Figure 1.

Figure 2.

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Figure 4.
![Experimental load-displacement plots for beams type TGCB1 obtained from the four-point bending tests [26,27,28]. Notation: E = Epoxy, A = Acrylate, S = Silicone, AF = annealed float, HS = heat-strengthened](https://sciendo-parsed.s3.eu-central-1.amazonaws.com/68ed236481e1b93419696e64/j_acee-2025-0039_fig_004.jpg?X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Content-Sha256=UNSIGNED-PAYLOAD&X-Amz-Credential=AKIA6AP2G7AKOUXAVR44%2F20251021%2Feu-central-1%2Fs3%2Faws4_request&X-Amz-Date=20251021T085156Z&X-Amz-Expires=3600&X-Amz-Signature=1e4862edd1dd441e568239b802d81ef569594b989f251e0f8eb12bda0713c547&X-Amz-SignedHeaders=host&x-amz-checksum-mode=ENABLED&x-id=GetObject)
Figure 5.
![Experimental load-displacement plots for beams type TGCB2 obtained from the four-point bending tests [13,14]. Notation: A = Acrylate, S = Silicone, LN = large groove (no edge treatment), SP = small groove (polished edges)](https://sciendo-parsed.s3.eu-central-1.amazonaws.com/68ed236481e1b93419696e64/j_acee-2025-0039_fig_005.jpg?X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Content-Sha256=UNSIGNED-PAYLOAD&X-Amz-Credential=AKIA6AP2G7AKOUXAVR44%2F20251021%2Feu-central-1%2Fs3%2Faws4_request&X-Amz-Date=20251021T085156Z&X-Amz-Expires=3600&X-Amz-Signature=8bc010f29bfc3c70472f24dabec2b5b5cb80968c5226a9bbdbc19bd18712889d&X-Amz-SignedHeaders=host&x-amz-checksum-mode=ENABLED&x-id=GetObject)
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Figure 14

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Figure 21.

