Research Article  Open Access
Hui Liu, Jun Hu, Guohui Li, Guangying Mo, "Numerical Analysis for UShaped ThinWalled Structure Reinforced Timber Beam Based on ThinLayer Beam Theory", Advances in Civil Engineering, vol. 2019, Article ID 7513645, 10 pages, 2019. https://doi.org/10.1155/2019/7513645
Numerical Analysis for UShaped ThinWalled Structure Reinforced Timber Beam Based on ThinLayer Beam Theory
Abstract
This paper presents a theoretical model, taking into account the shear deformation subjected to the influence of Ushaped member by geometric parameters as flange height based on thinlayer beam theory, to analyze the structural bending behavior of Ushaped member reinforced timber composite beams, and the feasible design forms of Usection have been pointed out. The algorithm for this composite beam is the most practical and effective method to meet the accurate solution. The formulas for the common forms of Usection are presented. It aims to develop a rational engineering approach. The proposed model has been validated by comparing the results obtained in the present analysis with experimental results and finite element analysis. Furthermore, the results suggested that the value of flange height can be onefifth the beam height based on the present analysis by comparison of two types of beams. And it is shown that the model provided here correlates consistently and satisfactorily with a wide range of timber beams reinforced by a thinwalled structure such as steel or aluminum alloy sheet bonded to their tension faces.
1. Introduction
Timber structures' natural features are attractive in applied engineering. As timber structures are brittle materials, different reinforcement techniques can be adopted for avoiding easily damageable parts of the building, such as concrete, steel, and FRP used for timber beams and sandwich beams [1–7]. However, the reinforcements often make beam confront stiffness degradation and bonded layers separation due to interlay slip associated with flexibility and deformation of connectors [8–10]. Shear stress plays a significant role in bending strength of composite beam as discussed in many research studies, and some numerical methods to estimate it have been established [5, 9, 11–16]. Malek et al. proposed that shear stress in the interface of concrete and plate beams leads to flexural cracks compared to other items including tensile stress, analytically given by unique definition from highorder ordinary differential equations applied to the concrete beam [17].
A system of Ushaped member provided to reinforce timber beam shows a ductile behavior with respect to the plate [18–20]. The materials such as steel, aluminum, cement asbestos, and GFRP adopted are all available [21]. And, a Ushaped member using GFRP fabric was first discussed by Theakston [22].
Many publications [11, 12, 23, 24] reported that using the Ushaped member can effectively improve the maximum bending capacity. Rescalvo et al. [19, 20] presented data to demonstrate the benefits in flexural strength, and stiffness of timber improved due to the Ushaped member [19, 20]. The same results were obtained with applications of the Ushaped member reinforced LVL beam in a study by Subhani et al. [25]. The improvements of 15.94% and 16.10% in flexural strength and stiffness, respectively, were observed from the experiment comparison [25].
Until now, various multilayered composite beam theories have been developed by many authors [26–31]. Several exact mathematical solutions were established based on the concepts of Timoshenko beam theory, including displacementbased theory, firstorder shear deformation theory, and higherorder theory [32]. Alternatively, Edward and Thomas [2] developed a plate theory to reflect the mechanical behavior of thinlayer composite structures shown by the model without externally imposed shear force in the cross section of thin layer [2]. Based on the plate theory, Hussein has completed analytical and experimental studies that give a calculated simulation focussed on the influence of the adhesive [9]. Recently, the plate theory was used in the thinwalled steel to strengthen timber composite structures [33].
The current study for simulating the flexural behavior of the Ushaped member reinforced composite beam mainly adopted the method calculating the strain relation based on the Bernoulli’s principle [6, 18]. Subhani et al. [25] presented an algorithm to be more accurate with a nonlinear model [25]. However, both simulations related to the experiment were given by available literature, and this method works by neglecting the transverse shear strains completely defined by the model considering the balance of compressive and tensile forces.
