3.1. Elements and Materials Definition
Field observations of the target building revealed bending-dominated failure in frame columns, characterized by circumferential cracking at member ends. Over the past decades, numerical simulation has emerged as a widely adopted method for studying column damage progression and failure mechanisms. Spacone et al. [
52] first proposed the concept of fiber beam–column elements, successfully applied to the seismic response analysis of reinforced concrete structures. Subsequently, McKenna and Fenves [
53] implemented this approach in the OpenSees software. Building on this work, Qu et al. [
54] investigated the progressive collapse of concrete frames under mid-column and side-column failure scenarios. With advancements in computational power, microscopic simulation methods have gained traction. Li et al. [
55] developed ABAQUS-based numerical models calibrated against experimental data, identifying the axial load ratio and the partial prestressing ratio as critical parameters for enhancing seismic resilience in RC frames. While solid-element models (e.g., ABAQUS) offered high-fidelity predictions of global and local deformations, their computational expense was prohibitive for large-scale analyses, and convergence issues may have compromised result accuracy. In contrast, fiber-section elements in Perform-3D effectively simulated this coupled axial–flexural behavior through discrete material integration. Each frame member was discretized into five segments along its length: two rigid zones at ends sandwiching a fiber-dominated region, with transitional elastic segments intervening (
Figure 3a). The fiber regions incorporated uniaxial material models for longitudinal rebars and confined/unconfined concrete, discretized into several fibers across the section [
56,
57,
58].
A bilinear model (Equation (1)) was chosen for the steel constitutive relationship, with parameters from the Chinese Code of Concrete [
59]. The concrete in the frame was categorized into confined and unconfined types based on its position relative to the stirrups. Confined concrete within stirrups adopted a confined concrete constitutive model, while unconfined concrete outside stirrups used an unconfined model. For hybrid frame–masonry systems, constitutive models were required to balance computational efficiency, physical fidelity, and experimental validation. Three widely adopted concrete models were considered: the Mander model [
60], the Saatcioglu–Razvi model [
61], and the modified Kent–Park model [
62]. The latter was selected for the following reasons. (i) Parameter simplicity: It required only 4–5 key parameters (e.g., peak strain, residual strength, and curvature coefficient), enabling straightforward calibration via uniaxial test data. (ii) Numerical robustness: It avoided convergence issues inherent to complex plastic potential functions (e.g., in the Mander model) during non-monotonic loading. (iii) Stirrup effect integration: It incorporated a reinforcement coefficient K to simultaneously account for stirrups’ contributions to both strength enhancement and ductility improvement, critical for distinguishing core and cover concrete behaviors. The modified Kent–Park model’s simplicity and accuracy made it widely applicable. Notably, its backbone curve under compression aligned with the Concrete01 and Concrete02 models in OpenSees [
53], which were also based on a modified Kent–Park framework. To suit the computational efficiency and accuracy of macro-elements in Perform-3D, the modified Kent–Park model was formatted into a five-segment format, as shown in
Figure 3 and Equations (1)–(3).
In these equations, σ and ε represent steel stress and strain; E is the elastic modulus; εy indicates the yield strain; fc and εc denote concrete compressive stress and strain; fc′ and ε0 signify cylinder compressive strength and corresponding strain; K symbolizes the strength enhancement factor; ρs stands for the volumetric stirrup ratio; fyh is the stirrup yield stress; and h″ indicates stirrup spacing.
Extensive numerical studies have investigated masonry wall failure mechanisms under seismic loading. Current modeling approaches for masonry walls are broadly categorized into micro-scale modeling and macro-scale modeling [
63,
64]. Micro-scale modeling approaches divide walls into individual masonry units and mortar, accounting for their anisotropic and heterogeneous properties and interfacial interactions. Alternatively, walls are treated as homogeneous entities with nonlinear material properties derived from block–mortar composites [
65]. These methods typically employ finite element (FEM) and discrete element (DEM) analyses with solid elements. For instance, Mughal et al. [
66] utilized ANSYS solid elements to explore damage evolution in multiple wall models, emphasizing the influence of opening ratios and boundary constraints. Tekeli et al. [
67] investigated failure mechanisms using ABAQUS, focusing on the impact of opening locations on wall collapse modes. However, micro-scale modeling requires highly refined meshes relative to component dimensions, resulting in computational complexity and high costs, which restricts its application to component-level studies. With advancements in seismic modeling, macro-scale modeling approaches—represented by the story mechanism model with concentrated mass elements connected via shear springs [
68], the diagonal strut model [
69], and the macro-element model with rigid interfaces and vertical springs [
70]—have enabled large-scale simulations while maintaining computational efficiency [
71,
72]. Among these, the simplified equivalent frame method (EFM) [
73,
74] has gained prominence due to its balance between accuracy and efficiency, being widely adopted by researchers and codes. Therefore, this study adopted EFM to model frame–masonry hybrid systems.
