4.1 Failure mode
The key objectives of this study are to investigate the impact of the curvature on the failure modes of the LBC composite beams and to identify the differences in the structural behaviours between the straight and curved beams. After examining the features of eight specimen rupture tests, a total of seven failure modes were categorised and the dominant failure mode and accompanying failure modes for each tested beam were identified. These failure modes are:
- Shear-bonding failure of laminated bamboo (failure mode ①). This failure line is clearly developed along the glue line of the laminated bamboo and this behaviour indicates that bonding strength between the laminated bamboo layer is a weak point of this type of material.
- Tension failure of the laminated bamboo component in the tension zone (failure mode ②). This is another failure mode associated with the laminated bamboo component (only two modes are associated with laminated bamboo).
- Compression zone longitudinal cracks (full length) of the concrete slab (failure mode ③). This could be caused by the transverse bending moment from the load spreading plate at the top concrete surface, as there is no transverse tension steel at the top of the concrete surface.
- Shear failure of concrete slab flanges at the shear-bending section of the composite beam (failure mode ④). This is a common failure mode observed at the final stage of the test.
- Flexural cracks of the concrete slab in the pure bending section of the composite beam (failure mode ⑤). This happened to every specimen beam and the cracks distributed evenly within the pure bending section.
- Diagonal shear cracks of the concrete inserts for specimens with large curvatures (BCC-2 and BCC-3, failure mode ⑥).
- Interface shear slip failure between the laminated bamboo and concrete components (failure mode ⑦). This failure mode was observed for every specimen beam during the tests.
A complete record of the dominant and accompanying failure modes for each specimen is listed in Table 3 and more details are listed in the Appendix.
For straight LBC beams (BCC-0a, b), all the dominant failure modes are the laminated bamboo glue line shear bonding failures (failure mode ①). The laminated bamboo in the tension zone was intact without sign of tension failure. All the other accompanying failure modes (failure mode ③, ④, ⑤ and ⑦) were not obvious until after the laminated bamboo's brittle dominant shear bonding failure. The shear bonding failures all happened abruptly with a distinctive large sudden sound, followed by the accompanying component failures.
The curved profile could be assumed to change the embed angle between the concrete and laminated bamboo, which could change the shear studs' effectiveness and eventually impact the failure modes. However, the test results reveal the opposite in that for all the curved LBC beams (BCC-1a,b, BCC-2a,b, BCC-3a,b), even with different curvatures, the dominant failure modes are still the shear bonding failure (failure mode ①), the same as the straight beams. There was one new type of accompanying failure mode observed in the tests; failure mode ②, tension failure of the laminated bamboo component. This failure mode happened right after the dominant failure. Meanwhile, the straight beams experienced the damaging effect of the shock wave quite evenly distributed along the whole beam length at the instance of failure. The damaging effect of the shock wave was concentrated on the weakest mid-span section in the curved beams due to the uneven stiffness distribution along the beam length with curved profiles.
In conclusion, after comparing the structural behaviours between the straight and curved LBC composite beam, it is clear that there are two interacting key aspects that influence the structural behaviours of these beams. One is the effectiveness of the shear studs; another is the interlayer shear bonding strength of laminated bamboo components. The effectiveness of the shear studs reflects whether the concrete and laminated bamboo components are working together. The interlayer shear bonding strength of laminated bamboo is proven to be the thresholding parameter that determines the overall flexural strength of the whole composite beam, whether straight or curved. The weak interlayer shear bonding strength in the laminated bamboo component led to the consistent dominant failure mode in all the specimens. The development of a stronger laminated bamboo-composite would require further studies to improve the bonding strength of the adhesive and the fabrication technology to increase the shear bonding strength. The effectiveness of the shear studs is the key factor that ensures the composite synergy of the laminated bamboo and concrete components. When the shear studs yielded or failed, the two-part composite beam still worked as a semi-composite beam or two separated beams that stacked together. So, the overall stiffness is reduced and any further burden will be put on the shear bonding strength of the laminated bamboo component and cause an earlier failure in shear bonding. Thus, the effectiveness of the shear studs and the interlayer shear bonding strength of the laminated bamboo interact with each other.
Between these two key elements, the shear bonding strength is heavily reliant on the quality of the adhesive, for bonding the bamboo materials, and advanced fabrication technology. The latter falls slightly outside of structural engineers' key focus research areas but to improve the effectiveness of the shear studs is one of the most relevant structural engineering topics that attracted much research interest in the recent years [31, 45-47] using the push-out test of scaled specimens. However, in this study, a different approach was developed to calibrate the concrete to laminated bamboo interface shear slip directly from the four-point bending test of full-scale LBC composite beams. Full details are discussed in Section 5.
4.2 Load-deflection behaviour and section stiffness
The load vs mid-span deflection curves for each specimen are shown in Figure 7. To visualise the composite effect of these specimens, the boundaries of non-composite effect and full composite effect are shown as two slope-shaped straight boundary lines in the figures. The lower boundary corresponds to the non-composite effect (lower bound) scenario, i.e., assuming that the laminated bamboo and concrete components are simply stacked up with no shear transfer in between. The upper boundary corresponds to the full shear-bonded composite effect (upper bound), i.e., assuming that the laminated bamboo and concrete components are connected firmly without any interface slip. Another vertical dashed line in each figure marks the span/250 deflection limit, i.e., the equivalent service limited in deflection.
