Description of the approach
Under seismic actions, the local response is related to the activation of OOP collapse mechanisms (Fig. 6) of parts of the building insufficiently connected to the rest of the structure. Furthermore, fragility curves were used to describe the local response in a probabilistic context. These curves are useful for defining related vulnerability models. The intensity measure (IM) adopted in this work is the peak ground acceleration (PGA) as required by Italian building code (IMIT 2018) and which represents a common choice in the case of URM buildings. Epistemic uncertainty was treated using a logic tree approach that allows describing the vulnerability of each mechanism (Sect. 4.1). The aleatory uncertainty of each mechanism deriving from the properties of the materials, the geometry of the elements, and the loads applied on the mechanism have been treated with the Monte Carlo method (Sect. 4.2). The input parameters for a given mechanism were treated as one of the possible combinations of existing walls. To create a group of walls representative of the type of structures considered, a number of 1000 walls have been created. Such walls are the final result of all the uncertainties considered deriving from the epistemic and aleatory ones.
To create the topological fragility curves, we proceeded as follows:
-
(i)
Identification of all possible configurations of the collapse mechanisms and relative weights (Sect. 4.1).
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(ii)
Extrapolation of the main collapse mechanisms from the logic tree (Sect. 4.1).
-
(iii)
Generation of walls for the various mechanisms (Sect. 4.2).
-
(iv)
Multiple stripe analysis and creation of fragility curves (Sect. 5.2.4).
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(v)
Typological fragility curves by combining the weights of mechanisms (Sect. 5.3).
Dynamic analysis of local collapse mechanisms
Modeling unreinforced masonry walls, subjected to seismic loads, represents an important challenge for both engineers and researchers because of its complexity of being described with nonlinear dynamic analysis. In this study, a single degree of freedom (SDOF) numerical model is used for the analysis of their dynamic behavior under seismic action.
Modeling strategy
The equation of motion for a rocking block associated with a given local mechanism can be derived using Lagrange’s equation (DeJong and Dimitrakopoulos 2014):
$$\frac{d}{dt}\left( {\frac{{\partial T\left( {\phi ,\dot{\phi }} \right)}}{{\partial \dot{\phi }}}} \right) - \frac{{\partial T\left( {\phi ,\dot{\phi }} \right)}}{{\partial \dot{\phi }}} + \frac{\partial V\left( \phi \right)}{{\partial \dot{\phi }}} = - B\left( \phi \right)\ddot{u}_{g} + Q\left( \phi \right)$$
(1)
where \(\phi\) is the lagrangian parameter that describes the motion, \(T\) and V indicate kinetic and potential energy, respectively, \(- B\left( \phi \right)\ddot{u}_{g}\) is the generalized inertial force induced by earthquake ground accelerarion üg, Q is the generalized force provided by static loads and overdot stands, as usual, for time derivative. Equation 1 can be rewritten in the following form:
$$I\left( \phi \right)\ddot{\phi } + J\left( \phi \right)\dot{\phi }^{2} + G\left( \phi \right) = - B\left( \phi \right)\ddot{u}_{g} + Q\left( \phi \right)$$
(2)
where \(I\left( \phi \right)\),\(J\left( \phi \right)\),\(G\left( \phi \right)\) and \(B\left( \phi \right)\) are nonlinear functions of \(\phi\). It is also possible to derive from Eq. 2, for different local mechanisms, the load multiplier that activates the rocking motion from a resting position, i.e. from a state with null acceleration and velocity (\(\ddot{\phi } = 0, \, \dot{\phi } = 0, \, \phi = 0\)):
$$\lambda = - \frac{{\left. Q \right|_{\phi = 0} - \left. G \right|_{\phi = 0} }}{{g\left. B \right|_{\phi = 0} }}$$
(3)
where g is the gravity acceleration. The same load multiplier can be obtained by the limit analysis approach. In rocking systems, the energy dissipation is associated with the impact of the blocks at the base (Housner 1963; Yim et al. 1980; Spanos and Koh 1984). The restitution coefficient is defined, indeed, as the ratio of angular velocity after and before the nth impact. This formulation, reported in Sects. 3.2.2. and 3.2.3, is widely used in the literature (Liberatore and Spera 2001; Makris and Konstantinidis 2003; Sorrentino et al. 2011). In the adopted models it is assumed that the rigid block is rocking on a rigid foundation (this is not completely true). The coefficient strongly depends on the contact interface as shown in experimental tests (ElGawady et al. 2011). If the role of the base is considered, a possible shifting rotation point defined on the basis of the interface (compressive behavior of interface and accounting of crushing effects) should be considered (Mehrotra and DeJong 2018).
