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Flexural strength of low-strength RC beams using CFRP composite Cover

Flexural strength of low-strength RC beams using CFRP composite

Open Access
|Dec 2025

Figures & Tables

Figure 1

RC beam detailing.

Figure 2

CFRP coupon testing: (a) universal machine test; (b) coupon under testing; (c) laminate CFRP coupons failure; and (d) fabric CFRP coupons failure.

Figure 3

Flexural strengthening program.

Figure 4

Test set-up.

Figure 5

CFRP mechanical properties.

Figure 6

Load–deflection curves.

Figure 7

Strain–load relationship at mid-span.

Figure 8

Crack pattern and associated modes of failure.

Figure 9

DIC frame illustrates crack initiating at different stages; (a) sample F1 (BF-L); and (b) sample F2 (BF-L-LB).

Figure 10

Comparison in ultimate deflection between experimental and DIC test for samples F1 (BF-L) and F2 (BF-L-LB).

Figure 11

Increase in ultimate moment capacity according to different CFRP schemes.

Figure 12

Comparison between F2 (BF-L-LB) and F3 (BF-L-SB-2) in moment and shear vs deflection.

Figure 13

Comparison between F6 (BF-L-SB-UE) and F7 (BF-L-SB-UE2) in moment and shear vs deflection.

Figure 14

Increase in ultimate load capacity according to different CFRP schemes.

Figure 15

Ductility index.

Figure 16

Section force distribution without CFRP.

Figure 17

GiD 3D model.

Figure 18

Load–deflection comparison between experimental, analytical, and GiD results for sample F1 (BF-L).

Figure 19

Load–deflection comparison between experimental, analytical, and GiD results for sample F2 (BF-L-LB).

Figure 20

Load–deflection comparison between experimental, analytical, and GiD results for sample F5 (BF-L-LB-UE5).

Figure 21

Crack pattern comparison between experimental and GiD.

Ductility index_

Beam symbolBeam ID P y (kN) Δ y (mm) P u (kN) Δ u (mm)μ ε u (steel-tension) P u /Δ u Ductility index Δ u /Δ y (μd)Increase in μd %Area under curve (kN mm)Increase in area under curve %
BF-LF148.46.751162,3643.22.39138
BF-L-LBF258.2773.410.83,3986.81.54−36%19239%
BF-L-SB-2F3465.973.420.12,8713.73.4143%413199%
BF-L-LB-UEF467.26.476.417.62,9424.72.7515%411198%
BF-L-LB-UE5F51047.2111.818.63,5806.02.588%510270%
BF-L-SB-UEF660.811.171.630.22,9002.42.7214%696404%
BF-L-SB-UE2F76710.778.222.83.42.13−11%547296%
BF-L-LBT-UEF860.66.172.811.32,8726.41.85−23%19541%

Details of strengthened RC beams_

LabelBeam symbolFRP materialSchemeNotes
F1BF-L Flexural control beam
F2BF-L-LBCFRP strip1-layer 100 mmBottom soffit
F3BF-L-SB-2CFRP sheet2-layer 100 mmBottom soffit
F4BF-L-LB-UECFRP strip/sheet1-layer 100 mm/1-layer 100 mm at both endsBottom soffit/U-wrapped only ends
F5BF-L-LB-UE5CFRP strip/sheet1-layer 100 mm/1-layer 500 mm at both endsBottom soffit/U-wrapped only ends
F6BF-L-SB-UECFRP sheet/sheet1-layer 100 mm/1-layer 100 mm at both endsBottom soffit/U-wrapped only ends
F7BF-L-SB-UE2CFRP sheet/sheet2-layer 100 mm/1-layer 100 mm at both endsBottom soffit/U-wrapped only ends
F8BF-L-LBT-UECFRP sheet/strip1-layer 100 mm/1-layer 100 mm/1 layer at both endsBottom soffit/top soffit center compression/U-wrapped only ends

