Abstract
In this study, nonlinear finite element analyses of reinforced concrete interior slab-column connections were performed to investigate their punching shear behavior under gravity and lateral loads without shear reinforcement. A numerical model based on the concrete damaged plasticity (CDP) model in ABAQUS was developed with suitable constitutive models for concrete and reinforcements using eight-node brick elements with reduced integration and three-dimensional truss elements, respectively. The model was calibrated in comparison with the test results of an interior slab-column connection without shear reinforcement. Moreover, the validity of the calibrated model was verified using other test results. Then, a parametric study was conducted to examine the influence of different design variables on the unbalanced moment and deformation capacity of slab-column connections. Finally, based on the existing experimental data and finite element analysis results obtained in this work, formulas for calculating the ultimate unbalanced moment and drift ratio were proposed using the nonlinear fitting method. The proposed formulas were compared with the existing methods provided by other national codes and researchers, verifying the rationality of the proposed formulas.
Keywords
Introduction
The problem of punching shear failure occurs in flat slab-column connections that are not typically reinforced with shear reinforcement. Many researchers have studied the punching shear behavior of slab-column connections without shear reinforcement (Drakatos et al., 2016; Inácio et al., 2020; Pan and Moehle, 1989; Robertson and Johnson, 2006). However, there is no agreement on the punching shear failure mechanism. Therefore, this work aims to conduct further research on the failure mechanism and mechanic behavior of slab-column connections without shear reinforcement.
Existing experimental results show that the main factors affecting the punching failure of slab-column connections are the gravity load level and flexural reinforcement ratio. The gravity load level is usually represented using the gravity shear ratio Vg/Vc, where Vg is the shear force acting on a critical perimeter due to the gravity load and Vc is the punching shear capacity of concrete calculated according to ACI318-19 (2019). Pan and Moehle (1989) tested two isolated slab-column connections with gravity shear ratios of 0.18 and 0.37. Moreover, Robertson and Durrani (1992) and Robertson and Johnson (2006) reported three single-story structures with two-span slab-column frames and three isolated slab-column connections with gravity shear ratios ranging from 0.18 to 0.54. Tang et al. (2019) reported four isolated slab-column connections with gravity shear ratios ranging from 0.39 to 0.72. The above test results showed that increasing the gravity shear ratio reduces the unbalanced moment capacity, deformation capacity, and lateral stiffness of slab-column connections. Pan and Moehle (1989) believed that the gravity shear ratio must not exceed 0.4 to ensure a connection drift capacity of 1.5%, while Robertson and Durrani (1992) suggested that the value of 0.4 should be reduced to 0.35. Generally, increasing the slab flexural reinforcement ratio could improve the unbalanced moment capacity and lateral stiffness of slab-column connections but reduce the lateral deformation capacity. This trend was confirmed by the test results presented by Choi et al. (2007), Ghali et al. (1976), and Robertson and Johnson (2006), wherein the gravity shear ratios were between 0.23 and 0.30. However, Drakatos et al. (2016) found that when the gravity shear ratio was approximately 0.6, increasing the slab longitudinal reinforcement ratio had little effect on the unbalanced moment capacity of slab-column connections that experienced punching shear failure, which was consistent with the test results of the specimens that experienced flexural failure with low gravity shear ratios of less than 0.05 (Morrison et al., 1983). When the gravity shear ratio was approximately 0.9, the specimens with reinforcement ratios of 0.8% and 1.6% showed little difference in terms of lateral deformation ability. Drakatos et al. (2016) and Morrison et al. (1983) showed inconsistent test results based on specimens with moderate gravity shear ratios ranging from 0.23 to 0.30 for plate slabs of 114–152 mm. These discrepancies may arise from the fact that Morrison et al. (1983) used low gravity shear ratios of less than 0.05 in the case of thin plate slabs of 76 mm, whereas Drakatos et al. (2016) used high gravity shear ratios of more than 0.59 in the case of thick plate slabs of 250 mm. Furthermore, the test results of Tang et al. (2019) showed that at a gravity shear ratio of 0.39, increasing the reinforcement ratio could not only improve the unbalanced moment capacity and lateral stiffness but also enhance the lateral deformation capacity of slab-column connections. Moreover, Inácio et al. (2020) found that the lateral deformation capacity of slab-column connections could be significantly improved using high-strength concrete in local areas of connections.
