Research Article | Open Access

Jun Han, Hong Yuan, "Full Debonding Process of Adhesively Bonded Composite and Metallic Pipe Joints under Torsion", *Mathematical Problems in Engineering*, vol. 2016, Article ID 1237493, 13 pages, 2016. https://doi.org/10.1155/2016/1237493

# Full Debonding Process of Adhesively Bonded Composite and Metallic Pipe Joints under Torsion

**Academic Editor:**Alkis S. Paipetis

#### Abstract

Bonded joints are very common in many pipeline systems, in which the bond behavior of the joint interface is of crucial importance. This paper presents two analytical solutions for the debonding process of a pipe joint under torsion, assuming that the bond interface follows either an exponential softening bond-slip law or a simplified bilinear model. The solutions are general, applicable to composites and metallic and indeed other pipes. Based on the analytical solutions, the influences of the bond length and stiffness on the torque-displacement curve and ultimate load are investigated. The solutions can be used to explain the stress transfer mechanism, the interface crack propagation, and the ductility of the joint.

#### 1. Introduction

Pipes are very important structures in many industries such as energy, aerospace, and construction [1]. In consideration of whole weight, strength, and maintenance workload, it is commonly accepted that there should be less joints in a piping system at first design. Due to the limitation of transportation, installation, and rehabilitation, a joint seems essential for a large structure system containing different components. The limitations of the overall system performance usually come from the capacity of pipe joints. Therefore, the pipe joints play the most important role in the overall integrity of most piping systems [2].

For metallic piping system, the joints can be divided into three types: flange coupling, welding, and adhesive bonding. The first two traditional connections have the same shortage, such as high stress concentration. However, the adhesively bonded pipe joint can effectively lower the stress concentration [3]. While for composite piping system, connecting methods can be roughly summarized as adhesive bonding, butt-strap, heat-activated coupling, and flange coupling. The first three joints are considered as permanent joints and the same joint mechanism is found. Most composite flanges are connected to composite pipe with one of the three permanent methods. Therefore, a general adhesively bonded pipe joint analysis can be used to analyze all the three types of permanent composite pipe joints [4].

Adhesively bonded pipe joints provide uniform load transfer over the bonded area. Nevertheless, stress distribution in the bondline adhesive is nonuniform. Among all the possible loading configurations, such as tension, torsion, and bending, torsion is one of the fundamental types. Due to the difficulties in the analysis of interfacial behavior, few theoretical studies of mode III (torsion) interfacial fracture problems are available in the previous references.

Based on the mechanics of composite materials and the maximum strain failure criterion, an analytical and experimental study was conducted to investigate the elastic and failure behavior of composite laminated pipe under torsion [5]. Based on the general composite shell theory, Zou and Taheri [6] studied the stress concentrations at and near the end of the joints as functions of various parameters, such as the overlap length and thickness of the adhesive layer. Pugno and Surace [7] confirmed that the maximum stresses were attained at the ends of the adhesive and that the peak of maximum stress was reached at the end of the stiffer tube and does not tend to zero as the adhesive length approaches infinity. Cheng and Li [8] developed an adhesively bonded smart composite pipe joint system by integrating electromechanical coupling piezoelectric layers with the connection coupler.

Finite element results are good supplements to analytical research. A finite element analysis was used to calculate the residual thermal stresses generated by cooling down from the adhesive cure temperature and a nonlinear analysis incorporating the nonlinear adhesive behavior was performed [9]. Taheri et al. [10–13] developed a simple method for assessing the behavior of adhesively bonded tubular joints under torsion, based on a parametric study conducted by 2D and 3D finite element analysis. A finite difference method was utilized to solve the system of equilibrium equations and it was modeled as a separate 3D elastic body without the uniform stress assumption [14].

In all previous solutions, linear elastic properties are assumed for the entire pipe joints. The linear elastic behavior may be appropriate for the pipes themselves. While for the adhesive layer which is usually the weakest link in the bonded joints and often suffers from microcracking and local damage, nonlinear modeling may be necessary. When the crack tip experiences inelastic damage, the concepts based purely on the theory of elasticity are not valid. Therefore, different bond-slip models with softening region were proposed in the previous references, such as rigid-softening, bilinear, trapezoidal, and exponential models [15–24]. The main differences between these models lie in the shape of the traction-displacement response and the parameters used to describe that shape. Based on the existing models, some studies have also been presented to solve interfacial debonding problem for the adhesively bonded joints and closed-form solutions are obtained [25–36].