Field observations and experimental data identified shear-dominated failure in window piers. To replicate these mechanisms accurately using this method, plastic shear hinges [
75,
76,
77] were incorporated into the modeling framework. These hinges exhibited high initial stiffness and remained elastic until a certain deformation was reached, after which their stiffness degraded as damage initiated. When the peak shear force was attained, irreversible damage caused a continuous reduction in load-carrying capacity until it equaled the friction force. Upper and lower walls, with higher stiffness than window piers, were modeled as rigid zones. Although piers between windows eventually failed via shear, their bending moment contribution could not be fully disregarded. Thus, bending moment contributions from window piers were retained through composite wall–column elements. These elements integrated fiber zones, elastic zones, and plastic shear hinges to simulate perforated walls. The constitutive model for the wall–column elements followed a five-segment framework, with the parameters [
75] detailed in
Figure 4 and Equation (4), while the shear hinge models are shown in
Figure 5 and Equations (5)–(8). Model simplification and element division are illustrated in
Figure 6.
where
σm and
εm represent the stress and strain of masonry;
fm and
ε0 denote the peak stress and corresponding strain of masonry, with strain set at 0.003;
Vm indicates the peak force of the shear hinge;
αy signifies the relative parameter between the yield strength and peak strength;
Vy symbolizes the yield strength of the shear hinge, equal to the product of
αy and
Vm;
λ represents the correction factor;
σ0 stands for the vertical compressive stress;
H and L denote the height and width of the wall;
ηsoft is the stiffness degradation coefficient.
3.2. Verification and Establishment of the Numerical Model
To verify the numerical modeling approach, experimental configurations from prior research [
50,
51] were replicated using the proposed methodology. According to the experiments, the elastic modulus (
E) and yield strength (
σy) of the steel reinforcement in the constitutive model required by the software were set to 197,000 MPa and 190 MPa, respectively. For the modified Kent–Park model of the core concrete, parameters
K and
Zm were set to 1.03 and 80.81, respectively. For the sake of brevity, the remaining parameters are not listed in detail, but these parameters have been tested and verified. As shown in
Figure 7, close agreement between the simulated and experimental hysteresis curves validated the modeling strategy, confirming its reliability for analysis of different components.
The numerical model of the case-study building was constructed following the workflow in
Figure 8. Frame–column axes (axes Ⓐ and Ⓑ) were modeled using the method depicted in
Figure 6a, incorporating combined elements for frame columns. Perforated walls (axis Ⓒ), with damage concentrated at window piers, were simulated by shear hinges. Transverse walls, sharing the same deformation mechanism as the perforated walls, were modeled using the same method. As shown in
Figure 2, most damage occurred in the vertical load-bearing components, with no significant damage to beams, which were therefore connected using members with high stiffness. The material properties adhered to the Chinese Code [
59], with concrete strength specified as C30, beams and columns reinforced with HRB400 steel, and walls constructed from clay bricks and mortar with a thickness of 240 mm. Considering the walls, finishes, and equipment, loading was calculated at 1 t/m
2 in accordance with the relevant codes [
78], with loads distributed to each node based on tributary area ratios.
According to the Chinese Seismic Code [
79], Luding County in Garzê Tibetan Autonomous Prefecture, Sichuan Province, has a seismic fortification intensity of 8 degrees, a basic design earthquake acceleration of 0.2 g, and is in the second earthquake design group. Three seismic station records from Luding County were selected for analysis. An elastic–plastic time–history analysis of the example building was performed with peak ground accelerations (PGA) adjusted to 0.1 g (service level earthquake, SLE), 0.2 g (design-basis earthquake, DBE), and 0.4 g (maximum considered earthquake, MCE) [
79,
80]. To enhance computational efficiency, records were truncated to remove invalid segments while maintaining ≤0.01 spectral acceleration tolerance. These seismic station data are presented in
Table 1 and
Figure 9.
3.3. Damage State of the Prototype
To evaluate the failure states of components along various axes in the model, the damage criteria for masonry walls and frame columns were defined in accordance with experimental studies and relevant codes. For perforated walls, research by the National Institute of Standards and Technology (NIST) [
81] indicated that collapse was assumed when the strain in 30% of the wall’s cross section reached 0.01. The Masonry Standards Joint Committee (MSJC) [
82] recommended that shear failure occurred when the applied shear force exceeded the wall’s maximum shear resistance. Lagomarsino et al. [
83] further proposed using the deformation corresponding to the peak shear force as the performance point, which aligns with drift ratio thresholds in codes [
84] for different damage states. Experimental observations [
7,
50] showed that masonry walls exhibited limited ultimate deformation, with minimal lateral drift between the peak load and collapse states, making them prone to brittle shear failure. Thus, deformation corresponding to the peak force of perforated walls was defined as the performance point for these components. For frame columns, damage was evaluated using longitudinal reinforcement strain, as these components typically undergo ductile bending failure under seismic loading [
85,
86]. Post-earthquake investigations confirmed localized damage concentrations at column ends with limited global drift, prompting the adoption of strain-based criteria over displacement-based methods to capture inelastic deformation. The correspondence between strain thresholds and damage states for column components is summarized in
Table 2.
Taking the model subjected to the SC.T2271 station data with a PGA of 0.4 g as an example, the plastic states of the model at the moment when a certain axis reached its maximum performance point and when the PGA reached its peak under this condition were extracted. As is shown in
Figure 10a, all
x-direction axes were damaged to varying degrees. Specifically, the load-bearing members of axis Ⓒ reached their performance limit points, indicating shear failure. In contrast, the strain of the rebars in the frame columns of axes Ⓐ and Ⓑ was less than 0.004, meaning no significant damage had occurred. Among the load-bearing components in the
y-direction, only axes ⑥ and ④ were damaged, with damage levels at 25–50% of their performance points. At peak ground acceleration, the strain of the rebars of axis Ⓐ was between 0.004 and 0.007, indicating minor damage. While the strain for axis Ⓑ was less than 0.004, the wall in axis ⑥ reached its performance point and failed in shear. The damage to the opposite wall in axis ② exhibited minor damage, suggesting torsional effects during dynamic motion. Comparing the damage at these stages, when all the components in axis Ⓒ reached their performance limits, damage to the frame columns on the other
x-direction axes was minor, indicating a high seismic reserve. The numerical results closely matched the actual seismic damage, further validating the overall numerical model.