Engineering Structures 207 (2020) 110238 Contents lists available at ScienceDirect Engineering Structures journal homepage: www.elsevier.com/locate/engstruct Role of punching shear reinforcement in the seismic performance of flat slab frames T ⁎ Brisid Isufia, , Ildi Cismasiua,b, Rui Marreirosa, António Pinho Ramosa,c, Válter Lúcioa,c a NOVA School of Science and Technology, Universidade NOVA de Lisboa, Caparica, Portugal UNIC Research Center in Structures and Construction of UNL, Caparica, Portugal c CERIS, Lisbon, Portugal b A R T I C LE I N FO A B S T R A C T Keywords: Punching Cyclic loading Flat slab Flat plate Seismic loading Headed studs Fragility Performance-based engineering Horizontal cyclic loading tests of flat slab–column specimens indicate that a considerable enhancement of the drift capacity can be achieved by introducing punching shear reinforcement. However, seismic design codes either do not recommend or do not cover buildings in which flat slabs are part of the primary lateral load resisting system. Nonetheless, flat slabs are popular, even in earthquake-prone areas. The purpose of this paper is to contribute towards a better understanding of the benefits and limitations of using punching shear reinforcement in the seismic performance of such structures. To this end, nonlinear static analyses and a set of fragility functions are derived for two reinforced concrete three story frame models. To minimize modelling uncertainties, the numerical models are calibrated based on two laboratory specimens (one without punching shear reinforcement and the other with headed studs) tested under reversed horizontal cyclic loading. The results show that the performance of the frames can be improved by introducing punching shear reinforcement. However, it is shown that the inherent flexibility of slab–column connections under lateral loading remains a limiting factor even when punching shear reinforcement is provided. 1. Introduction Horizontal cyclic loading tests of flat slab specimens have shown that a significant increase in the drift capacity of slab–column connections can be achieved by introducing punching shear reinforcement in the slab’s region around the column. Headed studs are among the most effective and practical solutions and their efficiency has been investigated through several horizontal cyclic loading tests [1–9]. Considerably high drift ratios at failure have been reported in the aforementioned publications (refer to [9] for a summary of results on tests under uniaxial lateral loading and square columns). In a real building, however, it is often not possible to attain such high drifts without failure of other structural elements (for example, columns, shear walls and nonstructural elements). Although tests indicate that the drift capacity can be large when punching shear reinforcement is added, the use of flat slabs as primary seismic elements in highly seismic areas is currently discouraged due to insufficient code regulations (for example, Eurocode 8 [10] does not fully cover such structures). Furthermore, flat slab structures have behaved poorly during some of the past earthquakes (notably the Mexico City earthquakes of 1985 [11] and 2017 [12]). A better understanding of the seismic behavior of such structures would therefore contribute to the risk mitigation of existing buildings and safer design of new ones. Currently, one of the most comprehensive approaches to study the seismic performance of structures or groups thereof is to analytically derive a set of fragility functions that represent the probability of exceeding a Damage State (DS) for a given ground motion Intensity Measure (IM). However, Silva et al. [13] pointed out that many challenges still exist in the nonlinear numerical modeling of components of reinforced concrete structures, with the main issue being the interaction between different failure modes. Flat slab–column connections represent a complicated case in which different failure modes ranging from pure flexure to pure punching can occur. Often, the failure is a combination of flexural yielding with punching shear failure. As a consequence, fragility analyses specific for flat slab buildings are scarce in the literature (a brief literature review is provided in Section 2). In this context, this paper aims to quantify the benefits and limitations of punching shear reinforcement in the seismic design of flat slab structures. To this end, two flat slab specimens tested under constant gravity loads and reversed horizontal cyclic drifts are used to reliably ⁎ Corresponding author at: Department of Civil Engineering, NOVA School of Science and Technology, Universidade NOVA de Lisboa, Quinta da Torre, Campus Universitário, 2829-516 Caparica, Portugal. E-mail address: b.isufi@campus.fct.unl.pt (B. Isufi). https://doi.org/10.1016/j.engstruct.2020.110238 Received 2 September 2019; Received in revised form 13 January 2020; Accepted 13 January 2020 Available online 28 January 2020 0141-0296/ © 2020 Elsevier Ltd. All rights reserved. Engineering Structures 207 (2020) 110238 B. Isufi, et al. was 2.0 m, with the slab in the middle (Fig. 1). The HE120M steel column was designed to remain elastic throughout the test. The connection between the steel column and the slab was made using rigid plates with a thickness of 50 mm and a square plan dimension equal to 250 mm. The longitudinal reinforcement ratio of the slab was approximately 1.0%. The concrete properties determined from tests are summarized in Table 1 along with the applied gravity load in the critical shear perimeter, Vg. The measured yield stress for steel reinforcement was 541.9 MPa for Φ12 mm