One-sided rocking
A one-sided rocking can be assumed for a wall even though the presence of internal constraints such as transverse walls and floor slabs. The governing equation for one-sided rocking of a rigid body can be written similarly to that for two-sided rocking:
$$I_{0} \ddot{\phi } + gM_{b} R\sin \left( {\alpha - \phi } \right) = - M_{b} R\ddot{u}_{g} \cos \left( {\alpha - \phi } \right)$$
(4)
where I0 is the polar moment of inertia with the pivot point 0, Mb is the mass of the block and α is the internal angle and R is the length of the half-diagonal. In the case of vertical restraint, the rotation ϕ of the system remains positive (Fig. 7). For one-sided cases, the experimental evidence shows that energy dissipation depends on the interface between rigid block and its external constraint through the coefficient (Sorrentino et al. 2011):
$$\eta_{1s} = \left( {1 - \frac{3}{2}\sin^{2} \alpha } \right)^{2} \left( {1 - \frac{3}{2}\cos^{2} \alpha } \right)$$
(5)
For a more accurate modeling of the seismic behavior of the wall, a tri-linear moment–curvature relationship with finite initial stiffness can be assumed on the basis of experimental test (Doherty et al. 2002). The tri-linear law takes account of initial imperfections, nonlinear material behavior, and the second-order effects. If this law is transformed into a tri-linear moment-rotation relationship, the motion equations can be written as follows (Boscato et al. 2014):
$$\begin{aligned} \ddot{\phi } & = - \frac{WR}{{I_{0} }}\left[ {\frac{{k_{i} }}{WR}\phi + \frac{{\ddot{x}_{g} (t)}}{g}\cos \left( {\alpha - \left| \phi \right|} \right)} \right]\quad \quad \quad \quad \quad \quad \quad {\text{if }}\left| \phi \right| \le \alpha_{1} \\ \ddot{\phi } & = - \frac{WR}{{I_{0} }}\left[ {{\text{sgn}} \left( \phi \right)\frac{{k_{i} }}{WR}\alpha_{1} + \frac{{\ddot{x}_{g} (t)}}{g}\cos \left( {\alpha - \left| \phi \right|} \right)} \right]\quad \quad \quad \quad \;{\text{if }}\alpha_{1} < \left| \phi \right| \le \alpha_{2} \\ \ddot{\phi } & = - \frac{WR}{{I_{0} }}\left[ {{\text{sgn}} (\phi )\frac{{k_{f} }}{WR}\left( {\alpha - \left| \phi \right|} \right) + \frac{{\ddot{x}_{g} (t)}}{g}\cos \left( {\alpha - \left| \phi \right|} \right)} \right]\quad \quad {\text{if }}\left| \phi \right| > \alpha_{2} \\ \end{aligned}$$
(6)
where R is the distance of the center of gravity from the rotation pivot, ki is the initial stiffness (\(k_{i} = \frac{WR\sin \left( \alpha \right)}{\alpha } \cdot \frac{{\alpha - \alpha_{2} }}{{\alpha_{1} }}\)); and kf is the final stiffness \(k_{f} = \frac{WR\sin \left( \alpha \right)}{\alpha }\) with parameter \(\alpha_{1} = \tan^{ - 1} \left( {3\frac{{\Delta_{1} }}{2H}} \right)\) (Table 2). The ultimate normalized rotation (\(\Delta_{u}\)) of the SDOF system is equal to 1. The ultimate normalized rotation corresponds to the Engineering Demand Parameter (EDP, see Sect. 5.2.3).