However, there are very few studies focusing on the analytical solution of full debonding process of pipe joints in the literatures. To the best of the authors’ knowledge, linear elastic properties are assumed for the entire pipe joints and very few researchers have taken interfacial softening and debonding into consideration. In the present study, there are two analytical solutions for the failure process of adhesively bonded interface, assuming that the bond interface follows either an exponential softening bond-slip law or a simplified bilinear model. The expressions for the interface slip and shear stress are derived for the different failure stages. The present research improves and clarifies the understanding of the interfacial debonding problem of bonded pipe joints under torsion. By modifying different shear modulus, the present results may be further extended to composite pipe joints, composite-metal pipe joints, or metallic pipe joints.

#### 2. Interface Model of Pipe Joint

##### 2.1. The Bonded Pipe Joint

Figure 1 shows a bonded pipe joint where two pipes (inner pipes) of the same diameter are joined together symmetrically with a pipe coupler (outer pipe) adhesively bonded to both pipes. Here the inner and outer pipes are defined as Pipes 1 and 2, respectively. Due to symmetry, only the right half of the pipe joint is considered. Let the length of the pipe coupler be 2*L*; the distance between the left end of Pipe 1 and the right end of the Pipe 2 is . Assuming that the pipe coupler is fully bonded with the inner pipes, the bond length between Pipe 1 and Pipe 2 is also for the right half of the pipe joint.

**(a) Cross section**

**(b) Side view**

**(c) Right half of the pipe joint**

##### 2.2. Assumptions

The following assumptions are made for the simplicity:(1)The adherents are homogeneous and linear elastic.(2)The adhesive is only under pure shear.(3)The pipe joint is under pure torsion which is resisted by the main pipe and coupler pipe; that is, the adhesive layer is assumed to only transmit shear stresses between Pipes 1 and 2, not contributing to any direct resistance to the torque.(4)Local bending effects in the pipe joint under the torsional load are neglected.

According to the classical torsion theory, the internal torsion and in Pipes 1 and 2 can be expressed, respectively, as follows:where subscripts 1 and 2 represent Pipes 1 and 2, respectively; is the shear modulus of the pipe material; is the first derivation of the rotational angle with respect to (Figure 1(c)); and is polar moment of inertia of the thin-walled pipes which can be expressed as follows:in which is the thickness of the pipes and is the radius the midline of the pipe cross sections (Figure 1(a)).

As the torque resultant in the soft and thin adhesive layer is ignored following assumption number 3 above, the equilibrium between external and internal torsion load in the pipe joint requires

##### 2.3. Governing Equations

Let the relative rotation between Pipes 1 and 2 at be as illustrated in Figure 2. Consider the torsional equilibrium of an infinitely small section in Pipe 1 (Figure 2):where is the interfacial shear stress in the circumferential direction and is the distance between the center of the pipe and midline of the adhesive layer which can be calculated byThe relative slip at the bond interface in the circumferential direction as can be found from the relative interfacial rotation :After substituting (1)–(4) into (5) and introducing the parameter , local bond strength , and interfacial fracture energy , we havewhereSubstituting (9) into (1), the relationship of and derivative of can be obtained:Equation (8) is the governing differential equation of the adhesively bonded joint. It can be solved once the local bond-slip model is given.

**(a)**

**(b)**

##### 2.4. Bond-Slip Model

As introduced before, researchers have proposed various bond-slip models. Experimental results indicate that the bilinear model which features a linear ascending branch followed by a linear descending branch provides a close approximation [31]. However, the use of linear softening law may lead to overestimating the mechanical properties of the joint. Therefore, a bond-slip law characterised by a linear phase, with slope , followed by an exponential softening branch is used [35]. And the results based on the two models are compared in order to provide better understanding of failure process.