bars (top bars), 549.5 MPa for Φ10 mm bars (bottom bars) and 488.8 MPa for the studs (Φ8 mm). The test setup is described in detail in [22]. This setup allows modelling of specimens with both negative and positive bending moment regions, i.e. the specimens represent the region from mid-span to mid-span in the longitudinal direction. For the transversal direction, the specimens are limited to points of zero moment under gravity loading, that is approximately a width equal to 22% of the span on each side of the column. This feature of the test setup makes it very suitable for the purposes of this study, because it allows for the direct calibration of the entire flat slab in the numerical models. The first step of each test was to apply the full gravity load with the values given in Table 1. Afterwards, reversed horizontal cyclic displacements were applied at the top end of the column while maintaining the gravity load constant, until failure of the specimen. A brittle punching shear failure occurred in the third cycle with target drift 1.0% in specimen C-Ref. The specimen with shear reinforcement, C-SSR5b, continued to carry the gravity load even after significant flexural yielding of the top reinforcement, until a 5.5% drift, when a punching shear failure outside the shear-reinforced zone marked the failure of the specimen. The horizontal force – displacement relationships for the two specimens are given in Section 6, along with the numerical results. calibrate numerical models of two reinforced concrete equivalent frames with similar geometry, material characteristics and loading but with different slab–column connection characteristics. In one of the frame models, no shear reinforcement is used in the flat slab around the columns. In the other frame model, the connections are reinforced with headed shear studs in a cruciform layout, leading to a significant enhancement of the ultimate drift capacity. The frames are compared in the framework of Performance Based Engineering. 2. Fragility analysis of structures containing flat slabs in the literature The fragility analysis of a 5-story flat slab building was presented in Erberik and Elnashai [14]. The authors used simplified two-dimensional models of a regular building for nonlinear static analyses and dynamic Time History Analyses (THA). The slabs were designed such that punching failures and progressive collapse would not occur. The effect of infill walls was taken into account. Hueste and Bai [15,16] included the possibility for a punching shear failure in their model of a 5-story reinforced concrete building with flat slabs, by adding a drift limit for which punching was deemed to occur based on the model proposed earlier in [17]. The lateral load resisting system of the building analyzed in [15,16] consisted of moment resisting frames in the perimeter of the building. Han et al. [18] performed a performance evaluation of two flat slab frame models with 3 and 7 stories with two levels of imposed loads, for different seismic hazard levels. The slabs contained no punching shear reinforcement. Han et al. [18] did not derive fragility functions, but they conducted pushover and nonlinear dynamic analyses and they concluded that the performance of the frames deteriorates with the increase of the ratio between the applied gravity load and the concentric punching shear resistance of the slab–column connections. Studies on the fragility analysis focused on slab–column connections as isolated components rather than the entire building were performed by Aslani and Miranda [19] and Gogus and Wallace [20]. These studies rely on experimental test results from the literature to propose component fragility functions which represent relationships between the probabilities associated with each damage limit state and the drift ratio and gravity shear ratio (GSR, defined as the ratio between the applied gravity load and concentric punching resistance). To the best of the authors’ knowledge, no previous study deals with the fragility analysis of flat slab frames without an accompanying lateral load resisting system, with flat slab–column connections susceptible to punching. The necessity for further research towards numerical modelling and derivation of fragility functions for structures with flat slabs was also highlighted in Silva et al. [13], in which a review of the current challenges and future trends in analytical fragility modelling was presented. 4. Overview of the frame models Two two-dimensional equivalent frame models of the prototype building were modelled and analyzed in the OpenSees [23] platform, one with flat slabs without shear reinforcement and another using studs as shear reinforcement. The frame models consist of an array of basic sub-assembly units such as those tested experimentally (Section 3), as illustrated in Fig. 2. The models are given names based on the following convention: number of stories followed by the type of slab–column connections. The types of slab–column connections are: NoSr for connections calibrated based on specimen C-Ref and SSR for connections calibrated based on specimen C-SSR5b, resulting in frames 3-NoSr and 3-SSR, respectively. It is assumed that punching failure can occur in the interior connections, and the connections are modelled with rotational springs as described in Section 6. It is assumed that punching failures cannot occur in the exterior connections due to the presence of a continuous support (a beam) for the slab. The columns represent a reinforced concrete square 250 × 250 column reinforced with 12Ø12 longitudinal bars. The cross-section dimensions of the columns are the same as the dimensions