In this paper, the mechanical behavior of the timber beam was reinforced with the Ushaped member as the thinwalled plate made in the steel plate or aluminum alloy strip unlike the composite beam reinforced by two parts fully glued. The method estimating the bending capacity cannot adequate to fit the principle, and so the research was presented to analysis based on thinlayer beam theory. The steel plate or aluminum alloy is widely used in engineering; notwithstanding that FRP has advantages of high tensile strength with easily moldable properties, but the premature catastrophic failure of FPR could easily occur by wood splinters when used in the composite beam [23]. This paper will show the bending capacity of Ushaped thinwalled member reinforced timber beam by the plate theory. The approach will be prescribed and compared with the thicker composite beams [34–36]. It will be applied to reflect correctly the potential function of U shape in terms of bending capacity and stiffness with respect to the layer slip or shear displacement.
2. Analytical Models
Several exact mathematical analytical solutions of displacement and stress for composite beams with different combinations have been presented in the professional literature.
In general, two different approaches have been adopted to study composite beams: thicklayer beam theories and thinlayer beam theories. In thicker layer beam theory approaches, researchers wanted to overcome connect issues and explain the behaviors of composite structures more accurately, which is known by the beam being inherently subjected to transverse shear between the sections. Girhammar et al. [36] presented the internal actions and established the first and secondorder models with respect to the slip effect deflection. Nie et al. [37], based on the uniform loading, have proposed the stiffness reduction method in deflection analysis. Girhammar and Gopu [38] presented an exact procedure using two secondorder ordinary differential equations in terms of interlayer slip for calculating deflection of composite beams [37, 38]. In thinlayer beam theory approaches, mainly known as sandwich construction in the form of thin face panels, the analytical model and solution to estimate the effective mechanical properties of adhesives are unavoidable. Theoretical studies about the bending capacity subjected to various working loads have been given, and the research on nonrigid adhesive applied the plate theory developed by Hussein [1, 2, 9, 39, 40]. In fact, the approaches were initiated by the Kirchhoff–Love plate theory.
2.1. Mechanical Model
Due to the highly nonlinear behavior of timber joints, fasteners such as screws are potentially ductile in nature compared with glued joints and carpenter joints. Under compressive stresses, steel or aluminum alloy plate used for reinforced timber can be loaded far over its elastic limit and be able to deform in a distinctly plastic manner, especially the aluminum alloy performs corresponding with timber in terms of mechanism properties behavior.
For a thinlayer beam, the basic structural principle is that the facings act together to resisting moment counteracting the external imposed bending moment. Figure 1 depicts the isolation unit which shows that moment is constant through the thickness, and the core resists the shear stresses set up by the external loads. In Figure 1, are external loads, represents the bonding force between two sections, and is the value of shear owing to the facings act. Then, and are bending moment and tensile with isolation units. This kind of theory's model defines a structural sandwich covered by a thin sheet as a major contributor to tensile strength [41]. The isolation unit of thicklayer beam model as two isolated beams connected together by the adhesive is shown in Figure 2. Especially, the moment is different from by each part, but in Figure 1, the value of moment is about equal to with the thin layer.
For verifying the reliability of the design models of Ushaped plate reinforced timber beam, De la Rosa et al. have analyzed them using the transformed section method and the section conditions of equilibrium. De la Rosa et al. have presented theory based on the formula derived from stressstrain relationship of materials and the conditions of equilibrium with Bernoulli's principle. However, the estimate method was checked with the results obtained experimentally on reinforcement of FPR [18]. A different calculation method to simulate the Ushaped plate as reinforcement based on Shen’s work was presented, which is translated from the thicklayer beam theory and displayed based on adding the contribution of Usection strength to the element without strengthening, while the reinforcement material is steel plate in concrete beam [42]. U section is nonrigid adhesive on the tension face of the timber beam and owed the property of selfsupporting due to the unwrapped form and is also weaker in free edge under compressive force caused by the nonbonded adhesive flange of the U section in the lateral sides of the beam. Thus, the thinlayer beam may be necessary and sufficient to reflect the mechanical simulation of timber beam assembled by a Ushaped member in such kinds of material properties.
