial deflection at the peak load. This discussion represents that the anticipated FEM predicts the axial loads of concentric GFRP-RC columns and axial deflections of eccentric GFRP-RC columns with higher accuracy.

6. Parametric Investigation

After validation, the anticipated FEM and empirical models were employed for the further analysis of 600 GFRP-reinforced rectangular columns under compressive loads. Four (4) different parameters of columns (a) longitudinal FRP reinforcement ratio ( ρ l ), (b) concrete compressive strength ( f c ), the tensile strength of GFRP rebars ( f u ), and width of column ( B ) was varied for different ranges to examine their effect on the axial capacity (strength) of the columns as reported in Table 5. The main aim of the parametric study was to construct a database of GFRP-RC columns with various geometrical and material parameters so that the predictions of proposed capacity models could be verified and compared by using these results.

6.1. Using FEA Model

6.1.1. Influence of Width of Column (B)

Figure 13 reports the influence of the effect of “B” of the GFRP-reinforced column on their AS. The examined values of this parameter were 375, 350, 325, 300, 275, 250, 225, 200, 175, and 150 mm. The enhancement of “B” from 150 to 375 mm resulted in an increase of 1041% in the axial compressive strength of GFRP-reinforced members with the enhancement of f c from 10 to 55 MPa at ρ l of 1.94% and fu of 850 MPa as fixed. Similarly, the enhancement of “B” from 150 to 375 mm resulted in an upsurge of 151% in the AS with the enhancement of f u from 700 to 1150 MPa.

6.1.2. Influence of Concrete Compressive Strength ( f c )

Figure 13 reports the influence of f c on the axial compressive strength of columns. The upsurge of f c from 10 to 55 MPa resulted in an enhancement of 1041% in the AS with the increase of “B” from 150 to 375 mm. Similarly, the enhancement of f c with the increase of ρ l from 0.97% to 5.35% resulted in an improvement of 343% in the AS of columns. By enhancing f c from 10 to 55 MPa, the AS resulted in an improvement of 357% with the upsurge of f u from 700 to 1150 MPa. This portrays that the enhancement of tensile strength of FRP rebars and compressive strength of concrete results in a similar effect on the AS of FRP-reinforced concrete columns.

6.1.3. Influence of Longitudinal Reinforcement Ratio ( ρ l )

The influence of reinforcement ratio was also reported in Figure 13. This parameter has been examined for the various values including 5.35%, 4.86%, 4.38%, 3.89%, 3.41%, 2.92%, 2.43%, 1.94%, 1.46%, and 0.97%. The enhancement of ρ l from 0.97% to 5.35% resulted in an improvement of 343% in the AS with an upsurge of f c from 10 to 55 MPa. Similarly, the enhancement of ρ l with the upsurge of fu from 700 to 1150 MPa resulted in an enhancement of only 0.6%. Furthermore, enhancing the “B” from 150 to 375 mm resulted in an improvement of 149% in the AS with the enhancement of ρ l from 0.97% to 5.35%.

6.1.4. Influence of Tensile Strength of FRP Rebars ( f u )

The influence of changing the f u on the AS is reported in Figure 13. Different values of f u with an augmentation of 50 MPa was examined in the range of 700 to 1150 MPa. The enhancement of fu from 700 to 1150 MPa resulted in an improvement of only 0.6% in the axial compressive strength with the increase of ρ l from 0.97% to 5.35%. An improvement of 151% was observed by enhancing “B” from 150 to 375 mm. Similarly, the enhancement of f u from 700 to 1150 MPa resulted in an improvement of only 357% in the axial compressive strength with the upsurge of f c from 10 to 55 MPa. Finally, it was concluded that the influence of the area of column and strength of concrete was significant on its axial compressive strength as compared with the other parameters.

6.2. Using Empirical Model

6.2.1. Influence of Width of Column (B)

The same parameters were evaluated in the parametric investigation using the proposed empirical model as shown in Figure 14 that displays the influence of “ B ” of GFRP-reinforced column on their AS. The examined values of this parameter were the same as in the numerical parameter study. The enhancement of “B” from 150 to 375 mm resulted in an increase of 1123% in the axial compressive strength of specimens with the enhancement of f c from 10 to 55 MPa at ρ l of 1.94% and fu of 850 MPa as fixed. Similarly, the enhancement of “ B ” from 150 to 375 mm resulted in an upsurge of 214% in the AS with the enhancement of f u from 700 to 1150 MPa.