of the steel base plate used in the laboratory tests. Modelling of the columns is discussed in Section 5. Both frames have 5 bays and the same overall geometry (Fig. 2). Gravity load is applied in locations distributed along the slab-beam elements, resulting in a shear force in the slab–column connections equal to Vg = 215 kN. This is close to the value applied in the experiments (Table 1) and it is kept the same for both frame models to facilitate comparison. For nonlinear THA (Section 8), it was assumed that the mass is consistent with the gravity load and it is lumped at the points of application of the gravity load. 3. Experimental program Two specimens tested under constant gravity loads and reversed horizontal cyclic displacements in one direction are used as the basis of calibration of the structural models for which the fragility curves are derived in this paper. Fig. 1 shows a general view of a specimen installed in the test setup. For a detailed description of the entire experimental campaign and the results, the reader is referred to [9,21]. Nonetheless, a brief description of the main details relevant to this paper is given in this Section. The two specimens were similar in terms of geometry and longitudinal reinforcement. However, one of the specimens (C-Ref) had no shear reinforcement whereas the other (C-SSR5b) was reinforced with five rows of twelve 8 mm diameter studs spaced at 70 mm in a cruciform layout near the column. The slab specimens had a thickness equal to 150 mm and plan dimensions of 4.15 m × 1.85 m. A steel column was used and the total distance from the pinned base to the pinned top 2 Engineering Structures 207 (2020) 110238 B. Isufi, et al. Fig. 1. Test setup. Table 1 Main characteristics of the specimens. Specimen fc (MPa) Ec (GPa) fct,sp (MPa) Vg (kN) Shear reinforcement C-Ref C-SSR5b 62.3 57.6 41.4 38.8 4.4 4.1 224.8 213.9 None Studs, 5 perimeters × 12 studs 5. Modelling of the columns concrete. With the input parameters as described above, the confined concrete strain–stress relationship is obtained following the procedure described in [24], resulting in εcu,c equal to 5.6% for a compressive stress of 41 MPa and confined compressive concrete strength equal to 75 MPa. The reinforcement was modelled using a Giuffré-Menegotto-Pinto model with isotropic strain hardening (named Steel02 in OpenSees). The yield stress was taken equal to 550 MPa for both longitudinal and transverse steel. A fiber modelling approach was adopted for the columns. Two concrete materials were defined: an unconfined concrete material that is used for the fibers outside the confined core and a confined concrete model. For the unconfined concrete model, a Kent-Scott-Park concrete material model with no tensile strength was used. To minimize the variables, the unconfined concrete strength was assumed equal to 60 MPa for all the columns (in both frames). This value is close to the concrete strength used for the slabs in the experimental campaign (Table 1). Confined concrete was modelled based on the work of [24]. The model for the confined concrete requires the following inputs: unconfined concrete strength, initial modulus of elasticity of unconfined concrete, the ultimate strain of confined concrete, geometry of the hoops (diameter, configuration and spacing), steel characteristics of the hoops and the diameter of the longitudinal bars. For the unconfined concrete strength, the same value used for the concrete cover (60 MPa) was used. The modulus of elasticity was calculated in accordance with Eurocode 2 [25], resulting in a value equal to 37.7 GPa. For the ultimate strain of confined concrete, εcu,c, the formulation proposed by [26] was used. The geometry of the assumed confining steel is shown in Fig. 3, along with the cross section of the columns and the shape of the stress–strain curves for confined and unconfined 6. Modelling and calibration of the slab–column connections 6.1. Description of the adopted model for the slab–column connections Nonlinear finite element models with 3D solid elements such as those described in [27] and [28] have been shown to provide good estimates of the response of flat slab–column systems under monotonic loads. However, dynamic analyses of large structural models under horizontal loading can be extremely time consuming and challenging for finite element models with solid elements. Alternatively, shell elements can be used to model the behavior of flat slabs. However, modelling of punching shear failure in this case is rather complex and it involves special formulations. An example of an efficient numerical nonlinear fiber elements II-1 III-3 III-4 II-2 II-3 II-4 I-3 I-4 nonlinear fiber elements Lx = 3.84m I-2 2.00m I-1 2.00m Lx /2 nonlinear fiber elements full restraint III-2 2.00m rotational springs III-1 specimen Lx Lx Fig. 2. Model of the equivalent frames. 