Theoretical models

An analytical formulation for modelling the behaviour of the FRP-to-concrete adhesive interfaces is presented and discussed in the present section. The behaviour of FRP-to – concrete joints in the linear range is examined in the first subsection. Then, the aspects more directly related at the ultimate behaviour are addressed in the second one.

1.1 A general analytical model: formulation in the linear range

A simplified model is formulated in the present section with the aim of simulating the behaviour of FRP laminates bonded on concrete and tested in pull-out, simulating how both the in-plane (namely, "slip") and out-of-plane displacement components develop throughout the FRP length. It is based on the following assumptions:

– the FRP strip is simulated as a Bernoulli beam;

– the adhesive layer is modelled as a bi-dimensional elastic domain in plane deformations.

Theoretical models Theoretical models

The generalized forces N, V, M applied on the transverse section of the strip at the abscissa z and the interface stresses (shear т and normal a, respectively) are represented in Fig. 2. The following equilibrium equations can be stated between those force and stress components:

Подпись: (3)dM + Tff – v = 0

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dz f 2

Fig. 2. Forces on the segmental FRP strip element

The parameters v, w and ф completely describe the displacement field of the strip and the following compatibility equations relate them to the axial strain є and the curvature X (Fig. 3):

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(4)

 

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(5)

 

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(6)

 

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Fig. 3. Displacements components of the segmental element

 

The interface slip s, namely the axial displacement at the bottom chord of the strip transverse section, can be also related to the displacement components represented in Fig. 3:

 

s = w + – Ф. (7)

Finally, the usual (generalized) stress-strain relationships can be introduced for the strip modelled as a Bernoulli beam:

 

N = EAf s = Efbftf s

 

(8)

 

b 13

M = EIf X = Ef-^ X, (9)

where EAf and EIf are respectively the axial and flexural stiffnesses which can be assumed for the strip transverse section. Based on the second assumptions reported at the beginning of section 2.1, The following equilibrium equations can be written for the infinitesimal 2D element of resin within the adhesive layer (Fig. 4):

 

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(10)

 

дт

yz

^ dy a

 

where ya and za are the Cartesian coordinates of the infinitesimal areal element of resin.

 

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Fig. 4. General plane stress-state for an infinitesimal element of the adhesive layer

 

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The corresponding strain measures can be expressed as functions of the displacement field va(ya, za) e wa(ya, za) within the adhesive layer:

Подпись: (11)_dVa dy a dwa_

Theoretical models Подпись: dw dy a

dza

where ya and za are the Cartesian coordinates of the infinitesimal areal element of resin. Finally, the following elastic relationships can be stated between stresses and strains:

8yy = ET yy -Va ‘CTzz ]

‘ 8zz = ET ‘l>zz Va -°yy ] , (12)

Y yz =G = 2-(1 +Va )-E-

where Ea and Ga are the elastic properties of the adhesive layer. In this formulation, it connects the FRP laminates to a stiff substrate representing the concrete element. The upper bound of this layer is connected to that strip and some compatibility equations should be written for introducing this physical constraint into the mathematical model. Thus, the three equations (10)-(12) can be worked out for deriving a relationship between the displacement components va(0,za) and wa(0,za) and the corresponding stress components ayy(0,za) and Txy(0,za). A key assumption can be introduced for simplifying the analytical expressions of the interface stresses, considering a constant value of the shear stress throughout the adhesive thickness (Rabinovich & Frostig, 2000):

Tyz =Ta(za) =Ta(z). (13)

Consequently, the second one of the two equations in (10) leads to the following simplification in terms of the normal stress in longitudinal direction:

^ = 0 ^^zz =f1 (ya =0 . (14)

The last implication derives by the assumption of zero axial stress on the initial section of the layer adhesive.

Further simplifications can be introduced looking after the first equations in (10) and introducing therein the stress-strain relationship and the compatibility equation within the adhesive layer:

and

 

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(17)

 

– v (z, +grliai у,

v a/ E dz 2 E }a

 

and the value of the unknown function g1 can be finally derived by imposing zero value to the displacement at the bottom interface (ya=ta):

 

hz)–! ■ + gllfal t = 0 ,

1 a} Ea dz 2 Ea a

 

(18)

 

/ 4 Ea, , dia ta

gl (za )– – v (za )+

 

(19)

 

Consequently, the following explicit expressions can be written for ayy, eyy and va described in (15), (16) and (17), by introducing the expression of g1 given by equation (19):

 

E (y z)= dTa■(ta -2ya V1Ы

yy a) dz I 2 ■ E I t

 

(20)

 

,(ya, za )-Ea-S„ (y„z. )-^ )- ^(z, ) ,

 

(21)

 

va (y„za )-v(za )-(1 – ^)+ ^) ya ■

Shear strain and stress can be related according to the following relationship:

 

(22)

 

(23)

 

Yyz (za )=-£-

 

and, considering the compatibility equation involving shear strains, further transformations can be carried out by introducing the compatibility equation in (11):

 

Y (z)-^ + ^ .

yzUj dza dy a

 

(24)

 

The first derivative of the longitudinal displacement wa inside the adhesive layer can be written as follows:

 

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dw.