6.2.2. Influence of Concrete Compressive Strength ( f c )

The effect of f c on the axial compressive strength of columns is reported in Figure 14. The upsurge of f c from 10 to 55 MPa resulted in an augmentation of 1123% in the AS with the increase of “ B ” from 150 to 375 mm. Similarly, the enhancement of f c with the increase of ρ l from 0.97% to 5.35% resulted in an upgrading of 389% in the AS of columns. By enhancing f c from 10 MPa to 55 MPa, the AS resulted in an improvement of 469% with the upsurge of fu from 700 to 1150 MPa.

6.2.3. Influence of Longitudinal Reinforcement Ratio ( ρ l )

Figure 14 also presents the influence of the FRP reinforcement ratio ( ρ l ) on the axial capacity of specimens. This parameter has been examined for the various values as investigated in the numerical parametric study. The enhancement of ρ l from 0.97% to 5.35% resulted in an improvement of 389% in the AS with an upsurge of f c from 10 to 55 MPa. Similarly, the enhancement of ρ l with the upsurge of fu from 700 to 1150 MPa resulted in an enhancement of 125%. Furthermore, enhancing the “B” from 150 to 375 mm resulted in an improvement of 236% in the AS with the enhancement of ρ l from 0.97% to 5.35%.

6.2.4. Influence of Tensile Strength of FRP Rebars (fu)

The influence of changing the f u on the AS was reported in Figure 14. Different values of f u with an increase of 50 MPa were assessed in the range of 700–1150 MPa. The enhancement of f u from 700 to 1150 MPa resulted in an improvement of 125% in the axial compressive strength with the increase of ρ l from 0.97% to 5.35%. An improvement of 151% was observed by enhancing “B” from 150 to 375 mm. Similarly, the enhancement of f u from 700 to 1150 MPa resulted in an improvement of only 469% in the axial compressive strength with the upsurge of f c from 10 to 55 MPa. Therefore, it is concluded that during the parametric investigation, both the models (FEM and empirical models) have portrayed their predictions of the axial strength of GFRP-reinforced columns close to each other.

7. Validation and Comparison of Proposed Models

The purpose of the parametric study using the proposed FEM and empirical models in the present work was to generate a database of GFRP-reinforced compressive members to validate and compare the anticipated models for the axial compressive strength of GFRP-reinforced columns. The numerical and empirical database consisted of 600 results of AS of GFRP-reinforced concentric specimens. The theoretical predictions of these 600 GFRP-RC specimens calculated using the anticipated empirical model were compared with that of the numerical model. The comparative study of FEM and theoretical predictions are reported in Figure 15. It was noticed that the anticipated empirical axial capacity model performed well for the numerical parametric results with an R2 of 0.87. Thus, the anticipated empirical and FEM model is accurate enough to capture the AS of GFRP-reinforced concrete columns.

8. Conclusions

In the present work, an experimental database of 278 FRP-RC compression members was established from the literature to recommend an empirical model that can accurately predict the AS of GFRP-RC specimens. An initial evaluation of 13 different previously anticipated empirical models was executed to achieve a general shape of the AS model. Finally, a new empirical equation for forecasting the AS of GFRP-reinforced short columns was proposed using the curve fitting and regression analysis technique. A validated FEM was suggested for GFRP-reinforced members and used along with an empirical model for a detailed parametric investigation. Following conclusions were extracted from this work.
A better performance has been reported by the newly developed empirical model for apprehending the axial compressive strength of FRP-reinforced concrete compressive members with R2 = 0.73 using a database of 278 experimental data points. This model depicted higher correctness as compared with all previous models for different statistical errors (RMSE and MAE). Furthermore, the new model has been proposed based on a large data of FRP-reinforced columns while the previously proposed models were proposed using small databases.
The axial contribution of FRP rebars has been involved in the model with a reduction factor of 0.85 0.0029 f c 0.646 for the concrete strength and a reduction factor of 0.0208 for the AS of FRP rebars.
The suggested FEM also apprehended the structural performance of FRP-reinforced concrete members with a high accuracy depicting only the errors of 3.78% and 15.9% for AS and equivalent axial deflection, correspondingly.
The parametric investigation depicted that the AS of the concrete and cross-sectional area of the concrete column had a significant influence on the AS of such members. The enhancement of the cross-sectional area of the column by an increase of 1.5 times resulted in the AS up to 1041%. Correspondingly, the enhancement of concrete strength by 4.5 times resulted in an improvement of 357% in the AS of columns. The influence of reinforcement ratio of FRP rebars and tensile strength of FRP rebars reported no significant influence on the AS.
Six hundred (600) specimens were tested in ABAQUS and empirical model to perform the parametric investigation and to generate a theoretical database for the assessment purposed FEM with the estimates of the theoretical model. The comparison reported a close agreement among each other with R2 = 0.87. Thus, the anticipated theoretical and FEA models are precise enough to further analyze the FRP-reinforced concrete columns.