Several mechanical models have been proposed by Choi et al. (2014a, 2014b), Deifalla (2020a, 2020b, 2021a, 2021b), Fan et al. (2021), Kinnunen and Nylander (1960), Muttoni (2008), Park and Islam (1976), Stasio and Buren (1960), and others, in addition to extensive experimental research on punching shear behavior. Some of them served as the foundation for the design formulas used in code provisions.
With the development of computers and computing technologies, the nonlinear finite element method has become a powerful tool for studying the performance of concrete structures. Many existing studies have been conducted on the finite element analysis (FEA) of the mechanical performance of slab-column connections under gravity loads (Bompa and Elghazouli, 2017; Eder et al., 2010; Lapi et al., 2020; Navarro et al., 2018; Shu et al., 2016; Vidosa et al., 1988; Wörle, 2014; Xiao and Chin 2007). However, there are relatively few studies on mechanical performance analyses under combined gravity and horizontal loads. Polak (2005) utilized three-dimensional (3D) layer shell elements to study the punching shear transfer mechanisms of slabs and discussed the influence of material parameters (cracked shear modulus of concrete, tension stiffening factors, and dowel action coefficients) on the numerical results. Guan (2009) also used layer shell elements to simulate the punching shear performance, and the focus of this research was to examine the impacts of the openings and column aspect ratio on slab-edge column connections. The failure criteria for the shell modeling approaches used by Polak (2005) and Guan (2009) are tension cracking or concrete crushing. Genikomsou and Polak (2015) established a 3D model with brick elements using the ABAQUS software, and the parameters were calibrated using the test results. Additionally, the rationality of the FEA model was verified by comparing the numerical results with the test results in terms of the load–deformation curve and cracking pattern. Setiawan et al. (2019) used a 3D nonlinear finite element analysis (NLFEA) using the software ATENA to investigate the effect of the cyclic degradation mechanism on the unbalanced moment capacity, lateral stiffness, and lateral deformation capacity of slab-column connections under lateral cyclic loading.
The existing experimental studies show that the gravity shear ratio, reinforcement ratio, and concrete strength have a great influence on the mechanical performance of slab-column connections without shear reinforcement under the combination of gravity and horizontal loads. In most concrete structure design codes, simplified empirical formulas are used to calculate the shear stress on the critical section of slab-column connections (ACI318-19, 2019; EC2-04, 2004). However, there are not enough experimental data and numerical analysis results for fully supporting the design calculation method. Therefore, the nonlinear FEA method was adopted in this work to study the strength and deformation performance of slab-column connections under the combination of gravity and horizontal loads and provide a reference for revising relevant codes. First, the model parameters were calibrated based on the specimen (RC1) tested by Tang et al. (2019), and the rationality of the calibrated model was further verified by other specimens (RC2, RC3, and RC4) tested by Tang et al. (2019) and (L0.5, G0.5, and G1.0), which were tested by Tian et al. (2008). Then, a parameter analysis was completed based on the calibrated model. The influence of the gravity shear ratio, reinforcement ratio, and concrete strength on the punching shear performance of the slab-column connections was studied. Finally, based on the experimental and FEA results, formulas for calculating the ultimate unbalanced moment and ultimate drift ratio were proposed, and the rationality of the proposed formulas was verified by comparing them with the existing standard calculation methods and the formulas proposed by other scholars.