The formulation of the planar twolayer composite beam model uses the following assumptions: (1) the materials are orthotropic and linear elastic; (2) the Ushaped layer is symmetrical with respect to the plane of deformation and forces, and the layers are continuously connected only on the bottom of beam; and (3) the faces are thin in comparison with the core depth. This implies that the flexural rigidity of each face about its own middle surface is negligible, and consequently, the inplane stresses resisted by each skin are uniformly distributed across its thickness.
A distribution of Ushaped reinforcement is shown in Figure 3, which is fabricated by attaching timber to the web part of the Usection. The tensile force obviously generates from the connection between the surfaces of two parts. There are loads which result in bending with the effect of Usection warping, such as the shear stress between interlayers and the friction both on web and flange between the timbers and due to the shear displacement lead by the distortion that induces influence of the extent to which the plane sections remain oriented after bending.
2.2. Shear Displacement Analysis
An interlayer slip often develops if it is up to sufficient magnitude and therefore affects significantly the deformation and the stress distribution of the composite system. The plate assembled to timber beam having finite stiffness, because of distortion, contributes most to any unequal displacement of the plate and the lower face of the timber with interlayer slip under edgewise loads, as assumed in the model of Figure 4. The U section can not only hold off vertical tensile force P by connectors but also prevent the shear slip by the strengthening function of the flange. The friction horizontally distributed between plane flange and timber functionally resists partial interaction especially contributed to the force induced by edgewise warping, works together with reinforcement of connector at the bottom of the beam and with extrusion forces generated by the Usection, and plays the role of supplementary stress as well as friction vertically transferred by lateral interfaces.
3. Numerical Analysis
3.1. UShape Simulation Based on the ThinLayer Beam Theory
The elemental longitudinal section of a prismatic rectangular beam integrates with the Ushaped member under uniformly distributed load along a beam of length L and the total load given by Q. The distance between centroids of principal momentcarrying member h is shown in Figure 3. Considering the interlayer effects of shear bonding stiffness, defined as α, the secondorder differential equation [2] for the shear stress τ and deflection ω can be expressed as follows:where is the stiffness of all beam parts as if unglued and is the stiffness of composite beam if parts were glued together; the bending moment and shear load at a point located at distance x from a reaction are calculated as follows:
Substituting the expression for given in equation (4) into equation (2),
Constants of integration A and B are evaluated using the following boundary conditions; the boundary conditions are evaluated at and , where the length of 0 represents the ends of the beam and half of span represents the midspan of the beam. At points, or , can be shown by Equation (6):
Using the above boundary conditions, the following expressions for A and B can be obtained:
By substituting equations (7) and (8) into equation (5), the shear stress is expressed as
Due to the strain obtained in equation (9), the maximum deflection ω_{max} which under the total compressive Q with integration and evaluation of integration constants leads towherewhere is defined as shear modulus of adhesive or shear load per unit span length to cause unit slip.
In a similar manner, an expression for the midspan deflection fulfills other load position conditions that can be obtained, and the function obtained to represent the constant of integration is given bywhere is the load position.
Based on the graphs [2, 9], and by taking α into numerical evaluation for the parametric study, always increase inducing values of decrease when remains increasing proportionally.
A parameter which represented constant coefficient under different forms of load distribution is used in the various expressions in the interests of brevity. The results can be simplified according to equations (10), (16), and (17) with a function ∆κ which reflected reactions between the interfaces of the elements.
The thinlayer beams in equation (10) describe the result that can be represented through a function W as
The function is denoted as equation (17) due to different models in terms of the different loading modes:
For the first case in equation (16),where Δκ is calculated in the term under the offset point load.
It can be seen that parameter in equations (17), (22), and (23) significantly determines the function contributing to midspan deflection.