For the exponential bond-slip law (Figure 3), the interfacial shear stress increases linearly with slip within the elastic range. The shear stress peaks at at which the value of the slip is denoted by . This stage is defined as elastic stage which is simplified as E. The interface enters the softening stage thereafter and the interfacial shear stress decays exponentially with the interfacial slip. This stage is defined as softening stage which is simplified as S. The mathematical expressions of the interfacial bond-slip law in Figure 3 areThe bilinear model (Figure 3) features a linear ascending branch followed by a linear descending branch to zero at a slip . This stage is defined as debonding stage which is simplified as D. It is usually treated as a simplified model of the exponential softening model. The results are usually very close if the fracture energy is the same for the two models [28]. This bond-slip model is mathematically described by the following:The positive coefficient in (12) characterises the exponential decay can be related to the slip parameters of the bilinear model by letting the interfacial fracture energy be equal for the two models:

#### 3. Debonding Process: The Exponential Model

##### 3.1. Elastic Stage

At small loads, there is no interfacial softening or debonding along the interface, so the entire length of the interface is in an elastic stress state. Substituting the first expression in (12) into (8) gives the following differential equation:whereThe inner pipe is free from stress at and subjected to a torque at , so the boundary conditions can be expressed as Based on these boundary conditions, the solution of (15) for the relative shear displacement and shear stress of the adhesive layer can be written in the formThe interfacial slip at the free end of the outer pipe (i.e., the value of at ) is defined as the displacement of the bonded joint for convenience and denoted by here. From (19), the torque-displacement is expressed as

##### 3.2. Elastic-Softening Stage

As the load increases, the interfacial slip reaches at and the bond enters the softening stage there. The whole interface is in an elastic-softening stage and the length of the softening region increases with the increase of torque . Substituting (12) into (8) gives (15) and the following equation for this stage:whereApplying the boundary conditions of (17) and (18) and the following continuity conditions:the solution for the elastic region of the interface (, i.e., ) is obtained asand the solution for the softening region of the interface (, i.e., ) is whereUsing (24), the constants and can be obtained asThe expression of slip at can be obtained from (26) asSubstituting (18) and (26) into (9) yieldsFor exponential model, by substituting (31) into (32), the expression of above can be rewritten asWhen is sufficiently large (approaches to infinity), (33) and (29) converge towherein which is the maximum possible value (the asymptotic value) can reach.

In bonded joints, there is usually an effective bond length , which is defined as the length beyond which an increase of the bond length the loading capacity of the bonded joint does not increase further [37]. For the exponential bond-slip law employed here, the loading (torque) capacity always increases with the bond length , but the rate of increase would be very small if is sufficiently large. Following Yuan et al. 2004, the effective bond length is defined here as the bond length which provides a resistance of 97% of . Following this definition, can be obtained from (30) and (33)–(35) aswhere

##### 3.3. Softening Stage

As the load increases, the peak of the shear stress moves towards the middle of the joint (). When the interfacial slip at reaches , the whole interface enters into softening. This stage is governed by (22) with the boundary conditions of (17) and (18). The solution for the interfacial slip and the shear stress of the bond interface can be obtained aswhere the constants and areSubstituting (18) and (38) into (9) yieldsThe expression of the slip at can be obtained from (38):

#### 4. Debonding Process: Bilinear Model

##### 4.1. Elastic Stage

The solution for the elastic stage is the same as that in Section 3.1.

##### 4.2. Elastic-Softening Stage

As the load increases, softening commences at once the shear stress reaches there. increases as the softening length increases. Substituting the first or the second expression in (13) into (8) gives (15) and the following:whereWith the same boundary and continuity conditions as in Section 3.2, the solution for the elastic region of the interface (, i.e., ) is the same as that in Section 3.2, and the solution for the softening region of the interface (, i.e., ) is given by Substituting (18) and (45) into (9) yieldsThe expression of the slip at can be obtained from (45):During this stage, the torque-displacement curve can be determined from (47) and (48). When the interfacial slip increases to at but the slip at is less than , the interface enters into elastic-softening-debonding stage. When the slip at reaches and the slip at is less than , the interface enters into softening stage. Therefore, there exists a critical bond length to distinguish the failure process:When the bond length is larger than , the interface enters into elastic-softening-debonding stage. When the bond length is shorter than , the interface enters into softening stage. For the bilinear model, reaches its maximum when the derivative of (47) with respect to equals zero. Therefore, at the ultimate load can be found from the following relationship:Substituting (50) into (47) yieldsIt can be shown from (50) and (51) that approaches the following value when is large:Following the same definition in (36) and considering that , the effective bond length when 0.97 is reached can be obtained from (50)–(52) to givewhere

