4.1. Measured data and seismic-resistant performance
The load cell installed on the table allowed the measurement of the module’s actual weight, including both the module itself and the concrete collar beam on which it was built. The measured weight was found to be 5781.0 kgf (56.693 kN). This measured weight was then compared to the theoretical weight. Table 2 indicates that the difference between the two weights is less than 5%, which confirms the accuracy of the theoretical densities used in the calculations.
Table 2
Specimen real and theoretical weight.
Total Weight | Beam weight | Real weight | Theoretical weight | Difference |
Wt | Wb | WR | WT | (WT - WR) / WR |
5781.0 kgf | 2332.8 kgf | 3448.2 kgf | 3559.5 kgf | 3% |
Throughout the entire test, detailed data were recorded to evaluate the seismic performance and describe the extent of damage to the module in each phase (refer to the video). In relation to Ghobarah’s (2004) criteria, in Phase 1, which simulated a frequent earthquake, immediate occupancy (IO) was confirmed, as no significant cracks were observed. The maximum measured drift was 0.16% at an acceleration of 0.264 g. In Phase 2, representing a rare earthquake scenario, operational limit state (O) was confirmed, as no significant damage occurred, except for slight out-of-plane movements of the walls perpendicular to the direction of motion, but a gradual loss of resistance and stiffness. The maximum measured drift was 0.50% at an acceleration of 0.809 g. Finally, in Phase 3, simulating a very rare earthquake, the shear walls exhibited the first cracks in the earth cladding, following the position of the timber structure and diagonal laths. Additionally, noticeable movement was observed in the bending walls, but no cracks in the cladding were observed. The autopsy revealed noticeable movement of the light earth infill and wall heel anchorage (see Fig. 9). The life safety (LS) structural performance level of the structure was defined for this stage, considering its transition into the inelastic phase characterized by losses in resistance and stiffness. However, it was confirmed that the timber structure could restore its original shape after the movement. The maximum measured drift reached 4.57% at an acceleration of 1.436 g.
For the three phases of movement, Table 3 presents the maximum set of electronically recorded data used to determine the key parameters necessary to analyze the module’s dynamic response. The LVDTs D1, D2, D5, and D6 measured the lateral displacement, showing low displacements between 4 and 12 mm until Phase 2, followed by a sudden increase to 115 mm when the first cracks in the cladding appeared. Additionally, the vertical displacement (D7 to D10) showed a gradual increase until Phase 3, reaching almost 12 mm. The instruments measured the maximum absolute and relative displacement, as well as the acceleration of the table and roof. By comparing the maximum acceleration at the top of the structure with the acceleration at the base for each phase, the dynamic amplification factor (DAF) was calculated.
Table 3
Absolute and relative data of lateral displacement, and acceleration of the table and roof.
Measured data | PHASE 1 | PHASE 2 | PHASE 3 |
Vertical displacements (D7, D8, D9, D10) | DV (mm) | 0.73 | 1.794 | 11.809 |
Absolute lateral displacement (D1, D2, D5, D6) | DL (mm) | 31.598 | 75.211 | 146.2 |
Relative lateral displacement (D1, D5, D6) | DR (mm) | 4.031 | 12.692 | 115.194 |
Lateral drift | Δ | 0.16% | 0.50% | 4.57% |
Structural performance level (limit state) | LS | IO | O | LS |
Table acceleration (A0) | Ao (g) | 0.264 | 0.809 | 1.436 |
Roof acceleration (A1, A3) | AR (g) | 0.596 | 2.671 | 5.577 |
Dynamic amplification factor | DAF | 2.26 | 3.30 | 3.88 |
4.2. Model dynamic properties
The test’s initial step included the system identification test, which aimed to determine the model’s dynamic properties. These free-vibration pulses were processed to identify the pulse with the best characteristics for extracting the desired parameters. Figure 10 represents the variation of the damping recorded by each accelerometer during the stages of the free vibration pulses. Throughout the test, there is an observable increase in shear wall damping (ξ). Sensors A1 and A3, located on the module’s roof, recorded very similar values, and their damping coefficients exhibited a stepped consistent increase throughout the test, with their curves practically matching for each phase from 5–17%. The damping curves of the bending walls, corresponding to Sensors A2 and A4, also showed a more gradual increasing trend, although they exhibited a slight decrease to 12% at the last free vibration pulse.