3 Lx Lx Engineering Structures 207 (2020) 110238 B. Isufi, et al. unconfined concrete ı confined concrete confined concrete 250 mm 250 mm Ec fc unconfined concrete ε cu,u =0.35% 12Ø12mm bars ε cu,c İ ε c1 =2 f c / E c Fig. 3. Cross section of the columns and confining reinforcement. model involving shell elements and nonlinear joint elements is proposed by Setiawan et al. [29]. For the purposes of this paper, however, simplified approaches using one-dimensional finite elements and nonlinear spring elements are considered, because the experimental results from Section 3 are directly used to calibrate the numerical models. The model used herein is partially based on the model proposed by Kang et al. [30]. However, some simplifications and modifications are proposed to better fit to the purposes of this study. A nonlinear fiber element modelling approach is adopted here (Fig. 4) to model the beam (“slab-beam”) elements instead of the elastic elements and slab plastic hinges of the original model. The behavior of the connection spring is shown in Fig. 5. This spring controls the unbalanced moment transfer from the column to the flat slab. Since the slab–column connections herein are calibrated based on experimental tests, simplifications are also made on the nonlinear behavior characteristics of this spring. A linear transition zone is added between the rigid branch and the perfectly plastic branch in the connection spring (Fig. 5-b) as it was found to produce results that better match the experimental data. Regarding the loss of unbalanced moment transfer due to punching shear failure, two representative scenarios are considered: drift induced punching is based on the connection rotation, which is estimated by taking out the contribution of the elastic deformation of the steel column in the laboratory. The reinforcement is modelled using a Giuffré-Menegotto-Pinto model with isotropic strain hardening (named Steel02 in OpenSees). A concrete material with linear tension softening (named Concrete02 in OpenSees) is used to model the slab-beams. It was found that neglecting the tensile strength leads to an initial stiffness that is closer to the experimental results. Therefore, tensile strength was set equal to zero for the subsequent analyses. The mechanical properties of the materials determined from tests were used (refer to Section 3). Assumptions were made for properties required by the material models that were not directly determined from tests. For instance, the strain hardening ratio of steel was assumed close to zero. The modulus of elasticity was taken equal to 200 GPa for reinforcement steel. Unconfined concrete ultimate strain was assumed equal to 0.35%. Concrete strain at strength fc was taken as described in Fig. 3 for unconfined concrete. - Punching shear failure before global yielding (i.e. before reaching the horizontal plateau in the unbalanced moment - drift relationship). This is the case of specimen C–Ref (Fig. 5-a). - Punching shear failure at a certain connection rotation (drift-induced punching), after global flexural yielding. This is the case of specimen C-SSR5b (Fig. 5-b). The connection spring characteristics were calibrated using the numerical model illustrated in Fig. 4. This model replicates the boundary conditions of the test setup. Equal deflections and rotations are enforced at the opposite slab borders (i.e. at mid-spans) through constraints. The column is made of two force-based elements with an elastic HE120M steel cross section with modulus of elasticity equal to 210 GPa. Four integration points are used along each column element. The slab is modelled by 6 force-based elements with fiber cross section. The division into six elements was made in order to apply the gravity load in the correct position (Fig. 4). The cross section was made of five stacked layers of concrete fibers and two layers of steel representing the 6.2. Calibration of the flat slab–column connections The rotational spring is modelled using the LimitState [31,32] uniaxial material in OpenSees [23], which has a trilinear backbone curve and a hysteretic behavior. The limit state model for the case of horizontal loading fibre element (column) constrained rotation and deflection gravity loads fibre element (slab) joint region coinciding points fibre column rigid elements connection spring fibre slab fibre element Fig. 4. Adopted model for the specimens and the flat slab–column connections. 4 Engineering Structures 207 (2020) 110238 B. Isufi, et al. Fig. 5. Connection spring moment-rotation relationship for specimen: (a) C-Ref, (b) C-SSR5b. top and bottom reinforcement respectively. Three integration points were used along each slab element. The rigid elements in the slab–column connection region were modelled using elastic elements with large axial, shear and bending stiffness. To fully describe the hysteretic behavior, the pinching factors for deformation and force (pX and pY) and a factor (β) need to be determined. The latter is used to calculate the unloading stiffness, Kunload, based on ductility, μ, and the initial loading stiffness, K0. A parametric study was conducted to estimate the parameters pX, pY and β based on two criteria: (a) the minimization of the difference between the energy dissipated during the test and in the numerical model and (b) numerical stability. The pinching factors were varied from 0.20 to 0.80 in steps of 0.05 while keeping β equal to 0.90, which was found suitable for numerical stability reasons. The minimum absolute difference in dissipated energy between the experiment and the numerical model was obtained for pinching factors pX = 0.8 (for displacement) and pY = 0.3 (for force). The comparison of the numerical results with the experiments is given in Fig. 6. A reasonably good match between the experiment and the numerical model was achieved. Fig. 7. Comparison of pushover curves for the two equivalent frame models. same figure in the primary axis. Using this graphical representation, it is possible to directly observe the influence of punching failures in the global response of the frames. For instance, it is noticed from Fig. 8-a that punching failures (starting from the lowest story) are associated with a change of the slope of the pushover curve. When punching failures occurred in the roof level, the base shear could not further increase significantly. In Fig. 8-b, the influence of slab–column connections in the global response is