дУа

 

dVa

dza

 

L dl.1 1 – Ll- lii.( ta – Уа dz I ta ) dz2 I 2Ea

 

(25)

 

Подпись: wa (a,za) = Подпись: >(t -y )+ — •( *a-y + ^-1 + 1^. 1 a Уаі dz I 2 2t I dz2 Theoretical models Theoretical models

and the corresponding function wa can be derived by integrating eq. (25) and introducing a zero-displacement condition for ya=ta (namely, at the bottom of the adhesive layer):

The above relationship can be utilized for deriving the expression of the axial displacements beneath the laminate (ya=0), corresponding to the slip at the interface s(z):

Подпись: wa(0,za) = s(z)Подпись:Theoretical models(27)

Theoretical models Theoretical models Theoretical models Подпись: CT (y ,z ) = E . s (y ,z ) = E yyJaf a) a yyJaf a) a

as well as equation (22) can be utilized for recognizing that the corresponding transverse component va(0,za=z) is equal to v(z):

Thus, the rotation field 9(z) of the laminate element can be easily defined through equation (6) and the generalized strain fields can be determined by means of equation (4) and (5).

Подпись: G d3v G — .-Г-Г + ——. t. 2 dz3 12Ea ' Подпись: (30)
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Подпись: Eftfta Подпись: dla dz2

The above equations can be finally combined for deriving a unique differential equation in terms of interface shear stresses. A first equation can be obtained by differentiating eq. (7) and introducing (4), (6) and (8). After a further differentiation and introducing the definition of interface slip provided by eq. (27), the following differential relationship between the shear stress and the transverse displacements can be obtained:

Another relationship is obtained by differentiating equation (3) and introducing equation (2), (5), (6) and (9) for expressing both the bending moment and the shear force in terms of transverse displacements and interface (shear and normal) stresses. The final expression of an equation in terms of tf and v (and their derivatives) can be obtained introducing equation (29):

Подпись:bf (tf + ta ) . djL – Efbftf3 . dv – Eabf. v = 0 2 dz 12 dz4 ta

Ga

• T – d2 Ta +f ta2 + tatf + tf2 Ї

Ga

d4Ta

E t t 3

n fLaLf

d6T EfG t 3tf3

a | f a a f

d8T

•di = 0. (32) dz

Eftfta

a dz2 ^ 3 6 12 J

Ea

dz4

12 • Ea

dz6 144 • Ea2

Подпись: 3 • t v = І Подпись: + 3 • tatf + f 6E„ Подпись: dz Подпись: Eftatf3 ^ d 6EG dz3 Подпись: Efta3tf3 ^ dr. 72 • E a2 dz5 Подпись: (33)

Finally, an expression of the displacement function v as a function of the interface shear stresses can be derived by solving equation (31) and introducing the (30):

Eight boundary conditions are needed for the problem at hand and they can be symbolically written as follows:

Ta|z=0 = 0 , Ta|z=L = 0 ,

(34)

N(0) , N(L)

(35)

0 EfAf ‘ lz=L EfAf ‘

О

II

hJ

Y

О

II

о

Y

(36)

_<

II

О

_<

II

О

(37)

Подпись: Fig. 5. Possible distributions of interface shear stresses throughout the adhesive interface

Typical solutions of the problem described by equation (32) and the boundary conditions (34)-(37) are represented in figures 5 and 6, in terms of shear and normal stresses respectively. In both graphs, the interface stress components are divided by the average shear stress Tm=F/bfL and the abscissa are reported in non-dimensional form as z = rnz.

The results of the analysis carried out by means of this model are completely controlled by the following non-dimensional parameters:

In t k t.

Eft a Ea ‘

(39)

G k

Ea kv, a ‘

(40)

ta

tf ‘

(41)

Подпись: CTyy/Tm rn L=10 Fig. 6. Possible distributions of interface normal stresses throughout the adhesive interface