Finite element model
Description of the finite element model
The FEA software ABAQUS was used for analysis in this article. Eight-node three-dimensional brick elements with reduced integration (C3D8R) were used to model the concrete, while the reinforcement was modeled using two-node three-dimensional truss elements (T3D2). The rebars were embedded into the concrete, so a perfect bond was assumed between the rebars and the concrete. According to the mesh sensitivity study of Deng (2018), six brick elements were used through the depth of the 150-mm slab. To save computational effort, a refined mesh size of 25 mm × 25 mm × 25 mm was used for the concrete in the slab width (c + 3h) centered on the column, while the mesh size of 25 mm × 50 mm × 50 mm was used for the remaining concrete. Here, c is the column size and h is the slab thickness. Further, a mesh size of 50 mm was used for all the rebars. The geometry and boundary conditions of the specimen (RC1), which were used for calibration, are presented in Figure 1. A reference point (RP) was established at the center of each support surface. A coupling constraint was adopted to couple the motion of a collection of nodes on the support surface to the motion of the RP. It was assumed that the column remained elastic to provide a simple approach, which was also used by other researchers (Genikomsou and Polak, 2016; Liu et al., 2015). The concrete damaged plasticity (CDP) model in ABAQUS was adopted to model the concrete behavior. The CDP model is suitable for concrete members under low confining pressure. Considering the damage effect, it is more suitable for simulating the crack development, crack closure, and stiffness recovery of concrete structures under cyclic loading (Hibbitt et al., 1998). Geometry and boundary conditions of the model.
Main parameters
The CDP model has five main parameters, which are the dilation angle (ψ), eccentricity (ε), yield stress ratio (σb0/σc0), yield surface shape factor (K c ), and viscosity parameter (μ). Some of their default values are usually assumed. The eccentricity was considered to be 0.1, the yield stress ratio was assumed to be 1.16, and the yield surface shape factor was assumed to be 0.667.
The stress–strain relationship of the concrete under uniaxial compression was represented based on Hognestad parabola (Genikomsou and Polak, 2015), which can be subdivided into three parts (Figure 2). The first part O-A represents the linear elastic branch, assumed until Compressive stress–strain relationship for concrete.
The uniaxial tensile stress–strain behavior of concrete was considered linear elastic until the peak tensile stress,
After cracking, an exponential tension-softening branch, which was proposed by Hordijk (1991), was selected for the tensile stress–crack width relationship to reduce the mesh sensitivity of the numerical results (Figure 3). (a) Tensile stress–crack width relationship and (b) tensile stress–strain relationship for concrete.
Two damage variables (d
c
and d
t
) were used for the concrete under compression and tension, respectively. Under compression, the damage was introduced after reaching the assumed elastic limit (σ
cA
), as shown in Figure 2, and the tensile damage occurred when the tensile strength
Meanwhile, the steel reinforcement stress–strain relationship was assumed to be elastically perfectly plastic, with the elastic modulus equal to 200,000 MPa according to ACI318-19. The Poisson’s ratio for reinforcement was usually set to 0.3 (Genikomsou and Polak, 2015; Laguta, 2020; Milligan, 2018).
Description of the test specimens
The test parameters and results of the specimens.
V + C refers to applying the gravity load and horizontal cyclic load and V refers to only applying the gravity load.
f y is the yield strength of flexural reinforcement and ρ is the reinforcement ratio within a slab width of (c + 3h) centered on the column. P refers to the punching shear failure.
The punching shear failure occurred in all specimens, with e/c values less than 2.6 (Table 1). Here, e is the eccentricity equal to M u /V g , M u is the ultimate unbalanced moment, and c is the column size. The following sections present information on the comparison analysis between test and simulation results.