##### 4.3. Joints with

###### 4.3.1. Elastic-Softening-Debonding Stage

If , as the torque increases, the interfacial slip at reaches which represents the initiation of debonding (or macrocracking or fracture). Because at the initiation of debonding, the corresponding value of , denoted by , can be obtained from (48) as Debonding propagates hereafter and the peak shear stress moves towards . Assuming that the debonded length of the interface starting at is , (25) and (45)-(46) are still valid if replacing by . Therefore, the torque-displacement relationship can be written asAs the interfacial shear stress at is zero, the following relationship can be obtained:Substituting (58) into (56) yields the following simplified form:At the end of this stage, the softening-debonding stage starts when . Substituting this into (58) yieldsMoreover, by substituting (60) into (59), (59) can be written as

###### 4.3.2. Softening-Debonding Stage

This stage is governed by (43) with the boundary conditions of (17) and Based on the boundary conditions, the following solution can thus be found by solving the governing equation (43):From (64) it is seen that the length of softening zone remains constant during this stage. The torque-displacement relationship can be obtained by solving (8) for the case of or directly displacement superposition along the bonded joint:

##### 4.4. For Joints with

###### 4.4.1. Softening Stage

As the load increases, the shear stress peak moves towards . When the interfacial slip at reaches , the whole interface enters into the softening zone. This stage is governed by (43) with boundary conditions of (17) and (18). Based on the boundary conditions, the following solution can be obtained by solving the governing equation (43):The expression of the slip at can be obtained from (68): As shown in the bond-slip law, when the interface slip reaches , debonding occurs. Substituting this condition into (70), the external load reduces to zero. Hence, it can be concluded that the softening stage here always represents the ultimate failure stage.

#### 5. Numerical Simulations

The results of an adhesively bonded metal-composite pipe joint are presented here. The typical inner diameter and thickness are assumed to be 300 and 10 mm for the metallic main pipe, respectively. And the inner diameter and thickness of the composite coupler are assumed to be 320.4 and 5 mm, respectively. For metallic main pipe, the mechanical properties are chosen as GPa, GPa, and . For composite coupler, the mechanical properties are chosen as GPa, GPa, GPa, and . The parameters for interfacial bond-slip laws are identified as MPa, mm, and mm.

According to the material properties and geometry parameters given above, the critical bond length for bilinear model can be calculated as mm. Therefore, bond lengths of 20 and 80 mm are chosen.

##### 5.1. Load-Displacement Curves

###### 5.1.1. Load-Displacement Curves for Exponential Model

The load-displacement curve for exponential model is shown in Figure 4. OA, AB, and BC are elastic, elastic-softening, and softening stages, respectively.

**(a) mm**

**(b) mm**

###### 5.1.2. Load-Displacement Curves for Bilinear Model

When the bond length is shorter than , take mm and the load-displacement curve is shown in Figure 5(a). OA, AB, and BC are elastic, elastic-softening, and softening stages, respectively. When the bong length is longer than , take mm and the load-displacement curve is shown in Figure 5(b). OA, AB, BC, and CD are elastic, elastic-softening, elastic-softening-debonding, and softening-debonding stages, respectively.

**(a) mm**

**(b) mm**

##### 5.2. Shear Stress Distribution

The shear stress distribution for exponential model is shown in Figure 6. When the load is small, the interfacial shear stress at loaded end is less than peak stress and the interface is in an elastic stage. When the interfacial shear stress reaches peak stress at loaded end, the interface enters into elastic-softening stage. As load increases, the peak stress moves from loaded end to unloaded end and the length of softening zone increases. When the interfacial shear stress at unloaded end reaches peak stress, the interface enters into softening stage. For simplified legend, the critical status is defined as the end. For example, the critical status between elastic stage and elastic-softening stage is defined as E-end in Figure 6(a). And the following abbreviations are the same.