Author Contributions

Conceptualization, A.R., S.A.R.S., H.A., M.A. and S.R.; methodology, A.R., S.A.R.S.; software, A.R., S.A.R.S., H.A.; validation, M.A. and S.R.; formal analysis, A.R., M.A. and S.R.; investigation, A.R., S.A.R.S. and S.R.; resources, A.R., S.A.R.S. and S.R.; data curation, S.A.R.S., H.A., M.A. and S.R.; writing—original draft preparation, A.R., S.A.R.S.; writing—review and editing, H.A., M.A. and S.R.; visualization, H.A., M.A. and S.R.; supervision, S.A.R.S., H.A., M.A. and S.R.; project administration, S.A.R.S. and H.A.; funding acquisition, H.A., M.A. and S.R. All authors have read and agreed to the published version of the manuscript.

Funding

This research has received no external funding.

Data Availability Statement

Some or all data will be available upon request from the corresponding author.

Conflicts of Interest

The authors declare that there is no conflict of interest.

Appendix A

Table A1. Constructed experimental database (GS = GFRP spirals, GH = GFRP hoops, SS = steel spirals, SH = steel hoops, N = no lateral reinforcement).
Table A1. Constructed experimental database (GS = GFRP spirals, GH = GFRP hoops, SS = steel spirals, SH = steel hoops, N = no lateral reinforcement).
Sr. No.Research Study B H D f c f u E f ε u Longitudinal ReinforcementTransverse ReinforcementAxial Strength
(mm)(mm)(mm)(MPa)(MPa)(GPa)(%)Bars ρ l (%)Type ρ t (%)(kN)
1Afifi et al. [23]--3002093455.41.568 No. 52.2GS12920
2Afifi et al. [23]--3002093455.41.564 No. 51.1GS12826
3Afifi et al. [23]--3002093455.41.5612 No. 53.2GS12998
4Afifi et al. [23]--3002093455.41.568 No. 52.2GS0.452857
5Afifi et al. [23]--3002093455.41.568 No. 52.2GS1.873019
6Afifi et al. [23]--3002093455.41.568 No. 52.2GS2.072964
7Afifi et al. [23]--3002093455.41.568 No. 52.2GS0.692804
8Afifi et al. [23]--3002093455.41.568 No. 52.2GS1.032951
9Afifi et al. [23]--3002093455.41.568 No. 52.2GS1.032865
10Afifi et al. [33]--3012193455.41.568 No. 52.2GS1.52840
11Afifi et al. [33]--3022293455.41.568 No. 52.2GS1.52871
12Afifi et al. [33]--3032393455.41.568 No. 52.2GS1.52935
13AlAjarmeh et al. [67]--25031.81237602.16 No. 52.41GS1.491588
14AlAjarmeh et al. [67]--25031.81237602.16 No. 52.47GS1.561408
15AlAjarmeh et al. [67]--25031.81237602.16 No. 52.59GS1.691559
16AlAjarmeh et al. [67]--25031.81237602.16 No. 52.78GS1.921411
17AlAjarmeh et al. [68]--251251281.561.32.16 No. 41.78GS1.571035.3
18AlAjarmeh et al. [68]--252251237.460.52.16 No. 52.79GS1.571109.2
19AlAjarmeh et al. [68]--25325127060.52.16 No. 64GS1.571247.9
20AlAjarmeh et al. [68]--254251237.460.52.14 No. 51.86GS1.57983.3
21AlAjarmeh et al. [68]--255251237.460.52.18 No. 53.72GS1.571406.1
22AlAjarmeh et al. [68]--256251281.561.32.19 No. 42.67GS1.571204.2
23Alsayed et al. [69]250450-39800401.56 No. 51SH0.153285
24Alsayed et al. [69]250450-39800401.56 No. 51SH0.153285
25Alsayed et al. [69]250450-39800401.56 No. 51SH0.153285
26Alsayed et al. [69]250450-38.5800401.56 No. 51GH0.183301
27Alsayed et al. [69]250450-38.5800401.56 No. 51GH0.183301
28Alsayed et al. [69]250450-38.5800401.56 No. 51GH0.183301
29De Luca et al. [70]610610-43.760844.21.388 No. 81GH0.6315235
30De Luca et al. [70]610610-40.671244.41.68 No 81GH0.6312949
31De Luca et al. [70]610610-36.160844.21.388 No. 81GH2.511926
32De Luca et al. [70]610610-32.871244.41.68 No 81GH2.510751
33Dong et al. [15]--21540930591.63 No. 30.55GS0.941018
34Dong et al. [15]--21540930591.64 No. 30.73GS0.941179
35Dong et al. [15]--21540930591.65 No. 30.92GS0.941288
36Dong et al. [15]--21540930591.66 No. 31.1GS0.941381
37Dong et al. [15]--21540930591.64 No. 30.73GS2.751459
38Dong et al. [15]--21540930591.64 No. 30.73GS2.751037
39Dong et al. [15]--21540880591.64 No. 30.73GS2.75523
40Dong et al. [15]--21537880591.64 No. 30.73GS2.75318
41Dong et al. [15]--21537880591.65 No. 30.73GS1.391290
