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Shear Rehabilitation of Damaged RC Beams Using Embedded Through-Section CFRP Bars Technique Cover

Shear Rehabilitation of Damaged RC Beams Using Embedded Through-Section CFRP Bars Technique

By:  and    
Open Access
|Mar 2026

Figures & Tables

Figure 1:

The effect of the a/d ratio for strengthened and unstrengthened specimens (Sogut et al, 2023)

Figure 2:

Flow chart of experimental program

Table 1:

Details of RC beam specimens

No. of seriesType of loadingSpecimen’s codesDamage ratio [%]Inclination angleLocation of CFRP bars
Series 1MonotonicM-100%Control--
M-50%50%--
M-70%70%--
MSC45-50%50%45°At the centre
MSC90-50%50%90°At the centre
MSN45-50%50%45°Near longitudinal reinforcement
MSN90-50%50%90°Near longitudinal reinforcement
MSC45-70%70%45°At the centre
MSC90-70%70%90°At the centre
MSN45-70%70%45°Near longitudinal reinforcement
MSN90-70%70%90°Near longitudinal reinforcement
Series 2RepeatedF-50%50%-
F-70%70%-
FSC45-50%50%45°At the centre
FSC90-50%50%90°At the centre
FSN45-50%50%45°Near longitudinal reinforcement
FSN90-50%50%90°Near longitudinal reinforcement
FSC45-70%70%45°At the centre
FSC90-70%70%90°At the centre
FSN45-70%70%45°Near longitudinal reinforcement
FSN90-70%70%90°Near longitudinal reinforcement
Figure 3:

Strengthening procedure of ETS CFRP bars technique; (a) Preparing holes using a drill, (b) Attaching a strain gauge to CFRP bars, (c) Cleaning the drilled holes by compressed air, (d) injecting the bonding adhesive into the holes and inserting CFRP bars

Figure 4:

The design of strengthening an RC beam with CFRP bars

Figure 5:

Test setup and steel reinforcement details of the tested beams

Figure 6:

Load vs. No. of cycles of repeated loading protocol for damaged ratios 50% and 70%

Table 2:

Repeated load protocol

StageNo. of cyclesDisplacement (mm)Load (kN)Cumulative loading cyclesAmplitude
0ne100.6317.39100.1
Two30.7621.29131.2
Three30.9126.23161.2
Four31.0927.42191.2
Five31.3133.41221.2
Sex31.5738.08251.2
Seven31.8844.27281.2
Eight32.2651.24311.2
Nine32.7164.44341.2
Ten33.2577.83371.2
Eleven33.992.77401.2
Twelve34.68100.44431.2
Table 3:

Experimental results of tested beams

Specimen codesPu (kN)Δu (mm)Δf (mm)Δ75% (mm)The efficiency of the ETS (%)Vmax (kN)Vf(exp.) (kN) K75%kNmm
M- Control101.434.66.343.06-50.715-24.86
M-50%88.994.345.393.04-44.495-21.95
M-70%79.94.085.042.78-39.95-21.56
MSC45-50%126.876.346.953.3642.5763.43518.9428.32
MSC90-50%112.545.475.913.4826.4656.2711.77524.25
MSN45-50%130.656.787.993.346.8165.32520.8329.69
MSN90-50%119.236.347.563.4233.9859.61515.1226.15
MSC45-70%122.056.957.213.9152.7561.02521.07523.41
MSC90-70%112.836.086.523.7441.2156.41516.46522.63
MSN45-70%127.17.477.93.8259.0763.5523.624.95
MSN90-70%118.516.66.953.7748.3259.25519.30523.58
F-50%82.184.265.133.12-41.09-19.75
F-70%71.393.824.783.03-35.695-17.67
FSC45-50%121.425.216.173.9747.7460.7119.6222.94
FSC90-50%105.454.65.133.4828.3252.72511.63522.73
FSN45-50%127.325.826.453.7354.9363.6622.5725.60
FSN90-50%116.244.955.733.7441.4558.1217.0323.31
FSC45-70%118.514.785.823.686659.25523.5624.15
FSC90-70%109.994.785.473.9154.0754.99519.321.1
FSN45-70%124.755.136.083.3974.7462.37526.6827.6
FSN90-70%113.974.875.913.8959.6456.98521.2922
Figure 7:

Load vs. displacement curves for control beam and pre-damaged beam up to 50% and 70%

Figure 8:

Load vs. displacement curves for 50% pre-damaged specimens

Figure 9:

Load vs. displacement curves for 70% pre-damaged specimens

Figure 10:

Load vs. concrete strain of control damaged/undamaged specimens

Figure 11:

Load vs. main steel strain of control damaged/undamaged specimens

Table 4:

Total strain of specimens (series 1)

Specimen codeConcrete strain μɛSteel strain μɛCFRP strain μɛ
M-50%24351848-
MSC45-50%263125781561
MSC90-50%255325131207
MSN45-50%265826121653
MSN90-50%258225531423
M-70%22451669-
MSC45-70%251425831315
MSC90-70%240824631064
MSN45-70%255426341572
MSN90-70%247625511209
Figure 12:

Load vs. CFRP bars strain of 50% pre-damaged beams

Figure 13:

Load vs. CFRP bars strain of 70% pre-damaged beams

Figure 14:

Failure mode of specimens (Series 1-under monotonic damage)

Figure 15:

Load vs. displacement curves for the control beam and pre-damaged repeated loading beam up to 50% and 70%

Figure 16:

Load vs. displacement curves for 50% pre-damaged repeated loading specimens

Figure 17:

Load vs. displacement curves for 70% pre-damaged repeated loading specimens

Table 5:

Total strain of specimens (Series 2)

Specimen codeConcrete strain μɛSteel strain μɛCFRP bars strain μɛ
F-50%24121823-
FSC45-50%257625491543
FSC90-50%251724871174
FSN45-50%260325861638
FSN90-50%255425211408
F-70%22211647-
FSC45-70%249325681302
FSC90-70%238124411042
FSN45-70%253126211557
FSN90-70%244625341186
Figure 18:

Load vs concrete strain of control damaged/undamaged specimens

Figure 19:

Load vs main steel strain of control damaged/undamaged specimens

Figure 20:

Load vs. CFRP bars strain of 50% pre-damaged beams

Figure 21:

Load vs. CFRP bars strain of 70% pre-damaged beams

Figure 22:

Failure mode of specimens (Series 2 - under fatigue damage)

DOI: https://doi.org/10.2478/cee-2026-0087 | Journal eISSN: 2199-6512 (formerly 1336-5835) | Journal ISSN: 1336-5835
Language: English
Submitted on: Dec 1, 2025
Accepted on: Dec 27, 2025
Published on: Mar 19, 2026
Published by: University of Žilina
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2026 Rafal A. Hadi, Raid A. Daud, published by University of Žilina
This work is licensed under the Creative Commons Attribution 4.0 License.