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Figure 3 Idealised bonded joint model<br />

Figure 4 Softening local bond-slip model<br />

Local Deformation (bond-slip) Model<br />

<strong>The</strong> actual local FRP-to-concrete bond-slip behaviour can be closely approximated by a bilinear bond-slip<br />

model (Yuan et al., 2004; Lu et al., 2005). However, Chen et al. (2007) have demonstrated that using a<br />

rigid-linear softening bond-slip model as shown in Figure 4 and retaining the fracture energy G f of a bilinear<br />

model leads to almost the same final predictions while significantly simplifying the calculation process. This<br />

linear softening bond-slip model is adopted in the present formulation where δ is the longitudinal slip at the<br />

interface, τ f is the peak bond stress (bond strength) and δ f is the ultimate slip when shear stress reduces to zero<br />

and the plate is considered to be debonded. Friction and aggregate interlock in the debonded area is ignored,<br />

leading to the absence of any residual shear strength after debonding. <strong>The</strong> bond-slip model in Figure 4<br />

represents a constitutive relation that can be described mathematically by the following equation:<br />

⎧ 0 when δ ( x)<br />

= 0<br />

⎪<br />

τ ( x)<br />

= f ( δ ) = ⎨<br />

τ f<br />

[ δ f − δ ( x)]<br />

when 0 < δ ( x)<br />

≤ δ<br />

(1)<br />

f<br />

⎪<br />

⎩δ<br />

f<br />

Failure Process and States of Interface<br />

Figure 5 shows the sequence of debonding propagation for a typical failure process and the corresponding<br />

interfacial shear stress distribution for the bonded joint shown in Figure 3. A point on the interface can be in a<br />

rigid, softening, or debonded state. Letters R (rigid), S (softening) and D (debonding) are used to describe the<br />

states of the interface from the plate end to mid-length. <strong>The</strong> entire interface is initially in a rigid state as the<br />

adopted local bond–slip model neglects elastic deformations. Softening initiates at the plate ends as soon as any<br />

loading is applied, resulting in micro-cracking and interfacial slip. <strong>The</strong> softening length of the interface a<br />

increases with increases in loading and reaches a d when debonding (macro-cracking) initiates at a slip of δ f . <strong>The</strong><br />

interface ahead of the softening front remains rigid and has no interfacial stresses in the present analysis (Figure<br />

5a-c), which makes the softening front abrupt. When the more accurate bilinear bond-slip model is used the<br />

actual stress distribution would be smooth ahead of the softening front throughout the whole loading process<br />

(Teng et al., 2006).<br />

Figure 5 Failure progression and interfacial shear stress distribution at different states of the bonded joint<br />

interface<br />

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