42Dong et al. [15]--21537880591.66 No. 30.73GS1.39944
43Dong et al. [15]--21537880591.67 No. 30.73GS1.39527
44Dong et al. [15]--21537880591.68 No. 30.73GS1.39296
45Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH0.51367
46Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH0.5880
47Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH0.5584
48Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH11449
49Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH1917
50Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH1788
51Elchalakani and Ma [26]160260-32.81200502.46 No. 41.8GH0.31402
52Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.31402
53Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.51367
54Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH11449
55Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.5880
56Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH1917
57Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH1788
58Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.5584
59Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.31041
60Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.51194
61Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH11357
62Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH0.5657
63Elchalakani et al. [29]160260-32.8930591.76 No. 41.8GH1804
64Elchalakani et al. [29]160160-32.8930591.76 No. 41.8GH0.5353
65Elchalakani et al. [29]160160-32.8930591.76 No. 41.8GH1454
66Elchalakani et al. [29]160160-32.8930591.76 No. 41.8GH0.5234
67Elchalakani et al. [29]160160-32.8930591.76 No. 41.8GH1244
68Guerin et al. [71]405405-25.3600401.56 No. 61GH0.664587
69Guerin et al. [71]405405-25.3600401.56 No. 61GH0.663433
70Guerin et al. [71]405405-25.3600401.56 No. 61GH0.661591
71Guerin et al. [71]405405-25.3600401.56 No. 61GH0.66645
72Guerin et al. [71]405405-25.3600401.56 No. 61GH0.664616
73Guerin et al. [71]405405-25.3600401.56 No. 61GH0.663405
74Guerin et al. [71]405405-25.3600401.56 No. 61GH0.661576
75Guerin et al. [71]405405-25.3600401.56 No. 61GH0.66636
76Guerin et al. [72]405405-25.3600401.58 No. 61.4GH0.845028
77Guerin et al. [72]405405-25.3600401.58 No. 61.4GH0.843627
78Guerin et al. [72]405405-25.3600401.58 No. 61.4GH0.842035
79Guerin et al. [72]405405-25.3600401.58 No. 61.4GH0.84914
80Guerin et al. [72]405405-25.3600401.58 No. 82.5GH0.635294
81Guerin et al. [72]405405-25.3600401.58 No. 82.5GH0.633790
82Guerin et al. [72]405405-25.3600401.58 No. 82.5GH0.632110
83Guerin et al. [72]405405-25.3600401.58 No. 82.5GH0.631008
84Hadhood et al. [52]--3053516801411.198 No. 52.2GH2.682564
85Hadhood et al. [52]--3053516801411.198 No. 52.2GH2.682060
86Hadhood et al. [52]--3053516801411.198 No. 52.2GH2.681511
87Hadhood et al. [52]--3053516801411.198 No. 52.2GH2.68776
88Hadhood et al. [52]--3053516801411.198 No. 52.2GH2.68366
89Hadhood et al. [52]--3053516801411.198 No. 52.2GS12608
90Hadhood et al. [52]--3053516801411.198 No. 52.2GS12134
91Hadhood et al. [52]--3053516801411.198 No. 52.2GS11513
92Hadhood et al. [52]--3053516801411.198 No. 52.2GS1745
93Hadhood et al. [52]--3053516801411.198 No. 52.2GS1654
94Hadhood et al. [52]--3053516801411.1912 No. 53.3GS12670
95Hadhood et al. [52]--3053516801411.1912 No. 53.3GS12123
96Hadhood et al. [52]--3053516801411.1912 No. 53.3GS11527
97Hadhood et al. [52]--3053516801411.1912 No. 53.3GS1852
98Hadhood et al. [52]--3053516801411.1912 No. 53.3GS1378
99Hadhood et al. [73]--3053516801411.198 No. 52.2GS1.82652
100Hadhood et al. [73]--3053516801411.198 No. 52.2GS1.82086
101Hadhood et al. [73]--3053516801411.198 No. 52.2GS1.81483
102Hadhood et al. [73]--3053516801411.198 No. 52.2GS1.8747
103Hadhood et al. [73]--3053516801411.198 No. 52.2GS1.8655
104Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.14709
105Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.13309
106Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.12380
107Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.11112
108Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.1797
109Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GH1.14689
110Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GH1.13299
111Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GH1.12435
112Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GH1.11054
113Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GH1.1838
114Hadhood et al. [73]--30570.2128954.92.312 No. 53.2GS1.14716
115Hadhood et al. [73]--30570.2128954.92.312 No. 53.2GS1.13380
116Hadhood et al. [73]--30570.2128954.92.312 No. 53.2GS1.12339
117Hadhood et al. [73]--30570.2128954.92.312 No. 53.2GS1.11135
118Hadhood et al. [73]--30570.2128954.92.312 No. 53.2GS1.1713
119Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.15120
120Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.13671
121Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.12538
122Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.11392
123Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.1611
124Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.74680
125Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.73341
126Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.72460
127Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.71061
128Hadhood et al. [73]--30570.2128954.92.38 No. 52.2GS1.7682
129Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.12608
130Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.12134
131Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.11512
132Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1745
133Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1354
134Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.13090
135Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.12342
136Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.11746
137Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1995
138Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1529
139Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.12652
140Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.12086
141Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.11483
142Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1747
143Hadhood et al. [73]--30535128954.92.38 No. 52.2GS1.1355
144Hadi et al. [34]--205371200502.46 No. 41.6GS2.11220
145Hadi et al. [34]--205371200502.46 No. 41.6GS2.1781
146Hadi et al. [34]--205371200502.46 No. 41.6GS2.1494
147Hadi et al. [34]--205371200502.46 No. 41.6GS4.21309
148Hadi et al. [34]--205371200502.46 No. 41.6GS4.2767
149Hadi et al. [34]--205371200502.46 No. 41.6GS4.2479
150Hadi and Youssef [74]210210-29.3164167.92.414 No. 41GH2.741285
151Hadi and Youssef [74]210210-29.3164167.92.414 No. 41GH2.74803
152Hadi and Youssef [74]210210-29.3164167.92.414 No. 41GH2.74615
153Hassan et al. [75]--15040800300.976 No. 32.1SS1.7426.59
154Hassan et al. [75]--15040800301.356 No. 32.1SS1.7411.88
155Hassan et al. [75]--15040800301.576 No. 32.1SS1.7387.36
156Hassan et al. [75]--15040800301.46 No. 32.1SS3.4529.56
157Hassan et al. [75]--15040800301.76 No. 32.1SS3.4490.33
158Hassan et al. [75]--15040800301.96 No. 32.1SS3.4460.91
159Hassan et al. [75]--15040800301.286 No. 32.1GH1.7490.33
160Hassan et al. [75]--15040800301.56 No. 32.1GH1.7460.91
161Hassan et al. [75]--15040800301.76 No. 32.1GH1.7430.4
162Karim et al. [35]--205371600662.426 No. 44.72GS1.911425
163Karim et al. [35]--205371600662.426 No. 44.72GS3.822041
164Karim et al. [52]--206371600662.426 No. 44.72GS1.911425
165Karim et al. [52]--207371600662.426 No. 44.72GS1.91781
166Karim et al. [52]--208371600662.426 No. 44.72GS1.91494
167Karim et al. [52]--209371600662.426 No. 44.72GS3.822041
168Karim et al. [52]--210371600662.426 No. 44.72GS3.82767