noticeable, but to a lesser extent. The maximum base shear force corresponds roughly to the point where the slab–column connections in the two lower stories reached their yielding plateau. The changes of slope due to punching failures are subtler to notice in the pushover curve of this frame. This is related to the fact that plastic mechanisms are formed in the columns for lower roof displacements, before the occurrence of punching failures. For both frames the connections in the first story failed first. The two upper level connections did not fail at all in frame 3-SSR, but failed soon after the first floor connections in frame 3-NoSr. To compare the pushover curves of frames 3-NoSr and 3-SSR and to 7. Static pushover analysis A pushover analysis was performed to assess the global behavior of the equivalent frame models. A lateral load pattern compatible with the first mode of vibration of the structure was applied. P-Δ effects were included. The resulting pushover curves for the two frame models are given in Fig. 7, where it can be noticed that the initial stiffness of the two frames is almost the same. However, the frame with no shear reinforcement in the flat slabs (3-NoSR) possesses a considerably lower base shear capacity. The post peak behavior of the two frames is similar (with comparable slope of the pushover curves). The unbalanced moments in one slab–column connection for each story are plotted in the secondary axis in Fig. 8. The names of the connections are defined in Fig. 2. Due to the regularity of the frame, the unbalanced moments in all the connections within the same story were approximately the same. The global pushover curve is plotted in the Fig. 6. Comparison of the specimen numerical models with the experimental results for specimen: (a) C-Ref, (b) C-SSR5b. 5 Engineering Structures 207 (2020) 110238 B. Isufi, et al. Fig. 8. Influence of punching failures in frame: (a) 3-NoSr, (b) 3-SSR. 0.5 Spectral acceleration (g) 0.28g 8. Seismic fragility analysis 0.30g 0.25g 0.4 8.1. Definition of damage states 0.20g 0.15g 0.3 0.2 Three damage states are defined: two global damage states and a damage state that corresponds to the occurrence of the first punching shear failure in the model. The occurrence of a punching failure is a major, potentially unrepairable, event. The flat slab-specific damage state is therefore introduced to understand the role of punching shear reinforcement in the seismic behavior of the frames from a performance-based perspective. The global damage states are based on the current version of EC8 [10], according to which two performance levels are defined for the design of new buildings: “no-collapse” and “damage limitation”. The no-collapse requirement is fulfilled if the structure withstands the design seismic action without local or global failures. In the design of conventional buildings with moment resisting frames, local failures are normally not a concern when capacity design rules are strictly followed. In case of the buildings with flat slabs, however, punching failures can occur, thus violating the no-collapse requirement. The three considered damage states are: 0.10g 0.05g 0.1 0.0 0.00 3-NoSr 3-SSR 0.02 0.04 0.06 0.08 0.10 0.12 Spectral displacement (m) 0.14 0.16 Fig. 9. Comparison of the capacity curves of the two frame models. evaluate the performance of each frame, the curves are transformed into idealized elasto–perfectly plastic curves for an equivalent Single Degree of Freedom (SDOF) system following the N2 procedure [33], as recommended in Annex B of EC8 [10]. The formation of the plastic mechanism is assumed to correspond to the point in the curve with maximum base shear force. The resulting capacity curves are plotted in Fig. 9 in Acceleration Displacement Response Spectrum (ADRS) format. Response spectra for different values of the reference ground acceleration, agR, are shown in Fig. 9. These spectra are constructed in accordance with EC8 [10], for ground type C and spectrum type 1. The values of agR that correspond to a complete exhaustion of the capacity of the structure are 0.25 g and 0.28 g for the frame 3-NoSr and 3-SSR respectively. These values are not far from each other. Furthermore, the two capacity curves demonstrate comparable ductility of the two frames, although one of them had shear reinforcement. There is some difference between the two frames in the reference ground acceleration for which the behavior becomes plastic (both are around 0.10 g, but global yielding is reached for a lower agR in 3-NoSr). Due to the high flexibility, the frames under consideration are subjected to lower seismic forces compared to stiffer structures. The intersection of the constant period line (elastic branch of the capacity curve and its extension in Fig. 9) with the response spectra occurs in the constant spectral velocity region of the spectra, i.e. the fundamental period of the frames is between TC and TD (EC8 [10]). On the other hand, this means that the displacements of the structure are larger compared to stiffer structures. This issue is addressed in the following sections. - DLS (damage limitation state). This DS corresponds to the damage limitation requirement of EC8 [10]. It is assumed that the building has ductile non-structural elements that do not interact significantly with the main structure. The criterion for DLS is set in terms of interstory drift ratios. A limiting value of 0.75% is considered for the drift ratio, in accordance with EC8 [10] for the described type of nonstructural elements. - NCS (no-collapse state). This DS corresponds to the fulfilment of the no-collapse requirement as defined in EC8. It is assumed