Figure 22.
![Comparison between numerical and experimental [27] loaddisplacement plots for the beam TBCB1_E_AF. Effects of different tensile strength of glass](https://sciendo-parsed.s3.eu-central-1.amazonaws.com/68ed236481e1b93419696e64/j_acee-2025-0039_fig_022.jpg?X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Content-Sha256=UNSIGNED-PAYLOAD&X-Amz-Credential=AKIA6AP2G7AKOUXAVR44%2F20251021%2Feu-central-1%2Fs3%2Faws4_request&X-Amz-Date=20251021T085156Z&X-Amz-Expires=3600&X-Amz-Signature=5bf4a65deeeae9a9ee0c7dbc76093fd16a62a9a7b8dd4a29e58c7e2076386e89&X-Amz-SignedHeaders=host&x-amz-checksum-mode=ENABLED&x-id=GetObject)
Figure 23.
![Comparison between numerical and experimental [13,14] load-displacement plots for the beam type TBCB2](https://sciendo-parsed.s3.eu-central-1.amazonaws.com/68ed236481e1b93419696e64/j_acee-2025-0039_fig_023.jpg?X-Amz-Algorithm=AWS4-HMAC-SHA256&X-Amz-Content-Sha256=UNSIGNED-PAYLOAD&X-Amz-Credential=AKIA6AP2G7AKOUXAVR44%2F20251021%2Feu-central-1%2Fs3%2Faws4_request&X-Amz-Date=20251021T085156Z&X-Amz-Expires=3600&X-Amz-Signature=a28ba614467a6944379cfd2aecdfc201e2ff039e1ff631c8a53ab63875d74b53&X-Amz-SignedHeaders=host&x-amz-checksum-mode=ENABLED&x-id=GetObject)
Experimental results (mean values and standard deviations) for beam specimens [13,14,26,27,28] and corresponding FE and analytical predictions_ Notation: PBSI – Post-breakage strength index PBSI = 100 × (Finit - Fult) / Fult_, PCDI - Post-cracking ductility index, PCDI = 100 × (uinit - uult) / uult, FE = 100 × (resultFE – resultEXP) / resultEXP, AN = 100 × (resultAN – resultEXP) / resultEXP
Experiments | Finite Element | Analytical | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Beam model | Fint [kN] | Fult [kN] | PBSI [%] | PCDI [%] | Kinit [MNm2] | Model | Fint [kN] | Fult [kN] | PBSI [%] | PCDI [%] | Kinit [MNm2] | Fint [kN] | Kinit [MNm2] |
TGCB1_E_AF | 11.6 (2.8) | 16.4 (2.2) | 51.5 (50) | 91.2 (86.7) | 0.898 (0.042) | E_AF_FE_FT45 | 7.2 | 12.2 | 70.6 | 176.9 | 0.920 | 7.5 | 0.817 |
ΔFE/ΔAN= | -38.4% | -25.7% | 41.3% | 94.3% | 4.9% | ||||||||
E_AF_FE_FT66 | 10.5 | 15.6 | 48.2 | 109.7 | 2.5% | 10.9 | -9.0% | ||||||
ΔFE/ΔAN= | -9.3% | -4.94% | -3.6% | 20.5% | 3.6% | ||||||||
TGCB1_E_HS | 25.5 (-) | 25.5 (-) | - | - | 0.898 (-) | E_HS_FE_FT45 | 25.5 | 25.5 | - | - | 24.5 | ||
ΔFE/ΔAN= | 0.1% | 0.1% | -3.9% | ||||||||||
TGCB1_A_HS | 25.5 (-) | 25.5 (-) | - | - | 0.907 | A_HS_FE_FT45 | 24.6 | 24.6 | - | - | 0.904 | 24.4 | 0.808 |
ΔFE/ΔAN= | -2.4% | -2.4% | -0.3% | -3.9% | -10.6% | ||||||||
TGCB1_S_HS | 19.8 (-) | 19.8 (-) | - | - | 0.720 | S_HS_FE_FT45 | 18.3 | 18.3 | - | - | 0.692 | 19.1 | 0.630 |
ΔFE/ΔAN= | -7.7% | -7.7% | -3.9% | -3.5% | -12.5% | ||||||||
TGCB2_A_AF_L | 11.1 (1.3) | 28.3 (2.4) | 158 (24.0) | 298 (51.2) | 1.253 () | A_AF_FE_L_ FT45 | 10.3 | 27.0 | 162 | 325.5 | 1.349 | 9.4 | 1.069 |
ΔFE/ΔAN= | -7.4% | -4.7% | 4.9% | 8.9% | 7.66% | -15.3% | 3.8% | ||||||
TGCB2_A_AF_S | 13.0 (1.1) | 28.7 (2.3) | 122 (24.0) | 210 (39.0) | 1.237 () | A_AF_FE_SG_FT45 | 10.5 | 21.8 | 108 | 302 | 1.367 | 9.6 | 1.081 |
ΔFE/ΔAN= | -19.2% | -23.8% | -11.4 | -43.6% | 10.5% | -26.2% | 6.3% | ||||||
TGCB2_S_AF_L | 8.8 (-) | 20.3 (-) | 131 (-) | 536 (-) | 0.918 (-) | S_AF_FE_SG_ FT45 | 8.2 | 22.8 | 179 | 465 | 1.075 | 7.4 | 0.826 |
ΔFE/ΔAN= | -6.9% | 12.4% | 36.7% | -13.3% | 17.1% | -15.9% | -10.0% |
Material properties used in numerical models for timber [27, 42]
Material | Et,l | Et,r | Et,t | νt, lr | νlt | νrt | Glr | Glt | Grt | ρt | ft |
---|---|---|---|---|---|---|---|---|---|---|---|
[MPa] | [MPa] | [MPa] | - | - | - | [MPa] | [MPa] | [MPa] | [kg/m3] | [MPa] | |
Pine wood | 12 410 | 880 | 880 | 0.44 | 0.40 | 0.52 | 1 090 | 1 090 | 140 | 510 | 34.9 |
LVL | 11 600 | 750 | 750 | 0.44 | 0.40 | 0.52 | 930 | 930 | 120 | 510 | 50 |
Material properties used in numerical models for adhesives [27]
Adhesive | ρ [kN/m3] | E [MPa] | ν [-] |
Silicone | 5 | 3 | 0.49 |
Acrylate | 5 | 100 | 0.40 |
Epoxy | 5 | 1 595 | 0.46 |
Overview of TGCB1, manufactured beam type TGCB1, n is the number of specimens produced
Beam type | Adhesive | Glass type | Length [mm] | Total height [mm] | Glass pane size [mm2] | Glass thickness [mm] | Timber block size [mm2] | Groove size [mm] |
---|---|---|---|---|---|---|---|---|
TGCB1 | Epoxy (n=6) | Annealed float | 4800 | 240 | 4800×190 | 8 | 45×60 | 12×20 |
Epoxy (n=2) Acrylate (n=2) Silicone (n=2) | Heat-strengthened |
Overview of manufactured beams, type TGCB2, n is the number of specimens produced [13,14]
Beam type | Adhesive | Glass type | Length [mm] | Total height [mm] | Glass pane size [mm2] | Glass thickness [mm] | Timber block size [mm2] | Groove size [mm] |
---|---|---|---|---|---|---|---|---|
TGCB1 | (n=1) | Annealed float | 3500 | 240 | 3500×200 | 10 | 45×60 | 13(15)×25 |
Mechanical and geometrical properties of parametric models_ Notation: R = Rectangular, P = Prism
Variation | FE/model | ft [MPa] | FE size [mm] | FE geometry [-] | Eint [MPa] |
---|---|---|---|---|---|
Reference | M-REF | 45.0 | 8 | P | 100 |
Variation of tensile strength of glass | M-FT-40.5 | 40.5 | 8 | P | 100 |
M-FT-49.5 | 49.5 | 8 | P | 100 | |
Variation of FE size | M-FE-R | 45 | 8 | R | 100 |
Variation of FE geometry | M-FE-16 | 45 | 16 | P | 100 |
M-FE-4 | 45 | 4 | P | 100 | |
M-FE-2 | 45 | 2 | P | 100 | |
Variation of adhesive stiffness | M-AE-10 | 45 | 8 | P | 10 |
M-AE-1000 | 45 | 8 | P | 1000 |