The module’s lateral stiffness (k) was determined using the relationship between the mass and the natural frequency (Eq. 5). The estimated stiffness values recorded for each movement sensor are presented in Table 4. Figure 11 illustrates the overall decrease in stiffness observed across all sensors during the test. In general, the graph demonstrates a linear decrease in stiffness until Phase 2. However, in Phase 3, which simulated a very rare earthquake scenario, a more significant decrease in stiffness is observed due to the formation of cracks and an increase in the period by up to 30%. It is worth noting that an increase in damping corresponds to a reduction in stiffness.
Table 4 presents the average values of the damping coefficient and natural period for the shear and bending stress of the module’s walls. In both types of movement, the natural and damping periods exhibit a gradual increase from 0.14 s to 0.18 s until Phase 2, followed by a significant increase to 0.26 s in Phase 3. For the structural analysis purpose, a damping period of 10%, a natural period of 0.191 s, and a natural frequency of 23 Hz can be summarized. It is worth noting that the module’s natural frequency is significantly different from the predominant frequency of the seismic signal (as shown in Fig. 7), indicating that the module remains far from the resonance condition. Regarding the system’s stiffness, all the sensors recorded comparable values with a consistent decrease over time. This decrease in stiffness was observed in each phase of the test. However, in Phase 3, a notable decrease in stiffness was observed specifically in the sensor located in one of the bending walls. This significant decrease indicates that the system experienced an incursion into the inelastic range during this phase.
Table 4
Dynamic properties of shear and bending stress walls.
Absolute dynamic properties | FV 0 | FV 1 | FV 2 | FV 3 |
Shear stress walls (A1 and A3) | Damping coefficient | ξ (%) | 5.052 | 8.327 | 10.017 | 16.980 |
Natural period | Tn (s) | 0.143 | 0.164 | 0.186 | 0.271 |
Natural frequency | ωn (rad/s) | 43.959 | 38.362 | 33.798 | 23.189 |
Lateral shear stiffness | k (kN/mm) | 6.664 | 5.073 | 3.938 | 1.854 |
Bending stress walls (A2 and A4) | Damping coefficient | ξ (%) | 10.257 | 10.829 | 12.600 | 12.593 |
Natural period | Tn (s) | 0.141 | 0.154 | 0.175 | 0.231 |
Natural frequency | ωn (rad/s) | 44.519 | 40.760 | 35.896 | 27.571 |
Bending stiffness | k (kN/mm) | 6.833 | 5.727 | 4.442 | 2.645 |
The maximum basal shear stress was calculated for each phase to analyze its relationship with the lateral displacements (using Eq. 7). Figure 12 illustrates the hysteretic behavior of the wall in axis 4, using the displacement (D6), which has been identified as the most flexible, in each phase. During Phases 1 and 2, there is a noticeable increase in the structural response due to the intensity of the seismic signal. Phase 3 also exhibits some increment, albeit with more disorder. Table 5 presents the data of the relative displacements of the sensors located on the roof (D1, D5, and D6) and the basal shears (V), organized by phases. Throughout all the phases, the values of D5 and D6 exhibit a slight difference, which becomes more pronounced in Phase 3. This difference in displacement indicates a variation in stiffness, which can be attributed to the influence of the spans of the door and window.
Table 5
Basal shears and relative displacements.
| Phase 1 | Phase 2 | Phase 3 |
DR1 (mm) | 4,031 | 12,692 | 60,136 |
DR5 (mm) | 2,270 | 6,195 | 62,738 |
DR6 (mm) | 3,287 | 9,299 | 115,194 |
V max (kN) | 20.462 | 47.736 | 96.938 |
Figure 13 presents the envelope curve of shear stress and deformation for each phase, using data from the three sensors positioned on the roof (D1, D5, and D6). In the first phase, the sensors’ relative displacements were relatively small, with the highest displacement slightly exceeding 4 mm. During the second phase, the relative displacements nearly tripled compared to the first phase, while shear forces increased by 2 to 3 times. However, an overall relationship between force and displacement can still be observed. In the third phase of the test, where the shear force doubled once again, a significant increase in relative displacements was observed. This increase, combined with the reduction in stiffness mentioned earlier, suggests that the light earth material experienced a notable decrease in its ability to resist shear forces. Indeed, the TFS demonstrated its ability to absorb and redistribute shear forces during the shaking table test. This behavior resulted in the model’s overall integrity and indicated an over-resistance stage. By effectively dissipating and transferring the applied forces, the TFS prevented the module from reaching failure even under severe seismic conditions.