169Karim et al. [52]--211371600662.426 No. 44.72GS3.82479
170Karim et al. [52]--212371600662.426 No. 44.72GS1.913068
171Karim et al. [52]--213371600662.426 No. 44.72GS1.911450
172Karim et al. [52]--214371600662.426 No. 44.72GS1.91805
173Khan et al. [47]--206371395561.56 No. 53.57GH-2812
174Khan et al. [47]--206371395561.56 No. 53.57GH-1487
175Khan et al. [47]--206371395561.56 No. 53.57GH-910
176Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-775
177Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-775
178Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-693
179Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-693
180Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-693
181Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-578
182Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-578
183Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-354
184Khorramian & Sadeghian [27]150150-3762938.71.626 No. 55.3N-354
185Maranan et al. [76]--25034.42118462.61.896 No. 52.43GH3.131772
186Maranan et al. [76]--25034.42118462.61.896 No. 52.43GH3.131791
187Maranan et al. [76]--25034.42118462.61.896 No. 52.43GH1.571981
188Maranan et al. [76]--25034.42118462.61.896 No. 52.43GH0.781988
189Maranan et al. [76]--25034.42118462.61.896 No. 52.43GS3.131838
190Maranan et al. [76]--25034.42118462.61.896 No. 52.43GS1.572063
191Maranan et al. [76]--25034.42118462.61.896 No. 52.43GH1.571624
192Maranan et al. [76]--25034.42118462.61.896 No. 52.43GS1.571208
193Mohamed et al. [32]--30042.993455.41.568 No. 52.2GH2.232840
194Mohamed et al. [32]--30042.993455.41.568 No. 52.2GH2.682871
195Mohamed et al. [32]--30042.993455.41.568 No. 52.2GH3.142935
196Pantelides et al. [49]--2543674043.31.714 No. 51.6GS0.751975
197Pantelides et al. [49]--2543674043.31.714 No. 51.6GS0.751788
198Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.01370
199Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.01370
200Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.01370
201Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.02365
202Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.02365
203Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SS0.02365
204Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.01345
205Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.01345
206Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.01345
207Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.02315
208Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.02315
209Prachasaree et al. [77]--15020.8735501.54 No. 31.9SS0.02315
210Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SH0.01365
211Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SH0.01365
212Prachasaree et al. [77]150150-20.8735501.54 No. 31.4SH0.01365
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Figure 1. Flow chart of the present work.
Figure 1. Flow chart of the present work.
Polymers 13 01265 g001
Figure 2. Performance of previous models (a) ACI 318-08 (b) ACI 318-11 (c) CSA S806-02 (d) CSA S806-12 (e) AS 3600-18 (f) Afifi et al. [23] (g) Mohamed et al. [32] (h) Tobbi et al. [48] (i) Samani and Attard [46] (j) Hadhood et al. [52] (k) Khan et al. [47] (l) Mohamed et al. [32] (m) Pantelides et al. [49].
Figure 2. Performance of previous models (a) ACI 318-08 (b) ACI 318-11 (c) CSA S806-02 (d) CSA S806-12 (e) AS 3600-18 (f) Afifi et al. [23] (g) Mohamed et al. [32] (h) Tobbi et al. [48] (i) Samani and Attard [46] (j) Hadhood et al. [52] (k) Khan et al. [47] (l) Mohamed et al. [32] (m) Pantelides et al. [49].
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Figure 3. Performance of the suggested model.
Figure 3. Performance of the suggested model.
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Figure 4. Distribution of AS of fiber-reinforced polymers (FRP)-reinforced columns attained from various models.