that this state is reached when the maximum base shear of the frame is reached or when a punching failure occurs anywhere in the frame. For convenience, it is assumed that the maximum base shear is reached when the roof displacement exceeds the corresponding displacement from the pushover curve of Fig. 7 (namely, 156.7 mm for 3-NoSr and 186.1 mm for frame 3-SSR). - FPDS (first punching shear failure). This DS is reached when at least one punching failure occurs in the structure, regardless of whether any global damage state is reached. This is not to be confused with NCS described earlier, because FPDS can be reached with NCS or after it. In other words, when punching shear failures occur after the attainment of the maximum base shear capacity, NCS is reached before FPDS. On the contrary, punching shear failures occurring before the frame has reached its maximum base shear capacity result in the simultaneous attainment of NCS and FPDS. 6 Engineering Structures 207 (2020) 110238 1.2 EC8, 0.2g 1.1 0.9 0.8 0.7 0.5 0.4 0.3 0.1 0.0 0.0 0.5 1.0 1.5 2.0 2.5 3.0 Period (s) (a) Acceleration (g) 1.2 EC8, 0.1g 1.1 0.9 0.8 0.7 0.5 0.4 0.3 0.1 0.0 0.0 0.5 1.0 1.5 2.0 2.5 3.0 Period (s) Acceleration (g) Acceleration (g) B. Isufi, et al. 1.2 EC8, 0.3g 1.1 0.9 0.8 0.7 0.5 0.4 0.3 0.1 0.0 0.0 0.5 1.0 1.5 2.0 2.5 3.0 Period (s) (b) (c) Fig. 10. Five percent damped spectra for the horizontal component for the three sets of ground motion records: (a) Set I, agR = 0.10 g. (b). Set II, agR = 0.20 g. (c) Set III, agR = 0.30 g. the frames under consideration. For nonlinear dynamic analyses, Rayleigh damping with a damping ratio of 5% at the first two modes of vibration was considered. A lognormal cumulative distribution function in the form given in Eq. (1) was fitted to the results obtained from the analysis by means of the Maximum Likelihood approach. According to [39], this approach is appropriate for fitting data from MSA. 8.2. Ground motion selection and scaling The selection and scaling of ground motion records for nonlinear dynamic analysis is an important task as it can influence the results [34]. Direct scaling of ground motion records should be done with caution. To minimize the scaling factors applied to the accelerograms, therefore maintaining the accelerograms realistic, the following approach is followed in this paper. Three sets containing 30 unscaled records each are chosen from the PEER NGA-West2 database [35,36] to three Eurocode 8 [10] target spectra, based on the mean squared errors. The chosen target spectra correspond to Ground Type C, Type 1 spectrum and reference ground accelerations 0.10 g, 0.20 g and 0.30 g for Set I, II and III respectively. The unscaled ground motions in the PEER NGA database were chosen from all fault types, with magnitudes from 6.5 to 8.5, velocity vs30 from 180 m/s to 360 m/s as recommended in EC8 for Ground Type C and distance from rupture surface limited from 10 km to 80 km. The unscaled records and the target spectra for each set are shown in Fig. 10 for the horizontal component and 5% damping. Basic information for each record is provided in Appendix C of [37]. The mean squared errors of the chosen records in relation to the target spectrum were less than 0.15 g2 for Set I, less than 0.28 g2 for Set II and less than 0.57 g2 for Set III. The larger error in Set III is due to the reduced number of records in the database that match the corresponding target spectrum. For the same reason, some records belong to both Set II and Set III. The ground motion records were scaled to spectral acceleration values for the fundamental period of vibrations of the structure Sa(T1) in steps of 0.1 g. The scaling scheme consisted in direct scaling of the accelerograms of Set I to Sa(T1) values from 0.1 g to 0.4 g, of Set II records from 0.5 g to 0.8 g and of Set III records from 0.9 g to 1.2 g. The fundamental periods of the two frames were approximately the same. The fundamental period of vibrations T1 = 0.95 s, that resulted after the application of the gravity load was used as a reference for scaling. For comparison, the Eigenvalue was T1,el = 0.52 s for linear elastic analysis. It is acknowledged that flat slab buildings are generally more flexible than common moment resisting frame buildings. P (DS|Sa (T1) = x ) = Φ ⎜⎛ ⎝ ln(x / θ) ⎞ ⎟ β ⎠ (1) In Eq. (1), the left-hand side represents the probability of reaching the damage state DS given the spectral acceleration x. This probability is shown in the right-hand side of the equation, where Φ is the standard Normal cumulative distribution function, θ is the median of the fragility function and β is the dispersion (logarithmic standard deviation) of the spectral acceleration. Further details are provided in Section 8.4.1. 8.4. Results and discussion 8.4.1. No-collapse state Fig. 11 shows the maximum roof displacements during the MSA performed on each frame model. During the nonlinear dynamic analyses, the Set I of ground motion records was scaled into additional levels of 0.010 g, 0.025 g, 0.050 g, 0.075 g, 0.125 g and 0.150 g for frame 3–NoSr. Scaling into these additional levels was necessary because it was found that failures occur for considerably low spectral accelerations in this frame model. Especially for high spectral acceleration values, some of the time history analyses were interrupted before the end of the time history. It was found that this always occurred after local or global failures that caused dynamic instability. A different marker is used for these analyses to clarify the fact that although they cross the threshold for the NCS, the roof displacement value is not valid. These analysis results are stacked