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Frontiers of Structural and Civil Engineering

ISSN 2095-2430

ISSN 2095-2449(Online)

CN 10-1023/X

邮发代号 80-968

2019 Impact Factor: 1.68

Frontiers of Structural and Civil Engineering  2023, Vol. 17 Issue (4): 649-668   https://doi.org/10.1007/s11709-023-0919-4
  本期目录
Numerical modelling of reinforced concrete flexural members strengthened using textile reinforced mortars
Naveen Revanna, Charles K. S. Moy()
Department of Civil Engineering, Xi’an Jiaotong-Liverpool University, Suzhou 215123, China
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Abstract

Externally bonded (EB) and near-surface mounted (NSM) bonding are two widely adopted and researched strengthening methods for reinforced-concrete structures. EB composite substrates are easy to reach and repair using appropriate surface treatments, whereas NSM techniques can be easily applied to the soffit and concrete member sides. The EB bonded fiber-reinforced polymer (FRP) technique has a significant drawback: combustibility, which calls for external protective agents, and textile reinforced mortar (TRM), a class of EB composites that is non-combustible and provides a similar functionality to any EB FRP-strengthened substrate. This study employs a finite element analysis technique to investigate the failing failure of carbon textile reinforced mortar (CTRM)-strengthened reinforced concrete beams. The principal objective of this numerical study was to develop a finite element model and validate a set of experimental data in existing literature. A set of seven beams was modelled and calibrated to obtain concrete damage plasticity (CDP) parameters. The predicted results, which were in the form of load versus deflection, load versus rebar strain, tensile damage, and compressive damage patterns, were in good agreement with the experimental data. Moreover, a parametric study was conducted to verify the applicability of the numerical model and study various influencing factors such as the concrete strength, internal reinforcement, textile roving spacing, and externally-applied load span. The ultimate load and deflection of the predicted finite element results had a coefficient of variation (COV) of 6.02% and 5.7%, respectively. A strain-based numerical comparison with known methods was then conducted to investigate the debonding mechanism. The developed finite element model can be applied and tailored further to explore similar TRM-strengthened beams undergoing debonding, and the preventive measures can be sought to avoid premature debonding.

Key wordsfiber reinforced polymer    textile reinforced mortar    finite element analysis    concrete damage plasticity    calibration and validation    parametric study
收稿日期: 2022-07-29      出版日期: 2023-06-25
Corresponding Author(s): Charles K. S. Moy   
 引用本文:   
. [J]. Frontiers of Structural and Civil Engineering, 2023, 17(4): 649-668.
Naveen Revanna, Charles K. S. Moy. Numerical modelling of reinforced concrete flexural members strengthened using textile reinforced mortars. Front. Struct. Civ. Eng., 2023, 17(4): 649-668.
 链接本文:  
https://academic.hep.com.cn/fsce/CN/10.1007/s11709-023-0919-4
https://academic.hep.com.cn/fsce/CN/Y2023/V17/I4/649
rebar size (mm) yield stress (MPa) ultimate stress (MPa) ultimate strain (%) elastic modulus (GPa)
10 480 590 17.1 210
8 550 680 8.0 210
Tab.1  
Fig.1  
Fig.2  
Fig.3  
Fig.4  
Fig.5  
dilation angle (° ) eccentricity (–) fb0/fc0 (–) K (–) viscosity (–)
40 0.1 1.1667 0.667 0
Tab.2  
Fig.6  
textile unit tensile stress (MPa) tensile strain (%) elastic modulus (MPa) bundle area (mm2) grid size (mm × mm)
carbon-Type-A [50] 4300 1.75 240 1.8 17 × 33
carbon-Type-B [50] 4300 1.75 240 2.7 17 × 33
Tab.3  
Fig.7  
ko (N/mm3) τm ax (MPa) Su (mm)
76.92* 2.31* 0.241*
Tab.4  
specimen TRM layers Exp-Pu (kN) Δu (mm) FEA-Pu (kN) Δu (mm) Exp/FEA-Pu Exp/FEA-Δu As/Af FEA mode of failure
Con-Exp NIL 49.47 29.80 45.80 29.64 1.08 1.01 NIL flexure
A1-Exp 1 58.18 18.23 59.77 17.25 0.97 1.06 34.60 debonding
A2-Exp 2 62.24 15.29 67.73 14.14 0.92 1.08 17.30 debonding
A3-Exp 3 83.29 22.08 91.58 20.50 0.91 1.08 11.53 debonding
B1-Exp 1 68.07 22.08 73.60 24.05 0.92 0.92 12.76 debonding
B2-Exp 2 73.55 15.40 76.28 14.18 0.96 1.09 25.21 debonding
B3-Exp 3 98.41 22.31 108.95 20.28 0.90 1.10 4.25 debonding
Average 0.95 1.05
STD 0.06 0.06
COV (%) 6.02 5.70
Tab.5  
Fig.8  
Fig.9  
Fig.10  
Fig.11  
Fig.12  
Fig.13  
Fig.14  
Fig.15  
Fig.16  
Fig.17  
Fig.18  
Fig.19  
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Fig.21  
Fig.22  
Fig.23  
Fig.24  
Fig.25  
Fig.26  
Fig.27  
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Fig.30  
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