Figure 4. Distribution of AS of fiber-reinforced polymers (FRP)-reinforced columns attained from various models.
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Figure 5. Normal distribution of testing to estimated strengths of GFRP-reinforced columns attained from various models.
Figure 5. Normal distribution of testing to estimated strengths of GFRP-reinforced columns attained from various models.
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Figure 6. Finite element simulations of (a) geometry (b) interactions (c) support conditions (d) meshing of GFRP-RC specimens.
Figure 6. Finite element simulations of (a) geometry (b) interactions (c) support conditions (d) meshing of GFRP-RC specimens.
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Figure 7. (a) Stress–strain relationship for concrete structures. (b) Tension stiffening model for concrete.
Figure 7. (a) Stress–strain relationship for concrete structures. (b) Tension stiffening model for concrete.
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Figure 8. (a) Linear elastic performance of GFRP ties. (b) Linear elastic performance of GFRP longitudinal bars.
Figure 8. (a) Linear elastic performance of GFRP ties. (b) Linear elastic performance of GFRP longitudinal bars.
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Figure 9. Sensitivity of various element types on load-deflection behavior of control specimen (a) concrete elements (b) FRP bars elements.
Figure 9. Sensitivity of various element types on load-deflection behavior of control specimen (a) concrete elements (b) FRP bars elements.
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Figure 10. Sensitivity analysis of (a) mesh size (b) dilation angle (c) viscosity parameter (d) shape factor of concrete on the load-deflection curve of the control specimen.
Figure 10. Sensitivity analysis of (a) mesh size (b) dilation angle (c) viscosity parameter (d) shape factor of concrete on the load-deflection curve of the control specimen.
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Figure 11. Load-deflection performance of GFRP-RC concentric columns.
Figure 11. Load-deflection performance of GFRP-RC concentric columns.
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Figure 12. Load-deflection performance of GFRP-RC eccentric columns (a) G75-25 (b) G75-35 (c) G150-25 (d) G150-45.
Figure 12. Load-deflection performance of GFRP-RC eccentric columns (a) G75-25 (b) G75-35 (c) G150-25 (d) G150-45.
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Figure 13. Detailed parametric investigation using FEM.
Figure 13. Detailed parametric investigation using FEM.
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Figure 14. Parametric investigation using an empirical model.
Figure 14. Parametric investigation using an empirical model.
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Figure 15. Comparison of predictions of anticipated empirical and FEM.
Figure 15. Comparison of predictions of anticipated empirical and FEM.
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Table 1. Statistical details of different parameters of database.
Table 1. Statistical details of different parameters of database.
ParameterB (mm)H (mm) f c (MPa)D (mm)Ag (mm2) f u   ( MPa ) E f   ( GPa ) ε u (%) ρ l (%) Af (mm2) ρ t (%) P n   ( kN )
MIN15015020.01501766240623.40.970.55212.530.01114
MAX61061070.230537210016801412.425.34051.605.315235
Mean24927236.225866289101056.71.782.091214.581.381814
*SD11411412.6545303933925.10.391.06764.621.061877
**COV0.460.430.350.210.810.340.450.220.510.630.771.04
* Standard deviation, ** coefficient of variation.
Table 2. Axial strength (AS) models for assessment.
Table 2. Axial strength (AS) models for assessment.
Code/ResearchProposed Model
ACI-318-08 [44] P n = 0.85 f c ( A g A s ) + f y A s