As shown in Figure 7, the elastic section of the load-mid-span deflection curve is nearly the same and approximately linear for all groups of specimens until the maximum deflection reaches l/250 of the span. However, there is a noticeable difference between the curved and straight composite beams in the elastic stage. The curved composite beam demonstrated a better shear bonding effect than the straight ones. As shown in Figure 7(b)-(d), the slope of the load-mid-span deflection curves for the curved composite beam at the elastic range is closer to the upper bound than the straight composite beam, as shown in Figure 7(a). This result indicates that the curved laminated bamboo to concrete contact surface configuration has improved the composite effect in the elastic stage. The improvement in the curved composite beams could come from the varying angles of directions along which the shear studs were anchored into the concrete and laminated bamboo components. By varying the angle of the shear studs, a better interlocking mechanism can be formed between the concrete and laminated bamboo components. While the shear studs in the straight composite beams are parallel to each other without the benefit of forming the interlocking mechanism, the shear connecting effect is weaker than the curved beam. Another interesting observation is that all beams failed at or close to the lower bound line. This result indicates that the ultimate rupture occurred at the moment when the shear studs failed completely, i.e., there was no shear connection at all between the concrete and laminated bamboo contact surface.
The main test results for all specimens are summarised in Table 3. Three indicators are used to characterize the composite beam behaviour, two for the elastic stage and one for the inelastic stage. As there is no clear boundary between the elastic and inelastic stages, two indicators, one related to loading, i.e., loading at 100 kN, and one related to deflection, i.e., mid-span deflection reaches span/250, were used to mark the stage change after inspecting Figure 7. The corresponding mid-span deflection at 100 kN and the corresponding load attainted at the moment the mid-span deflection reached span/250 were used to estimate the flexural stiffness and Coefficient of Composite Efficiency (CCE, ) of the composite beams at the elastic stages. The CCE was used to specify the composite effect of the concrete and laminated bamboo components. It was quantified by the percentage of the fully composited beam stiffness that a specimen achieved in a test within the elastic range. The third component of Table 3 summarises the test results for the ultimate state, including ultimate loads, maximum mid-span deflections, and the ductility indicator. The ductility is the ratio of the corresponding load Pl/250 (loading attainted when mid-span deflection reached span/250) to the ultimate load.
As shown in Table 3, in the elastic range, the overall flexural stiffness increased by around 20%, and the average CCE increased from 67-77% to 80-90% when compared with the straight composite beam, whether using the 100 kN load or span/250 as the phase change indicator. However, the test results also show that the flexural stiffness and CCE of the composite beams did not increase when the curvature increased, they either levelled off or slightly decreased. For the ultimate limit state, there is no noticeable increase in the ultimate loads and maximum deflections recorded from the straight to curved composite beams. However, the ductility of the composite beams with a medium level of curvature shows a slight increase when compared to the straight, low, and high-curvature composite beams. In conclusion, the curved LBC composite beams have a slightly higher flexural stiffness in the elastic stage when compared to the straight LBC beams, but the curved design setup does not benefit from the ultimate flexural capacity. There is no clear benefit to the ductility of the composite beams except a small increase for the medium curvature composite beams.
4.3 Load-strain relationship
The load-strain relationship of the mid-span cross-section was measured by the strain gauges distributed vertically on the side surface (CS7-9 on concrete, GS1-6 on laminated bamboo, as shown in Figure 5). The load-strain history logged by the sensors are shown in Figure 8. Compared to the other non-bio-based composite beams, such as steel reinforced concrete (SRC) beams, the tracks in the strain history plot intersect each other. For example, the tracks of strain gauges CS7-9 and GS1-3 intersect. This result indicates that there was interface shear slip between the concrete and the laminated bamboo contact surface and the shear connectors were degrading during the test. To verify this degradation, the load-strain histories were re-plotted along the depth of the cross-section, as shown in Figure 9. When subjected to small loading, the strain profile along the depth of the cross-section suggests that the cross-section more and less remained plane. However, when the loading increased, the difference between the strain gauges CS9 and GS1, next to the concrete to laminated bamboo contact surface, also increased due to the shear connector degrading and shear stud failures. So at this stage, the plane cross-section remained plane regionly, i.e., the plane of concrete and laminated bamboo components remained two separated planes, respectively. The LVDTs S1-5 also captured the slip between the concrete and laminated bamboo, and the test results are shown in Figure 10.
The load-strain history of strain gauge CS1-6, installed at the top surface of the mid-span of the concrete component, is shown in Figure 11. Most of the readings from different sensors were well aligned, i.e., there was no significant twist during the test. But some sensors at the cross-section's edge exhibited a discernible, but insignificant, discrepancy with others. This indicates the specimen was slightly twisted during the test which could be due to the imperfect test setup. This observation suggests that using strain gauges at the top surface of a T-section at mid-span is a reliable way to monitor whether a lateral torsion developed during the test.