Finite element analysis
Parameter calibration of the finite element model
The test results of RC1 were used to calibrate the parameters of the FEA model. It was assumed that the envelope (skeleton curve) of the hysteretic curve for the specimen is the same as the monotonic loading curve. In other words, the influence of the cyclic loads on the skeleton curve was ignored. In this study, the displacement-controlled mode was used to apply a horizontal monotonic load during the simulation test. According to the loading rate of conventional seismic tests, such tests could be regarded as quasistatic problems. The implicit (ABAQUS/Standard) algorithm was used to solve the model. The numerical integration was performed using the Newton–Raphson method. Under the premise of no obvious loss of calculation accuracy and efficiency, the convergence rate of the model in the softening segment could be improved by taking a smaller value of the viscosity parameter. In this article, the viscosity coefficient was set as 0.00001, which is consistent with the research results of Genikomsou and Polak (2015) and Navarro et al. (2018). The analysis showed that when the slab thickness to element size ratio is greater than or equal to six, the numerical simulation accuracy of the punching failure is good and does not change significantly with the refined mesh size (Deng 2018). To determine the refined mesh size in this study, it was reasonable to use the ratio of the slab thickness to the element size to be equal to six (i.e., six layers of elements were divided along the thickness of the slab).
The concrete volume change due to the inelastic strains is called dilatancy, and it could be modeled by adopting the dilation angle in the CDP model. According to Genikomsou and Polak (2015), the dilation angle (ψ) should range from 31° to 42°. In the calibration process, four different values of the dilation angle (i.e., ψ = 20°, 30°, 38°, and 42°) were examined (see Figure 4(a)). In the figure, the unbalanced moment was determined from the measured lateral load and effective column height (Hc) and the drift ratio was defined as the ratio of the column top displacement to the effective column height. Figure 4(a) shows that a dilation angle of 38° provided better prediction results in terms of the ultimate unbalanced moment and drift ratio. Lapi et al. (2020) summarized the dilation angle used in the existing FEA and found that it ranged from 35° to 40°, so the value of the dilation angle in this article is also consistent with the statistical results. Therefore, the dilation angle was selected as 38° for all the subsequent specimens. Unbalanced moment–drift ratio response of RC1: (a) for different dilation angle values and (b) for different fracture energy values.
The fracture energy of concrete is defined as the energy required to produce a tensile crack per unit area (Figure 3). According to Equations (5)–(7), the fracture energy can be associated with the concrete strength. Three different values derived from Equations (5)–(7) were investigated, and it could be seen that the influence of the concrete tensile behavior on the slab response is notable (Figure 4(b)). The results obtained from either Equation (5) or (6) present an underestimation or overestimation of the ultimate unbalanced moment. However, the most accurate results could be acquired using Equation (7). Thus, Equation (7) was considered to determine the fracture energy values for all the simulated specimens.
According to the above-calibrated results, the static analysis method was adopted. The viscosity coefficient, refined mesh size, and dilation angle were 0.00001, 25 mm, and 38°, respectively. The fracture energy was determined according to Equation (7). Finally, the simulated unbalanced moment–drift ratio response was obtained and then compared with the test results. The results show that the simulation response of the connection under monotonic loading is in good agreement with the skeleton curve of the tested hysteresis response for the positive horizontal loading displacement (Figure 5). The FEA overestimated the specimen’s stiffness possibly because the adopted concrete model did not realistically simulate the punching shear behavior owing to its complexity. The test and simulation response of the unbalanced moment–drift ratio for RC1.
The CDP model assumes that when the maximum principal plastic strain is positive, the concrete cracks and crack direction are perpendicular to the maximum principal plastic strain direction (Genikomsou and Polak, 2015). Therefore, the maximum plastic principal strain (PE, max. Principal) can be used to approximate the failure mode of the slab-column connections. In the event of failure, Figure 6 depicts the tested cracks as well as the maximum principal plastic strain contour plots of the specimen RC1. By comparing of the test and FEA results in Figure 6, it could be seen that the maximum principal plastic strain calculated based on ABAQUS could well simulate the cracking pattern of the slab-column connections. Crack patterns of specimen RC1: (a) top slab and (b) cross section.