4.3. Model allowable capacities
Regarding the model’s shear performance, Sensors D5 and D6 were positioned on the walls in the direction of movement. The wall at Sensor D5 contained a window, while the one at D6 had a door. Due to the model’s geometric symmetry, it can be hypothesized that each shear wall should resist half of the shear force acting in the wall’s plane. By considering half of the shear force induced on the model for each phase of the test, along with the displacements recorded by the corresponding sensors, Table 6 and Fig. 15 can be created (see Eq. 8). These present the shear stiffnesses of Sensors D5 and D6. As can be seen in the graphic, the shear stiffness also tends to decrease in each phase, the reduction being more marked in the last phase. The graph also shows that the wall containing the door has lower values, as expected. It is interesting to mention that, in the cyclic lateral load test previously carried out, a lateral stiffness in the elastic range of the wall of 3.853 kN/mm was determined. This value is quite close to the average of the values obtained for the shear walls in the first phase, in which the effect of block separation was not yet significant (see Fig. 14).
Table 6
Shear stiffness by phase.
Phases | 50% V max (kN) | DR5 (mm) | DR6 (mm) | k5 (kN/mm) | k6 (kN/mm) |
Phase 1 | 10.231 | 2.270 | 3.287 | 4.507 | 3.113 |
Phase 2 | 23.868 | 6.195 | 9.299 | 3.853 | 2.567 |
Phase 3 | 48.469 | 62.738 | 115.194 | 0.773 | 0.421 |
Finally, the seismic coefficient is determined as the ratio between the basal shear force and the weight of the structure. Knowing that the light earth model’s weight is 34.21 kN, and considering the shear forces that acted in each phase of the test, Fig. 15 is presented below. We can observe that the seismic coefficient’s increase in each phase of the test is directly related to the shear forces applied. In the third phase, the acting force was 2,867 times the weight of the structure, reaching a maximum relative displacement of 115.194 mm. However, the structure was able to resist the catastrophic earthquake.
4.4. Discussion
The shaking table test performed on the proposed TFS demonstrated good seismic performance, providing valuable insights into the system’s dynamic properties. The module’s real weight enabled the calculation of an average weight per square meter of 0.4 ton/m2, less than half of the nominal 1 ton/m2 predictable for structures of reinforced concrete. Table 7 compares the proposed TFS’s seismic performance with the analytical performance levels of conventional TFSs and the drift limits prescribed by commonly used performance criteria. The analysis reveals that the TFS exhibited a higher initial stiffness compared to conventional TFSs. However, it also exhibited increased brittleness, particularly in the immediate occupancy (IO) and operational (O) performance states, during the elastic range until Phase 2, where no damage was observed. In Phase 3, there were visible cracks on the cladding and noticeable movement of the bending and shear walls, indicating some level of structural damage and the life safety (LS) limit state. The TFS exhibited elastic behavior during both frequent and rare earthquakes, indicating its ability to withstand moderate seismic activity without experiencing significant damage. Additionally, during a severe earthquake, the TFS exhibited a subsequent inelastic stage, where it displayed over-resistance and substantial displacements without reaching failure.
Table 7
Maximum drift values in accordance with the triggered performance level.
