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ond-slip parameters calculated using Lu et al.’s (2005b) bi-linear bond-slip model are: δ f = 0.16 mm; τ f = 3.5<br />

MPa; and G f = 0.28 N/mm. <strong>The</strong>se parameters may also be obtained using other models such as Seracino et al.<br />

(2007). Key points in the load-displacement response are marked as O, A and B in Figure 6. <strong>The</strong> curve OA<br />

represents the S–R state of the interface, with point A representing the initiation of debonding. <strong>The</strong> plateau AB<br />

represents the D–S–R state, with point B representing the end of the D-S-R state when the softening front<br />

reaches mid-span. <strong>The</strong> curve starting from B onwards (dotted line in Figure 6) refers to the D–S state which<br />

has little practical significance as discussed above.<br />

20<br />

Bending moment (kNm)<br />

16<br />

12<br />

8<br />

4<br />

O<br />

•<br />

A<br />

B<br />

• •<br />

0<br />

0.0 0.3 0.5 0.8 1.0 1.3 1.5<br />

Relative displacement at the left plate end (mm)<br />

Figure 6 Load-displacement response of the bonded joint in CMR<br />

FLEXURAL DEBONDING TEST DATABASE<br />

A large database containing 67 RC beams with the flexural strengthening plate terminated in a CMR and which<br />

failed due to flexural debonding has been assembled from an extensive literature survey.. <strong>The</strong> database includes<br />

54 steel plated beams, 9 CFRP plated beams, 2 GFRP plated beams and 2 C-GFRP plated beams. All the beams<br />

failed due to flexural PED failure either by concrete cover separation or interfacial failure or a combination of<br />

these two modes. Geometric and material parameters for the beams can be found in Oehlers and Moran (1990),<br />

Oehlers (1992), Mohammed Ali et al. (2001), Smith and Teng (2003) and Yao and Teng (2007). Measured<br />

debonding moments and debonding moments predicted by the expressions derived earlier are presented in Table<br />

1. It is seen that these tests cover a wide range of important parameters: (1) elastic modulus of plate E 2 = 8.8-257<br />

GPa; (2) nominal thickness of plate t 2 = 0.165-32 mm; (3) cube strength of the concrete f cu = 25-59 MPa; (4)<br />

split tensile strength of the concrete f t = 2.55-4.9 MPa; (5) elastic modulus of concrete E 1 = 20-32 GPa; (6) axial<br />

stiffness of plate per unit width E 2 t 2 = 37.6-3150 (x10 3 ) N/mm; (7) effective axial stiffness of beam per unit<br />

width E 1 d e = 2.4-7.1 (x10 6 ) N/mm; (8) flexural rigidity of the cracked plated RC beam section (EI) c,p = 0.83-6.7<br />

(x10 12 ) Nmm 2 ; (9) flexural rigidity of the cracked un-plated RC beam section (EI) c,0 = 0.38-4.7 (x10 12 ) Nmm 2 ;<br />

(10) width ratio of beam to plate α w = 1.0-4.8; (11) internal tensile reinforcement steel ratio ρ s = 0.44-5.40 %;<br />

(12) interfacial fracture energy G f = 0.25-0.88 Nmm/mm 2 ; and (13) interfacial bond strength τ f = 2.7-6.8<br />

N/mm 2 .<br />

<strong>The</strong> formulation of the present theoretical model includes the adhesive thickness t a , but the results are<br />

insensitive to the value selected. <strong>The</strong> predictions from the theoretical model presented in the rest of the paper do<br />

not include the effect of adhesive parameters. Not all concrete properties such as f t , f cu and cylinder strength f c<br />

were available for many test beams. In such cases, the relationships provided in BS 8110 (1997) and ACI 318-08<br />

(2008) have been used to calculate the missing properties from those available.. Compression reinforcement is<br />

ignored in all calculations.<br />

-172-

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