Results of RC beams critical in flexural (F1–F11)_

Beam ID P cr (kN) M cr (kN m) V cr (kN) Δ cr (mm) P y (kN) M y (kN m) V y (kN) Δ y (mm) P u (kN) P u/P u.control M u (kN m) V u (kN) Δ u (mm)Failure mode
F193.04.50.7648.416.124.26.75117.025.516Flexural tension failure
F2227.311.02.0658.219.429.1773.443.9%24.536.710.8Concrete cover separation and flexural tension failure
F3144.77.01.334615.323.05.973.443.9%24.536.720.1CFRP plate debonding and concrete cover separation and flexural tension failure
F412.512.64.20.9167.267.222.46.476.462.7%27.741.517.6CFRP plate debonding and flexural tension failure
F5237.711.51.910434.752.07.2111.8119.2%37.355.918.6CFRP plate debonding and flexural tension failure
F616.55.58.21.9160.820.330.411.171.640.4%23.935.830.2CFRP plate debonding and flexural tension failure
F7227.611.42.696722.333.510.778.253.3%26.139.122.8CFRP plate debonding and flexural tension failure
F8248.112.12.3860.620.230.36.172.842.7%24.336.411.3CFRP plate debonding and flexural tension failure and flexural compression failure

Material properties of CFRP fabric and CFRP laminate provided by the manufacturer_

CharacteristicsManufacturer data
CFRP fabricCFRP laminate
Ultimate tensile strength (MPa)4,0003,100
Fiber modulus (GPa)230170
Ultimate tensile elongation (%)1.71.8
Thickness (mm)0.1671.4
Fiber density (g/cm3)1.821.6

CFRP composite material properties_

CouponAve. width (mm)Ave. thick. (mm)a Max load (kN)Max tensile stress (MPa)Max tensile strainModulus of elasticity (GPa)Poisson’s ratio
CFRP sheet (0.167 mm/ply)
150.10.71212,5600.0122209.8
250.30.73212,5300.0121209.1
350.50.78232,7000.0131206.1
450.00.82222,6060.0125208.50.28
550.80.88232,6900.0127211.8
650.10.90222,6200.0126207.9
Average 50.3 0.80 22 2,618 0.0125 208.9
CFRP laminate (1.4 mm plate thickness)
1501.41331,8970.0114166.4
2501.41311,8720.0105178.3
3501.41271,8080.0093194.40.26
4501.41341,9080.0114167.4
5501.41301,8630.0103180.9
6501.41311,8710.0105178.2
Average 50 1.4 131 1,870 0.0106 177.6

Mechanical properties of LSC_

() MPa(f t) MPa(f r) MPa(E) GPaPoisson’s ratioSlump test (mm)Velocity based on UPV test mm/μ s Density (kg/m3)
LSC17.32.383.5921.360.172654.252,246

Number of cracks at ultimate load_

Beam symbolBeam IDNumber of shear cracks diagonalNumber of flexural cracksCrack width at failure-mid span (mm)Failure mode
BF-LF10132.2Diagonal tension failure
BF-L-LBF21161.0Flexural compression failure
BF-L-SB-2F32171.0Flexural compression failure
BF-L-LB-UEF42151.0Flexural tension failure and flexural compression failure
BF-L-LB-UE5F50171.5Flexural compression failure
BF-L-SB-UEF62192.0Flexural tension failure and flexural compression failure
BF-L-SB-UE2F71191.0Flexural tension failure
BF-L-LBT-UEF80151.0Flexural compression failure

Comparison between experimental, numerical, and analytical analysis_

Exp.GiDAnaly.Evaluation
Beam ID P u (kN) M u (kN m) V u (kN) Δ u (mm) P u (kN) M u (kN m) V u (kN) Δ u (mm) P u (kN) M u (kN m) V u (kN) Δ u (mm) P u.Exp./P u.GiD P u.Exp./P u.Analy. Δ u.Exp./Δ u.GiD Δ u.Exp./Δ u.Analy.
F15117.025.51349.81725.51254.215.49.41.0240.9411.081.38
F261.420.530.710.867.522.533.87.56421.410.10.9090.9591.441.07
F5111.837.355.918.5100.533.550.3181.1121.03
DOI: https://doi.org/10.2478/msp-2025-0041 | Journal eISSN: 2083-134X | Journal ISSN: 2083-1331
Language: English
Page range: 38 - 58
Submitted on: Oct 8, 2025
|
Accepted on: Dec 2, 2025
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Published on: Dec 31, 2025
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2025 Mand Kamal Askar, Yaman Sami Shareef Al-Kamaki, published by Wroclaw University of Science and Technology
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.