Phases | Drift’s demands for code FEMA 356 | Roof rift limit (1) | Drift performance of a numerical analysis of a TFD (2) | Shaking table test drift result | Seismic performance levels of the module during the test |
1 | 1% temporary | 0.2% | 0.83% | 0.16% | P1. Light or frequent earthquake | Immediate occupancy |
0.25% permanent |
2 | 2% temporary | 1.5% | 1.45% | 0.50% | P2. Rare earthquake | Operational |
1% permanent |
3 | 3% temporary or | 2.5% | 2.27% | 4.57% | P3. Very rare earthquake | Life safety |
permanent |
-
Ghoborah (2001) and SEAOC (1995) Vision 2000 drift limit states
-
Benedetti et al. (2022) analytical performance drift limits
The module’s shear walls exhibited a gradual increase in damping throughout the three phases, reaching a maximum value of 17%. This increase in damping can be attributed to the independent movement of the light earth panels, as confirmed during the autopsy of the structure. These panels’ movement allowed for the dissipation of energy, resulting in higher damping and a subsequent reduction in stiffness. In contrast, the bending walls initially demonstrated a significant damping effect, which gradually increased until Phase 3. However, beyond Phase 3, the damping decreased to 12%. This observation indicates a different behavior compared to the shear walls, with a decrease in damping over time.
The results indicate that in the module’s elastic range, which includes Phases 1 and 2, the stiffness values of both the shear walls and the bending walls were similar, averaging between 3.9 and 4.2 kN/mm. However, in the subsequent inelastic stage (Phase 3), a more significant decrease in stiffness is observed. The shear walls exhibit a stiffness of 1.9 kN/mm, while the bending walls show a stiffness of 2.6 kN/mm. These findings highlight the module’s structural response under seismic loading and illustrate the transition from elastic to inelastic behavior. The decrease in stiffness reflects the system’s ability to deform and absorb energy, which is important to mitigate the impact of seismic forces.
To assess the TFS’s lateral stiffness, a comparison was made with the standard lateral stiffness of a wood stud wall without cladding, as outlined in Table 8.6.8 of NTE E.010. According to this standard, a 2.80 m long wall should have a minimum lateral stiffness of 0.48 kN/m. It was found that the lowest stiffness value in the dynamic test, wall in axis 4, was much higher than this standard requirement. This comparison suggests that the light earth blocks, particularly in the last phase of the test, did not contribute significantly to the model’s stiffness. Instead, it was the timber structure itself that exhibited the most resistance during the destructive earthquake, approaching the limit of its structural capacity.
When comparing the proposed TFS with the Peruvian code of seismic design NTP 030 (Seismic-Resistant Design), it is important to consider different scenarios and conditions. In more severe conditions, such as a timber essential building with irregularities, built in a high seismic zone and on soft soil, the seismic coefficient specified in the code would be around 0.71. This value is slightly higher than the seismic coefficient used in the first phase of the test, during which the module did not suffer any damage. In usual design conditions for timber buildings, the seismic coefficient typically ranges between 0.18 and 0.25. This implies that the TFD, as tested in the dynamic test, demonstrated good seismic performance even under more severe conditions compared to the usual design scenarios. It suggests that the TFD has the potential to withstand seismic forces and can be a viable option for seismic-resistant design.
4.5. Recommendations
The preceding paragraphs show that the results observed in the test correspond to seismic conditions of unlikely severity. However, the test has shown some of the system’s limits, which must be considered, knowing that earthquakes cause accumulative damage. In general terms, it is necessary to reduce the lateral displacement of the walls, which caused the final reduction of the system’s overall stiffness.
It was proven that the triggered failure occurred due to the reduction in the stiffness of the shear walls with openings; it is recommended to increase the openings’ stiffness by adding a timber column on both edges of the opening. Sensors D3 and D4, located on the door, showed a high incrementation of displacement in Phase 3, related to the highly noticeable movement of the columns located on the doors (4.57% drift).
In the case of the flexion walls, the maximum drift of Sensor D1, at the center of the roof collar beam of 2.39% was slightly higher than the 2% temporary life safety drift recommended by the codes. To reduce the displacement of the flexion walls, assuming the worst-case scenario, where the collar beam takes the total maximum shear force of 48.469 kN, with a free length of 252 cm, it would need a moment of inertia of 3,044 cm4. It can be noted at this point that the collar beam used in the model was insufficient in terms of both its dimensions and its location in relation to the shear force’s line of action.
Finally, despite the improvement of the general anchorage of the wall to the base, the vertical displacement of the edges was more than is acceptable, which on the autopsy of the wall proved the stress of the connections. The vertical displacements can still be improved by incorporating edge anchorage that controls the vertical displacement of the module’s edge columns, which will reduce the general lateral drift.