Table 2 The trilateral moment rotation curves parameters Two block mechanism
The two-block mechanism can be used to describe the dynamic behavior of a wall that is characterized by the formation of the classical pivot interface at the wall top, bottom, and mid-height. The top and bottom pivot can rotate if they are under a ground motion excitation. The mechanism is described by these main parameters: α1 and α2 the describe the slenderness of the two blocks; I01 and I02 that are the polar moment of inertia regarding the relative mass centers Mb1 and Mb2 that are the masses of the bottom and the top blocks (Fig. 8). The resulting equation of motion is equivalent to those proposed in the literature (Sorrentino et al. 2008; DeJong and Dimitrakopoulos 2014; Mauro et al. 2015) and can be written as follows:
$$\begin{gathered} \left( {I_{01} + B_{1} I_{02} + B_{2} M_{b2} R_{2}^{2} } \right)\ddot{\phi } + \left( {C_{1} I_{02} + C_{2} M_{b2} R_{2}^{2} } \right)\dot{\phi }^{2} + gAR_{2} \left[ {M_{b1} + M_{b2} \left( {1 + \frac{{B_{2} }}{{4A^{2} }}} \right)} \right] = \hfill \\ - A\left( {M_{b1} + M_{b2} } \right)R_{2} \cot \left( {\alpha_{1} - \phi } \right)\ddot{u}_{g} + Q \hfill \\ \end{gathered}$$
(7)
with the following system coefficients that are not constant but are functions of rotation \(\phi\).
$$\begin{aligned} A & = \frac{{\sin \left( {\alpha_{2} } \right)}}{{\sin \left( {\alpha_{1} } \right)}}\sin \left( {\alpha_{1} - \phi } \right) \\ B_{1} & = \frac{{A^{2} \cot^{2} \left( {\alpha_{1} - \phi } \right)}}{{1 - A^{2} }} \\ B_{2} & = 4A^{2} \left[ {1 + \sqrt {B1} } \right] \\ C_{1} & = \left[ {1 - \frac{{A^{2} }}{{\sin^{2} \left( {\alpha_{1} - \phi } \right)}}} \right]\left( {\frac{A}{{1 - A^{2} }}} \right)^{2} \cot \left( {\alpha_{1} - \phi } \right) \\ C_{2} & = \frac{{B_{2} }}{2}\left[ {\frac{A}{{\sqrt {1 - A^{2} } }} - \frac{{A^{2} - 2}}{{\left( {1 - A^{2} } \right)}}\cot \left( {\alpha_{1} - \phi } \right)} \right] \\ Q & = - 2ANR_{2} \sqrt {B_{2} } \cos^{2} \left( {\alpha_{2} } \right)\left[ {\frac{1}{{\sqrt {B_{2} } \cos^{2} \left( {\alpha_{2} } \right)}} + 1 + \xi \tan^{2} \left( {\alpha_{2} } \right) + \frac{{\left( {\xi - 1} \right)\tan \left( {\alpha_{2} } \right)\sqrt {1 - A^{2} } }}{A}} \right] \\ \end{aligned}$$
(8)
The critical rotation and the horizontal load multiplier of the system become:
$$\begin{aligned} \phi_{cr,0} = & \alpha_{1} \\ \lambda = & \tan \left( {\alpha_{1} } \right)\frac{{M_{b1} + \left( {M_{b2} + \frac{N}{g}} \right)\left( {2 + \frac{{\tan \left( {\alpha_{2} } \right)}}{{\tan \left( {\alpha_{1} } \right)}}} \right) + \left( {2\xi - 1} \right)\frac{N}{g}\frac{{\tan \left( {\alpha_{2} } \right)}}{{\tan \left( {\alpha_{1} } \right)}}}}{{M_{b1} + M_{b2} }} \\ \end{aligned}$$
(9)
and the coefficient of restitution \(\eta_{tb}\) is defined as follows:
$$\eta_{tb} = \frac{{M_{b1} R_{1}^{2} + I_{01} \frac{{\tan \alpha_{2} }}{{\tan \alpha_{1} }} - 2M_{b1} R_{1}^{2} \sin^{2} \alpha_{1} + M_{b2} R_{1}^{2} \left[ {2 + \frac{{\sin \alpha_{1} \cos \alpha_{1} }}{{\tan \alpha_{2} }} - \sin^{2} \alpha_{1} \left( {4 + \frac{{\tan \alpha_{2} }}{{\tan \alpha_{1} }}} \right)} \right]}}{{M_{b1} R_{1}^{2} + I_{01} - I_{02} \frac{{\tan \alpha_{2} }}{{\tan \alpha_{1} }} + M_{b2} R_{1}^{2} \left[ {2 + \sin \alpha_{1} \cos \alpha_{1} \left( {\frac{1}{{\tan \alpha_{2} }} + \tan \alpha_{2} } \right)} \right]}}$$
(10)
The coefficient of restitution depends on the slenderness of the wall and the position of the hinge. For the stockier wall and lower intermediate hinge, the energy dissipation will decrease. For this type of mechanism, the value of the coefficient of restitution is between 0.84 and 0.90 from experimental tests (Graziotti et al. 2016). This model, does neither include progressive damage (Doherty et al. 2002) nor an energy damping term (Tomassetti et al. 2019). In this paper, the analytical formulation (Eq. 10) is used for the analyses.