around roof displacement value of 400 mm and some random scatter is added to get a sense of the quantity of analyses. In Fig. 11, the threshold roof displacement for the NCS is shown with a vertical dashed line for each frame model. Counting the analyses that exceed the threshold and adding the ones in which localized punching failures occurred, the total number of analyses that exceed NCS is determined for each spectral acceleration value. Knowing the total number of analyses for each IM (spectral acceleration), the percentage of analyses that exceed NCS is calculated. In Fig. 12, these calculated values are represented by markers. The fragility functions are obtained by fitting lognormal distribution functions to these markers, as described in Section 8.3, resulting in the curves shown in Fig. 12. Fig. 12 demonstrates that the performance of the two frames is very different. It is almost impossible to fulfil the no-collapse requirement in frame 3-NoSr for spectral acceleration values higher than 0.2 g. On the other hand, the no-collapse requirement is easily fulfilled in frame 3SSR for similar spectral acceleration values. The ability of the frame 3NoSr to resist seismic actions without local or global failures is very 8.3. Derivation methodology of the fragility functions For the derivation of fragility functions, the frame models described in Section 4 were subjected to a Multiple Stripes Analysis (MSA) [38,39]. This type of analysis consists in multiple nonlinear dynamic time-history analyses for several IM levels. MSA is similar to Incremental Dynamic Analysis (IDA), but in contrast to IDA, different ground motion inputs can be used in MSA for different IM levels. Considering the purpose of this paper (Section 1), only aleatory uncertainties related to the ground motion were considered. A total of 360 analyses per frame were run, corresponding to three sets of thirty ground motion records each scaled in four levels (see Section 8.2). The spectral acceleration at the fundamental period of vibration was chosen as IM. This choice is often made in the derivation of fragility functions for first-mode dominated structures [13] and it is deemed appropriate for 7 Engineering Structures 207 (2020) 110238 1.2 1.1 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0 0 50 100 150 200 250 300 350 400 Roof displacement (mm) Spectral acceleration Sa(T1) (g) Spectral acceleration Sa(T1) (g) B. Isufi, et al. 1.2 1.1 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0 0 50 100 150 200 250 300 350 400 Roof displacement (mm) THA completed THA interrupted after dynamic instability max. base shear threshold (a) (b) Fig. 11. Results of the MSA - maximum roof displacements for each spectral acceleration level at frame: (a) 3-NoSr and (b) 3-SSR. Probability of exceeding NCS 1.0 even after punching failures (Fig. 8-a), because the columns had sufficient strength and ductility. Since punching failures are major events for a structure (potentially leading to progressive collapse), they should be carefully considered in the structural model and in the post-processing of the results. 0.9 0.8 0.7 0.6 8.4.2. Damage limitation As mentioned earlier, the DLS is deemed to be reached when the limiting drift ratio is reached. The technique followed to derive the fragility functions for DLS was similar to that adopted for NCS, but the threshold here was the limiting drift ratio. For the two frame models, the corresponding fragility functions are plotted in Fig. 13. It is noticed that the fragility curves corresponding to DLS are basically the same for both frame models. The minor differences in the figure are not of significant importance, because they are caused by the additional scaling levels of spectral accelerations that were used in frame 3-NoSr. Although it was shown that the performance of the two frames was very different for the ultimate limit state (NCS in Section 8.4.1), Fig. 13 proves that there is no difference towards the fulfillment of the damage limitation requirement of EC8 [10]. In general, this holds true as long as the ultimate drift capacity of the slab–column connections is higher than the limiting drift of the damage limitation state. As it was discussed in Section 3, the ultimate drift of the specimen C-Ref (without shear reinforcement) was 1.00%, which is higher than the considered limiting drift of 0.75%. 0.5 0.4 0.3 MSA results, 3-NoSr NCS curve for 3-NoSr MSA results, 3-SSR NCS curve for 3-SSR 0.2 0.1 0.0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 Spectral acceleration Sa(T1) (g) Fig. 12. Fragility functions for NCS. limited. A major improvement of the performance was achieved by adding shear reinforcement in the flat slabs around the columns. The mean value of the lognormal fragility function corresponding to the NCS curve for 3–SSR is 0.45 g (Table 2). For the target spectrum shape considered (see Section 8.2), this spectral acceleration value at period T1 corresponds to a reference ground acceleration of 0.25 g. This value is only slightly lower than the value determined using the pushover analysis method described in EC8 [10], as shown in Fig. 9. This indicates that when enough drift capacity is provided for the slab–column connections (for example, through sufficient punching shear reinforcement), the rather convenient pushover analysis method can be used to estimate the performance of the structure. On the other hand, the mean value of the lognormal curve corresponding to 3-NoSr is very far from the prediction of Fig. 9. The reason for this is that the occurrence of local failures is not clearly visible in the pushover analysis. The base shear in the frame continued to