CSA S806-02 [45] P n = 0.85 f c ( A g A F R P )
CSA S806-12 [11] P n = α 1 f c ( A g A F R P ) ;   α 1 = 0.85 0.0015 f c 0.67
Afifi et al. [23] P n = 0.85 f c ( A g A F R P ) + α g f F R P A F R P ; α g = 0.35
Samani and Attard [46] P n = 0.85 f c ( A g A F R P ) + 0.0025 E F R P A F R P
Khan et al. [47] P n = 0.85 f c c ( A g A G F R P ) + α f G F R P A G F R P ; α = 0.61
Tobbi et al. [48] P n = 0.85 f c ( A g A F R P ) + ε c o E F R P A F R P ;   ε c o = 0.003
Pantelides et al. [49] P n = 0.85 f c c F R P A c + A F R P ε c F R P E F R P ;   ε c F R P = 0.003
ACI 318-11 [50] P n = 0.85 f c ( A g A s )
AS-3600:2018 [51] P n = 0.85 f c ( A g A F R P ) + 0.0025 E F R P A F R P
Mohamed et al. [32] P n = 0.90 f c ( A g A F R P ) + ε f g E F R P A F R P ; ε f g = 0.002
Hadhood et al. [52] P n = α 1 f c ( A g A F R P ) + 0.0035 E F R P A F R P ;
α 1 = 0.85 0.0015 f c
Mohamed et al. [32] P n = 0.85 f c ( A g A F R P ) + ε p E F R P A F R P ; ε p = 0.002
Table 3. Specimens for numerical simulations.
Table 3. Specimens for numerical simulations.
Sample LabelLongitudinal ReinforcementTransverse ReinforcementEccentricity (mm)
GFRP BarsReinforcing Ratio (%)
G150-456-ɸ12.7 mm1.836.35 mm @ 150 mm c/c45
G150-256-ɸ12.7 mm1.836.35 mm @ 150 mm c/c25
G150-C6-ɸ12.7 mm1.836.35 mm @ 150 mm c/c0
G75-356-ɸ12.7 mm1.836.35 mm @ 75 mm c/c35
G75-256-ɸ12.7 mm1.836.35 mm @ 75 mm c/c25
G75-C6-ɸ12.7 mm1.836.35 mm @ 75 mm c/c0
G250-C6-ɸ12.7 mm1.836.35 mm @ 250 mm c/c0
Table 4. Testing and numerical simulation results.
Table 4. Testing and numerical simulation results.
Sample LabelExperimental ResultsFEA Results from ABAQUS % Difference in Peak Loads (KN)% Difference in Vertical Def. at Peak Load (mm)
Peak Load (KN)Vertical Deformation at Peak Load (mm)Peak Load (KN)Vertical Deformation at Peak Load (mm)
G150-45584.215.67547.815.126.239.70
G150-25880.284.86883.945.360.4110.28
G150-C1366.766.871384.098.071.2617.46
G75-35787.806.13694.515.0611.8417.45
G75-25917.167.30895.685.742.3421.36
G75-C1449.066.391486.267.282.5613.92
G250-C1401.85.791426.917.011.7921.07
Table 5. Ranges of the parameters during the parametric investigation.
Table 5. Ranges of the parameters during the parametric investigation.
VariableFixed ValueStudied Values
Concrete strength (MPa)3010, 15, 20, 25, 30, 35, 40, 45, 50, 55
Tensile strength (MPa)850700, 750, 800, 850, 900, 950, 1000, 1050, 1100, 1150
Side length of column (mm)200150, 175, 200, 225, 250, 275, 300, 325, 350, 375
Reinforcement ratio (%)1.940.97, 1.46, 1.94, 2.43, 2.92, 3.41, 3.89, 4.38, 4.86, 5.35
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Raza, A.; Shah, S.A.R.; Alhazmi, H.; Abrar, M.; Razzaq, S. Strength Profile Pattern of FRP-Reinforced Concrete Structures: A Performance Analysis through Finite Element Analysis and Empirical Modeling Technique. Polymers 2021, 13, 1265. https://doi.org/10.3390/polym13081265

AMA Style

Raza A, Shah SAR, Alhazmi H, Abrar M, Razzaq S. Strength Profile Pattern of FRP-Reinforced Concrete Structures: A Performance Analysis through Finite Element Analysis and Empirical Modeling Technique. Polymers. 2021; 13(8):1265. https://doi.org/10.3390/polym13081265

Chicago/Turabian Style

Raza, Ali, Syyed Adnan Raheel Shah, Hatem Alhazmi, Muhammad Abrar, and Samia Razzaq. 2021. "Strength Profile Pattern of FRP-Reinforced Concrete Structures: A Performance Analysis through Finite Element Analysis and Empirical Modeling Technique" Polymers 13, no. 8: 1265. https://doi.org/10.3390/polym13081265

APA Style

Raza, A., Shah, S. A. R., Alhazmi, H., Abrar, M., & Razzaq, S. (2021). Strength Profile Pattern of FRP-Reinforced Concrete Structures: A Performance Analysis through Finite Element Analysis and Empirical Modeling Technique. Polymers, 13(8), 1265. https://doi.org/10.3390/polym13081265

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