Verification of the calibrated finite element model
The calibrated FEA model was further verified using the specimens RC2, RC3, and RC4 in the study by Tang et al. (2019) and the specimens L0.5, G0.5, and G1.0 in the study by Tian et al. (2008). For the specimens RC2, RC3, RC4, and L0.5, which were subjected to gravity and lateral loads, the ultimate unbalanced moment–drift ratio responses obtained using the FEA simulation were in good agreement with the test results (Figures 7(a)–(d)). For the specimens G0.5 and G1.0, which were subjected to vertical loads, the vertical load-deflection responses obtained using simulations showed good agreement with the experimental results (Figures 7(e) and (f)). According to Table 2, the maximum relative error between FEA and test results was within 15% in all specimens, which is an acceptable difference. Figure 8 shows a comparison of the tested crack patterns and the maximum principal plastic strain contour plots of all the specimens at failure. The main characteristics of tested cracks at failure, which are concentrated near the column and developed to the slab boundaries, can be captured realistically using NLFEA. The simulations all showed brittle punching shear failure, similar to the test. The slab top reinforcements passing through the column reached the yield strain under the vertical load in the case of simulated specimen RC2 in Figure 8(a). When the horizontal load was applied, the slab bars near the column gradually yielded, whereas the other slab bars far away from the column remained elastic. When the peak load was reached, the slab concrete near the column could no longer support the horizontal load due to the large tensile strain and the connection failed because of brittle punching failure. This is consistent with the experimental results. For the slab top reinforcements passing through the column under a vertical load, a strain of nearly half of the yield strain was achieved for simulated specimen L0.5 in Figure 8(d). The yielding of top bars extended to 530 mm outside the column face in the lateral loading direction when the peak lateral load was reached at 1.75%. Owing to the large plastic strain, the slab concrete around the column was severely damaged after the peak load was reached. The sudden drop of combined vertical and lateral loads revealed a brittle punching shear failure. The FEA results agreed well with the experimental results. The numerical simulations also confirmed differences in crack distribution between specimens RC2 and L0.5, which could be attributed to different reinforcement arrangements. Unbalanced moment–drift ratio response or gravity load-deflection response for specimens: (a) RC2, (b) RC3, (c) RC4, (d) L0.5, (e) G0.5, and (f) G1.0. Test and FEA results. ρ
t
is the reinforcement ratio within a slab width of (c + 3h) centered on the column, M
u
is the ultimate unbalanced moment, V
u
is the ultimate vertical load, θ
u
is the ultimate drift ratio, w
u
is the ultimate deflection, G0.5 and G1.0 are only subjected to vertical loads, and the test and FEA results are the ultimate vertical load (V
u
) and ultimate deflection (w
u
), respectively. Crack patterns at failure on the top surface of connections only under gravity loads: (a) RC2, (b) RC3, (c) RC4, (d) L0.5, (e) G0.5, and (f) G1.0.

Parametric study
A parametric study for the RC slab-column connections without shear reinforcement was conducted using the calibrated CDP model. The geometrical size and loading position of the slab-column connections were the same as those of RC1. There are three main parameters: the gravity shear ratio (V
g
/V
c
), reinforcement ratio (ρ
s
) for flexural reinforcement within a slab width of (c + 3h) centered on the column, and compressive strength of concrete slab
Figure 9 shows the ultimate unbalanced moment with varying reinforcement ratios and gravity shear ratios. The ultimate unbalanced moment of the slab-column connections decreases with an increase in the gravity shear ratio and increases with an increase in the reinforcement ratio or concrete strength. However, the increment in the ultimate unbalanced moment is minor when the reinforcement ratio is more than 1.2%. The reason is that when the reinforcement ratio reaches a certain level, the concrete strength plays a dominant role in determining the unbalanced moment capacity. In this case, increasing the reinforcement ratio has no significant effect on the unbalanced moment capacity. Figure 10 depicts the ultimate drift ratio with varying reinforcement and gravity shear ratios. The ultimate drift ratio decreases with an increase in the gravity shear ratio and increases with an increase in the concrete strength. When the gravity shear ratio is less than a threshold value (approximately 0.23), ductile flexural failure often occurs at the connections with a small reinforcement ratio. Alternatively, increasing reinforcement ratio, which leads to the brittle punching failure of the connections, reduces the lateral deformation capacity. However, if the gravity shear ratio is greater than this threshold value, there is a critical reinforcement ratio of nearly 0.8%. For low reinforcement ratios up to the critical value, increasing the reinforcement ratio reduces the cracking of slab concrete under the vertical load, which improves the lateral deformation capacity of the slab-column connections subsequently subjected to the horizontal load. Moreover, if the reinforcement ratio is greater than the critical value, the reinforcement fails to yield or yields partially before failure occurs. In this case, increasing the reinforcement ratio reduces the lateral deformation capacity of the slab-column connections. For the same gravity shear ratio, the connection with a higher concrete strength is subject to greater gravity load, but exhibits a larger unbalanced moment capacity and improved lateral deformation capacity. Curves of the ultimate unbalanced moment with the changes in the reinforcement and gravity shear ratios: (a) fc' = 32 MPa, (b) fc' = 52 MPa, (c) fc' = 72 MPa, and (d) fc' = 92 MPa. Curves of the drift ratio with the changes in the reinforcement and gravity shear ratios: (a) fc' = 32 MPa, (b) fc' = 52 MPa, (c) fc' = 72 MPa, and (d) fc' = 92 MPa.

