Experimental Investigation of the Behaviour of Short-Span FRP-Reinforced Glulam Beams with Hoops and Tension Anchoring
Abstract
:Highlights
- What are the main findings?
- Hoops and tension anchoring effectively prevented stress concentration failures at the FRP termination points while also providing improvements in strength, stiffness, and displacement at failure compared to the unreinforced specimens.
- The reinforcement scheme consisting of tension anchoring contributed to an enhancement of the post-peak behaviour. Unlike tension anchoring, specimens reinforced with hoops did not see an improvement in post-peak behaviour.
- What are the implications of these findings?
- Tension anchoring is a promising reinforcement configuration where partial access to all four sides of the member while minimizing the overall quantity of reinforcement in comparison to full-length confinement.
- The favourable behaviour exhibited by the tension anchoring should be further evaluated on larger glulam specimens, in addition to investigating the potential of using FRP anchoring when access to all four sides is not possible.
Abstract
1. Introduction
2. Experimental Programme
2.1. Description of Materials
2.2. Reinforcement Configurations
2.3. FRP Application Process
2.4. Full-Scale Four-Point Bending Test Set-Up
3. Experimental Results
3.1. Overview of Flexural Tests on GFRP-Reinforced Glulam Beams
3.2. Effects of Hoops and Simple Tension Reinforcement
3.3. Effects of Tension Anchoring
3.4. Effects of Full-Length Confinement
3.5. Effects of Beam Depth
3.6. Enhancement of Wood Tensile Failure Strain Due to FRP
4. Discussion
5. Conclusions
- The hoops consisting of unidirectional and bidirectional fabrics were both successful in preventing previous premature failures due to stress concentration at the termination point; however, in order to leverage the full potential of hoops, unidirectional fabric should be used as it provided a higher clamping pressure than that provided by the hoops using bidirectional fabrics.
- Tension anchoring using bidirectional fabrics showed promising results with increased peak loads, displacement at peak load, stiffness, and post-peak behaviour. The tension anchoring used in combination with simple tension reinforcement that consist of unidirectional fabrics did not perform as well due to the improper FRP bond (wood-to-FRP, FRP-FRP) arising from the fabrication and epoxy mix. Future studies should investigate the potential of the configuration.
- Full-length confinement showed the most significant improved response as anticipated; however, the tension anchoring provided the closest response with lesser FRP materials.
- The reinforcement schemes consisting of hoops and tension anchoring showed favourable and promising response at larger spans and beam depth.
- An average increase in wood tensile failure strain in the reinforced beams compared to the unreinforced beams of 1.16 was obtained, showing that the reinforcement configurations allowed for a flexural failure rather than shear failure.
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Abbreviations
glulam | Glued-Laminated Timber |
CLT | Cross-Laminated Timber |
FRP | Fibre-Reinforced Polymer |
AFRP | Aramid Fibre Reinforced Polymer |
BFRP | Basal Fibre Reinforced Polymer |
CFRP | Carbon Fibre Reinforced Polymer |
GFRP | Glass Fibre Reinforced Polymer |
CSA | Canadian Standards Association (CSA Group) |
ASTM | American Society for Testing and Materials |
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Specimens | Legend | ||
---|---|---|---|
Depth | ID and FRP Scheme | ||
100d | A-1 | S[0]2 H[0]2 | FRP Reinforcement Configurations |
A-2 | S[0]4 H[0]2 | S—Simple Tension U—U-Shape H—Hoops C—Full-Length Confinement TA—Tension with Anchoring | |
A-3 | S[0]2 H[0/90]2 | ||
A-4 | S[0]4 H[0/90]2 | ||
B-1, B-2 | S[0]2 TA [0/90]2 | ||
B-3, B-4 | TA [0/90]4 | GFRP Layers Types | |
C-1, C-2 | U [0]2 C [0/90]2 | 0—Unidirectional 0/90—Bidirectional | |