**(a) mm**

**(b) mm**

The shear stress distribution of mm and mm for bilinear model are shown in Figures 7(a) and 7(b), respectively. When the load is small, the interfacial shear stress at loaded end is less than peak stress and the interface is an in elastic stage. When the interfacial shear stress reaches peak stress at loaded end, the interface enters into elastic-softening stage. As load increases, the peak stress moves from loaded end to unloaded end and the length of softening zone increases. When the interfacial shear stress at unloaded end reaches peak stress while , the interface enters into softening stage shown as in Figure 7(a). When and the interfacial shear stress at unloaded end is less than peak stress, then the interface enters into elastic-softening-debonding stage as shown in Figure 7(b). The length of debonding zone increases as the peak stress moves to unloaded end. When the interfacial shear stress at unloaded end reaches peak stress, the interface enters into softening-debonding stage.

**(a) mm**

**(b) mm**

##### 5.3. Parametric Study

Figure 8(a) shows the influence for different bond lengths of bilinear model on the load-displacement curves. From the figure, the significant influence for bond length on the curves could be observed. In the range of the effective bond length, as the bond length increases, not only the interface failure processes change but also the ultimate load and interfacial slip. Specifically, the increase of the bond length can increase damage ductility. However, when the bond length reaches a certain length (effective bond length), the ultimate load will hardly change. Figure 8(b) shows the influence for different bond lengths of exponential model on the load-displacement curves. From the figure we know that as the bond length increases the ultimate load increases. But the failure processes are all the same. Namely, the increase of the bond length can also increase damage ductility.

**(a) Bilinear model**

**(b) Exponential model**

Figure 9 shows the comparison of the load-displacement curves between the two models for different bond lengths. The load-displacement curves are different when a softening area exists. In addition, since there is no debonding situation in the exponential model, the displacement can increase unlimitedly, with this being different from bilinear model in which the slip would approach . From the figures, the load increases faster in the bilinear model as the bond lengths increases. However, when the bond length is long, the ultimate loads between the two models seem no more different.

**(a) mm**

**(b) mm**

**(c) mm**

**(d) mm**

Figure 10 shows the load-displacement curves for different ratios of torsion stiffness (). From the figures we can see that as the ratio increases, the ultimate load increases but the slip decreases; namely, the ductility reduces. Moreover, the larger the ratio is, the smaller the change magnitude will be.

**(a) Bilinear model**

**(b) Exponential model**

Figure 11 shows the relationship of effective bond length and ratio of torsion stiffness. From the figure we can see that a stiffer coupler leads to a longer effective bond length. But as the ratio is getting larger, the effective bond length does not obviously increase. As the ratio increases, the effective bond lengths of two models have the similar trend, but the effective bond length of exponential model is longer than that of bilinear model.

Through the numerical computation, the ultimate load of exponential and bilinear models for different bond lengths could be obtained. Figure 12 shows the ultimate load for different bond lengths. From the figure we can see that, for bilinear model, when the bond length is short, the ultimate load increases significantly with the bond length. When the bond length is long, the ultimate load stays essentially unchanged. For the exponential model, when the bond length is short, the trend is similar to the bilinear model, but the ultimate load is relatively smaller. Both models have the same ultimate load when the bond length is relatively long.

#### 6. Conclusions

On the basis of fully understanding the mechanical behavior of the joint interface, this paper gives a further understanding of the key factors of interfacial debonding. By modifying different shear moduli, the present results may be further extended to composite pipe joints, composite-metal pipe joints, or metallic pipe joints. Based on the derivations in the current study, some important conclusions are summarized as follows:(1)Through the nonlinear fracture mechanics, the analytical expressions of the interfacial shear stress and the load-displacement relationship at loaded end of pipe joints under torsion loads could be gotten. Thus the shear stress propagation and the debonding progress of the whole interface for different bond lengths could be predicted.(2)The influences of different bond length on the load-displacement curve and the ultimate load are studied through the analytical solutions. The stress transfer mechanism, the interface crack propagation, and the ductility behavior of the joints could be explained.

#### Competing Interests

The authors declare that they have no competing interests.

#### Acknowledgments

The authors gratefully acknowledge the financial support provided by the Science and Technology Scheme of Guangzhou City (201510010013), Science and Technology Scheme of Guangdong Province (2012A030200003), and the Natural Science Foundation of China (National Key Project no. 11032005).

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Copyright © 2016 Jun Han and Hong Yuan. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.