Validation of the proposed formulas
When calculating the unbalanced moment capacity, both ACI318-19 (2019) and EC2-04 (2004) adopted the eccentric shear stress model. ACI318-19 assumed that the shear stress was linearly distributed on the critical section, while EC2-04 assumed that the shear stress was uniformly distributed on the critical half-section. Moreover, the formulas of the punching shear capacity in addition to the positions and shapes of the critical section were different. ACI318-19 considered the influence of the gravity shear ratio and provided the formula of the ultimate drift ratio, while EC2-04 did not provide the corresponding formula.
For the connections with square columns, ACI318-19 assumed that 40% of the unbalanced moments was transferred by the linear shear stress on the critical section of concrete and that the remaining 60% was transferred by the flexural reinforcement in the (c + 3h) slab width. The unbalanced moment capacity M
ACI
of the reinforced concrete slab-column connections with the square columns according to ACI318-19 can be calculated using Equation (9):
For a given shear force V
g
and moment M, the shear stress v
Ed
acting on the critical section of the slab-column connection according to EC2-04 is
The maximum permissible shear stress vRd acting on the critical section is
Herein, 81 test data and 64 FEA data of the interior slab-column connections were collected (Appendix A). Based on these test and FEA data, the effect of the gravity shear ratio on the moment ratio was investigated (Figure 11). The ordinate moment ratio is the ratio of the tested unbalanced moment to the calculated value based on ACI318-19, EC2-04, and the proposed formula. The abscissa γG,ACI is equal to Vg/Vc,ACI, where Vc,ACI is the punching shear capacity calculated using ACI318-19. The abscissa γG,EC is equal to Vg/Vc,EC, where Vc,EC is the punching shear capacity calculated using EC2-04. Notably, the moment ratio calculated using ACI318-19 did not change significantly with the gravity shear ratio but exhibited a large dispersion (Figure 11(a)). The moment ratio calculated using EC2-04 showed a small dispersion; however, the calculated results significantly deviated from the test results when the gravity shear was relatively large (Figure 11(b)). Therefore, based on EC2-04, a modified formula (14) considering the gravity shear ratio was proposed to predict the ultimate unbalanced moment with improved accuracy. Relationship between the moment ratio and gravity shear ratio based on different methods: (a) ACI318-19, (b) EC2-04, and (c) proposed formula.

When the ultimate drift ratio of the slab-column connections was determined, the corresponding lateral force resistance system could be designed. If necessary, the shear reinforcement could be provided to avoid the brittle punching failure of the slab-column connections. Considering the gravity load influence, ACI318-19 (2019), Hueste and Wight (1999) and Megally and Ghali (1994) proposed different formulas for calculating the ultimate drift ratio θu, which are expressed using Equations (17)–(19), respectively.