The rocking response results are obtained from a MATLAB code that numerically solves the nonlinear equations by means of a 4th–5th order Runge–Kutta integration technique (The Mathworks Inc. 2016).
Comparison between linear and nonlinear kinematic approaches and nonlinear dynamic analysis
In this section, a critical review of seismic response assessment techniques for local collapse mechanisms in existing masonry structures is discussed. To have statistically robust results, three types of walls with the two different configurations of constraints are subjected to nonlinear dynamic analyses (Table 3). Each wall was subjected to 44 accelerograms with 2 constraint configurations for 10 different amplitude scales of ground motion. A total of 1320 nonlinear dynamic analyses were performed. The results of the dynamic analysis are expressed by the ratio between energy demand (ED) and capacity (EC) (Shawa et al. 2012; Sorrentino et al. 2016). The energy demand (ED) is calculated as the maximum potential energy during the seismic action or as the sum of the potential and kinetic energy at instability. The capacity energy (EC) is calculated as the difference in the potential energy of the system. In Fig. 9, the results obtained from the nonlinear dynamic analyses are compared with the methods proposed by the Italian code (IMIT 2018). In the Italian code, the evaluation of local collapse mechanisms is recommended with two approaches: the force-based approach and the displacement-based approach. The force-based approach defines the acceleration capacity (a0*). The acceleration demand is defined as the peak ground acceleration (PGA) divided by behavior factor q = 2.0 according to Eurocode 8 (CEN 2004, Table 4.4). This behavior factor is suitable for partitions and facades. The ratio between demand acceleration (PGA at the base of the block) and capacity acceleration is used to compare the force-based approach to the ratio of energy demands and capacity from dynamic approach that are presented in Fig. 9a–c. The displacement-based approach, on the other hand, defines a displacement capacity (du*). The corresponding demand displacement is evaluated using the spectral displacement (SDe(TS)) at the secant period (TS) of the local mechanism. The secant period of mechanism is defined as:
$$T_{S} = 2\pi \sqrt {\frac{{d_{s}^{*} }}{{a_{s}^{*} }}}$$
(11)
where \(d_{s}^{*} = 0.4 \cdot d_{u}^{*}\) and \(a_{s}^{*}\) is the relative pseudo-acceleration of the bilinear response curve (Sorrentino et al. 2016). The ratio between displacement demand and capacity is used to compare the displacement-based approach to the ratio of energy demands and capacity from the dynamic approach that are presented in Fig. 9b–d. As it can be observed in Fig. 9, the number of non-conservative cases is less for the one-sided mechanism, while it increases in the case of two-blocks mechanism. Furthermore, it is possible to see how displacement-based approach can reduce the number of non-conservative cases. Both code approaches confirm that they are in some cases unconservative. This evidence is due to several factors, for more details see (Shawa et al. 2012; Mauro et al. 2015; Sorrentino et al. 2016).
Table 3 Block used in the analysis, b is the thickness of the wall whereas h is the height of the wall