C-3, C-4 | C [0/90]4 | Example: S[0]3 H[0/90]2 | |
160d | D-1, D-2 | S[0]3 H[0/90]2 | Three layers of unidirectional simple tension FRP with two layers of bidirectional hoops |
E-1, E-2 | TA [0/90]6 |
Specimen | Pmax a | ΔP,max b | K c | ɛt,max d × 10−4 | ɛc,max e × 10−4 | ɛFRP,max f × 10−4 | Glulam Primary Failure Modes | ||
---|---|---|---|---|---|---|---|---|---|
Depth | ID and FRP Scheme | (kN) | (mm) | (kN/mm) | (mm/mm) | (mm/mm) | (mm/mm) | ||
100d | Unreinforced g,h | 32.8 (0.11) | 26.0 (0.10) | 1.70 (0.13) | 47.9 (0.15) | −49.3 (0.18) | - | Splintering, shear | |
Simple tension g,h | 34.7 (0.06) | 18.8 (0.25) | 2.14 (0.15) | 34.7 (0.22) | −44.9 (0.37) | 53.5 (0.38) | Shear, stress concentrations at FRP termination point | ||
A-1 | S[0]2 H[0]2 | 39.5 | 18.3 | 2.36 | 43.6 | −11.4 | 59.8 | Splintering | |
A-2 | S[0]4 H[0]2 | 36.8 | 27.4 | 1.72 | 42.4 | −28.3 | 73.9 | Brash | |
Avg. | 38.2 | 22.8 | 2.04 | 43.0 | −19.8 | 66.8 | - | ||
A-3 | S[0]2 H[0/90]2 | 35.0 | 15.1 | 2.42 | 56.8 | −45.4 | 67.2 | Splintering | |
A-4 | S[0]4 H[0/90]2 | 40.0 | 16.5 | 2.50 | 36.3 | −42.9 | 40.3 | Splintering | |
Avg. | 37.5 | 15.8 | 2.46 | 46.6 | −44.1 | 53.7 | - | ||
B-1 | S[0]2 TA [0/90]2 | 36.4 | 24.8 | 1.86 | 45.4 | −45.6 | 74.1 | Brash at a knot within TA | |
B-2 | 32.4 | 21.5 | 1.65 | 45.1 | - | 66.7 | Splintering | ||
Avg. | 34.4 | 23.1 | 1.75 | 45.2 | −45.6 | 70.4 | - | ||
B-3 | TA [0/90]4 | 47.2 | 31.8 | 2.38 | 41.2 | −37.5 | 51.4 | Splintering | |
B-4 | 44.3 | 36.2 | 1.93 | 61.1 | - | 80.3 | Splintering, shear | ||
Avg. | 45.7 | 34.0 | 2.16 | 51.1 | −37.5 | 65.9 | - | ||
C-1 | U [0]2 C [0/90]2 | 56.1 | 36.2 | 2.76 | 62.8 | −43.5 | 71.2 | Splintering, localized | |
C-2 | 49.7 | 32.0 | 2.71 | 52.2 | −51.3 | 88.6 | Splintering, localized | ||
Avg. | 52.9 | 34.1 | 2.74 | 57.5 | −47.4 | 79.9 | - | ||
C-3 | C [0/90]4 | 58.1 | 26.5 | 2.80 | 116.0 | −45.2 | - | Splintering, localized | |
C-4 | 58.8 | 25.8 | 2.76 | 63.7 | −34.7 | 65.8 | Splintering, localized | ||
Avg. | 58.5 | 26.2 | 2.78 | 89.9 | −40.0 | 65.8 | - | ||
160d | Unreinforced-Theoretical i | 52.8 | 29.7 | 1.78 | - | - | - | - | |
D-1 | S[0]3 H[0/90]2 | 62.9 | 36.2 | 2.11 | 60.1 | −43.8 | 44.4 | Splintering | |
D-2 | 60.0 | 36.8 | 2.16 | 50.2 | −48.1 | 54.6 | Cross-grain at a knot | ||
Avg. | 61.4 | 36.5 | 2.14 | 55.2 | −46.0 | 49.5 | - | ||
E-1 | TA [0/90]6 | 63.8 | 36.2 | 2.22 | 57.9 | −50.4 | 55.7 | Splintering | |
E-2 | 67.7 | 35.5 | 2.31 | 54.2 | - | 54.2 | Splintering | ||
Avg. | 65.7 | 35.9 | 2.27 | 56.1 | −50.4 | 55.0 | - |
Specimen | Wood Tensile Failure Strain, ɛt,max × 10−4 (mm/mm) | b |
---|---|---|
Unreinforced a | 47.9 | - |
A-1 | 43.6 | 0.91 |
A-2 | 42.4 | 0.88 |
A-3 | 56.8 | 1.19 |
A-4 | 36.3 | 0.76 |
B-1 | 45.4 | 0.95 |
B-2 | 45.1 | 0.94 |
B-3 | 41.2 | 0.86 |
B-4 | 61.1 | 1.27 |
C-1 | 62.8 | 1.31 |
C-2 | 52.2 | 1.09 |
C-3 | 116.0 | 2.42 |
C-4 | 63.7 | 1.33 |
D-1 | 60.1 | 1.26 |
D-2 | 50.2 | 1.05 |
E-1 | 57.9 | 1.21 |
E-2 | 56.1 | 1.13 |
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Chen, H.; Vetter, Y.; Shrimpton, C.; Lacroix, D. Experimental Investigation of the Behaviour of Short-Span FRP-Reinforced Glulam Beams with Hoops and Tension Anchoring. Fibers 2025, 13, 80. https://doi.org/10.3390/fib13060080
Chen H, Vetter Y, Shrimpton C, Lacroix D. Experimental Investigation of the Behaviour of Short-Span FRP-Reinforced Glulam Beams with Hoops and Tension Anchoring. Fibers. 2025; 13(6):80. https://doi.org/10.3390/fib13060080
Chicago/Turabian StyleChen, Herry, Yannick Vetter, Catherine Shrimpton, and Daniel Lacroix. 2025. "Experimental Investigation of the Behaviour of Short-Span FRP-Reinforced Glulam Beams with Hoops and Tension Anchoring" Fibers 13, no. 6: 80. https://doi.org/10.3390/fib13060080
APA StyleChen, H., Vetter, Y., Shrimpton, C., & Lacroix, D. (2025). Experimental Investigation of the Behaviour of Short-Span FRP-Reinforced Glulam Beams with Hoops and Tension Anchoring. Fibers, 13(6), 80. https://doi.org/10.3390/fib13060080