Figure 12 shows the relationship between the ultimate drift ratio and gravity shear ratio as well as the calculation curves of the ultimate drift ratio. In Figure 12, “Proformula” is the abbreviation of the proposed formula. It could be seen from the figure that the ultimate drift ratio generally showed a decreasing trend with the increase in the gravity shear ratio. The ACI318-19 formula roughly gave the lower limit of the ultimate drift ratio, but there were some overestimated data. The calculation formula proposed by Hueste and Wight (1999) was only applicable to the case in which the gravity shear ratio was greater than 0.2 and roughly yielded the average predicted value of the ultimate drift ratio. The calculation formula provided by Megally and Ghali (1994) is not applicable to the case where the gravity shear ratio is relatively small. It is obviously unreasonable that the ultimate drift ratio tended to infinity as the gravity shear ratio approached zero. In the slab-column-wall structures, the slab-column frame mainly shared the gravity load, while the horizontal load was mainly carried by the shear wall. Hence, it is very important to ensure that the slab-column frame has a good lateral deformation capacity to work with the shear wall. Therefore, considering the influence of the gravity load, a relatively conservative formula (20) was obtained based on the test and FEA results. Compared with the other formulas, the proposed formula is more reasonable in agreement with the lower limit of the ultimate drift. In addition, γG,EC in Equation (20) was replaced by γG,ACI. Figure 12(b) indicates that this formula can also well fit the lower limit of the relationship between the ultimate drift ratio and gravity shear ratio calculated using ACI318-19. Relationship between the ultimate drift ratio and gravity shear ratio based on different codes: (a) EC2-04 and (b) ACI318-19.

Conclusions
In this study, FEA was performed to investigate the punching shear behavior of slab-column connections without shear reinforcement. A numerical model was proposed based on the CDP model in ABAQUS, whose major parameters were calibrated by comparing the test and numerical results. This calibrated model was applied to a parametric study considering the effects of various variables. The primary conclusions are as follows. An FEA model was established based on the CDP model in ABAQUS. The parameters of the model, such as the viscosity coefficient, mesh size, and fracture energy, were calibrated using a tested slab-column connection. Moreover, the principle of each parameter value was presented and the calibrated model was used for analyzing other tested connections. The analytical results were in good agreement with the experimental results. Based on the calibrated FEA model, the effects of the gravity shear ratio, reinforcement ratio, and concrete strength on the punching shear performance of the reinforced slab-column connections without shear reinforcement were investigated. The results showed that the ultimate unbalanced moment of the slab-column connections decreased with an increase in the gravity shear ratio and increased with an increase in the reinforcement ratio or concrete strength. Moreover, the ultimate drift ratio decreased with an increase in the gravity shear ratio and increased with an increase in the concrete strength. When the gravity shear ratio was less than the threshold value (nearly 0.23), the lateral deformation capacity of the connection decreased with an increase in the reinforcement ratio. However, if the gravity shear ratio was greater than this threshold value, the lateral deformation capacity of the connection increased first and then decreased with an increase in the reinforcement ratio. For the same gravity shear ratio, the connection with a higher concrete strength showed a larger unbalanced moment capacity and improved lateral deformation capacity. According to the experimental and FEA results, the formulas for calculating the ultimate unbalanced moment in ACI318-19 and EC2-04 were evaluated. Based on the formula for EC2-04, the correction coefficient of the formula for calculating the ultimate unbalanced moment was proposed and the accuracy of the corrected formula showed obvious improvements. To ensure the lateral deformation capacity of the connection, a formula for calculating the ultimate drift ratio was also proposed, which exhibited a higher guarantee rate than the other formulas.
The proposed methods for predicting the unbalanced moment capacity and ultimate drift ratio are limited to the test and numerical database used in this study and to interior slab-column connections with square columns, unless other evidence exists.
Footnotes
Declaration of conflicting interests
The author(s) declared no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.
Funding
The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: The authors would like to acknowledge the financial support from the Natural Science Foundation of China (No. 51178175), which made the research possible.