increase Probability of exceeding NCS 1.0 Table 2 Lognormal parameters of the fragility functions. Damage state DLS NCS FPDS 3-NoSr 3-SSR 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 θ β θ β 0.07 0.07 0.07 0.34 0.34 0.34 0.08 0.45 0.69 0.18 0.35 0.45 MSA results, 3-NoSr DLS curve for 3-NoSr MSA results, 3-SSR DLS curve for 3-SSR 0.0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 Spectral acceleration Sa(T1) (g) Fig. 13. Fragility functions for DLS. 8 Engineering Structures 207 (2020) 110238 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0 0.0 Probability of exceeding DS Probability of exceeding DS B. Isufi, et al. DLS NCS FPDS 0.2 0.4 0.6 0.8 1.0 Spectral acceleration Sa(T1) (g) 1.2 (a) 1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0 0.0 DLS NCS FPDS 0.2 0.4 0.6 0.8 1.0 Spectral acceleration Sa(T1) (g) 1.2 (b) Fig. 14. Fragility functions for all damage states considered for frame: (a) 3-NoSr and (b) 3-SSR. 8.4.3. Damage state of the flat slabs The fragility functions corresponding to the global damage states are plotted in Fig. 14 along with the flat slab specific damage state, FPDS. The lognormal parameters describing each fragility function are summarized in Table 2. The figure shows that FPDS is reached when NCS is reached in frame 3-NoSr, whereas it is reached after the NCS in frame 3-SSR. This demonstrates that the limiting factor in the frame without shear reinforcement was punching shear in slab–column connections. On the contrary, in the frame with studs, punching failures occurred only after the structure had reached its maximum resistance (i.e., FPDS was reached after NCS). In EC8 [10], damage limitation should be ensured for frequent earthquakes (with a shorter return period compared to the design earthquake, and normally, with a lower ground acceleration). In Fig. 14-a and Table 2 it is noticed that the curves for NCS and DLS perfectly match for the frame 3-NoSr. This means that the frame is not properly designed from a performance-based point of view. The earthquakes that cause exceedance of the DLS also cause exceedance of NCS. In frame 3-SSR, on the other hand, the two performance levels are clearly distinguished. This major improvement of the seismic performance was achieved by just introducing shear reinforcement in the flat slabs. Under these conditions, it was shown that the capacity of the frame can be assessed reasonably well through a conventional pushover analysis. - It was shown that the ultimate capacity can be substantially improved by introducing punching shear reinforcement if it is designed such that it enables the flat slab–column connection to exhaust the full unbalanced moment transfer capacity, as it occurred in specimen C-SSR5b and the corresponding frame model. - The damage limitation requirement was violated for relatively low spectral accelerations (median 0.07 g to 0.08 g) for both frames. This indicates that even with shear reinforcement installed, the damage in the non-structural elements remains a limiting factor for the use of flat slab frames without bracing elements in highly seismic regions. CRediT authorship contribution statement Brisid Isufi: Conceptualization, Methodology, Formal analysis, Investigation, Resources, Data curation, Writing - original draft, Writing - review & editing, Visualization. Ildi Cismasiu: Conceptualization, Resources, Writing - review & editing, Supervision. Rui Marreiros: Conceptualization, Writing - review & editing, Supervision. António Pinho Ramos: Conceptualization, Writing - review & editing, Resources, Supervision. Válter Lúcio: Conceptualization, Writing - review & editing, Resources, Supervision. 9. Conclusions Declaration of Competing Interest The role of punching shear reinforcement in the enhancement of the global behavior of two regular three-story flat slab structures towards seismic actions was investigated through pushover analyses and a set of fragility functions developed specifically for this purpose. Given the complexity of punching shear failure under seismic loading, the results cannot be considered to cover the entire range of scenarios that are encountered in practice. However, the following conclusions on the role of punching shear reinforcement in the global seismic behavior of flat slab frames are derived: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper. Acknowledgements The first author wishes to acknowledge the support received by an individual scholarship under the Grant Agreement 2014-0848/001001-Erasmus Mundus Action 2-Partnerships. - It was shown that punching failures in the frame without shear reinforcement were the governing factor in the global structural behavior. Since a punching failure is a major event for a structure, possibly unrepairable and with a high risk of being followed by progressive damage, such failures are considered to violate the nocollapse requirement of EC8 [10]. Punching failures occurred for very low spectral accelerations (median equal to 0.07 g) in the case of the frame without punching shear reinforcement. - In the frame with shear-reinforced flat slabs, yielding of the bending reinforcement of the slab–column connections was found to be related to the maximum frame base shear. Punching failures occurred for very large drifts, in the post-peak region of the pushover curve and their influence was not significant in the capacity of the frame. References [1] Dilger W, Cao H. Strength of slab-column interior connections under reversed cyclic loading. Proc. Fifth Int. Colloq. Concr. Dev. Ctries., Cairo. 1994. p. 595–608. [2] Robertson IN, Kawai T, Lee J, Enomoto B. 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