3.2. ThickLayer Beam
This method is to simulate the composite beam by secondorder shear deformation theory presented [43]. It assumes that the displacement u has a cubic variation through the thickness of each section, with moment differential equations of equilibrium for beams considering corrected shear force with respect to slip effects. The resulting equations for midspan deflection of the beam under uniformly distributed load are given as follows:
Likewise, under offset point, the load is given asin all of whichand the thicklayer beams in equations (18) and (19) can be simplified by
For the second case in equation (21),where Δκ2 is calculated in the term under the uniformly distributed load:
In the two cases, the general expressions for displacement are presented, all for a simply supported beam. It can be seen that the algorithms formed in two cases are different shown by the relationships of with fundamental function . The thinlayer theory’s simplified expression of contains the as argument in function calls. The thicklayer theory’s expression contains the ∆κ representing the intercept with respect to . Equation (26) can be obtained bywhere is the bending moment, is the axial force, is the external shear force, represents each part, and is the height of the beam. When neglecting external shear force, the method assumes to be applied to simulate the thinlayer model by equations (24)–(26); the results to be calculated are
It can be seen that the both sides of equation (27), a set of axial interface force, commensurate with extensional stiffness of each parts leading to balancing themselves; that is, the equation obtained a solution that has no value to concern in this way. It means that the equation for two cases could not be interchanged for calculation of composite beam in two forms. Numerical and mechanical analysis are done to illustrate the effectiveness and efficiency of adopting thin layer beam theory for numerical analysis of the Ushaped member composite timber beam without losing any generality, there are insignificant effects to interlayer shears, but the face normal stress presents greater sensitivity to the variation of bond stiffness value as researches [9, 17] have shown. In principle, increased bond stiffness induces increased face normal stress. The same function implies that adopting expressions is reasonable due to the absence of loads which were induced by flange assuming an advantage in the remaining composite beam bearing the load together herein.
3.3. Finite Element Analysis
This work was not aimed at identifying the relationship of load and slip deflection for the composite structure but rather to analyze the flexural behavior strengthened by the Ushaped member provided. Here, the loaddisplacement plot for models of bending capacity simulation with regard to the height of flange was obtained with two types of the composite beam containing two kinds of materials for Ushaped member: one is steel and the other is aluminum alloy. The finite element analysis based on experiments shown in Figure 6 will be discussed further.
(a)
(b)
The Ushaped member in steel is an SUOT beam according to data of L1 [44], while the AUT beam is an aluminum alloy Ushaped sheettimber composite beam; the main mechanical properties of aluminum alloy are ƒ_{t} = 206 MPa, E = 0.7 × 10^{5} MPa, and γ = 0.34; the values of timber according to the test of Pseudotsuga menziesii wood are ƒ_{c} = 28.32 MPa, E = 11003 MPa, and γ = 0.3, where E is the elastic modulus, γ is the Poisson ratio, ƒ_{t} is the yield strength, and ƒ_{c} is the compressive strength. Timber simulation based on the trilinear strainsoftening constitutive model [45] and the damaged plasticity model was used to describe the behavior of the aluminum alloy. The finite element analysis carried out the AUT and SUOT; it also found the modeling method to be effective with which the models were calibrated against the experimental loaddeflection data. Then, simulations have done to keep the mechanical properties same and change the flange height of AUT to 0, 5 mm, 13 mm, 26 mm, 39 mm, 52 mm, and 65 mm and 0, 5 mm, 15 mm, 30 mm, and 45 mm for flange height of SUOT.
It can be seen that the loaddisplacement response of AUT beam simulated by ANSYS in Figure 7 suggested that increasing the flange height of Ushaped member has a significant influence on the stiffness as shown by the decrease trend of displacement at midspan beam with the same load condition. The fitted curves (e.g., Figures 8 and 9) slightly overestimate both AUT beam and SUOT beam, and the reduction in maximum displacement and compressive stress indicates providing higher bearing capacity. The curves indicate the flange height of the Ushape member adopted 1/5 beam height that is available, and it is obvious that the carrying capacity would not improve when the height is above 1/5 beam height.
Comparing the carbon fiberreinforced timber beam, an increase in its carrying capacity is likely to be produced which proved the good behavior of a Ushaped member with fiberreinforced plastic as well [46–48]. The study [18] does not show the relationship of flange height and carrying capacity, but it can be found that reducing the flange height would be superior for carrying capacity according to the equilibrium and the structure analysis sketch.
4. Experiment of Timber Beams Assembled by UShaped Member
To check its effectiveness, the thinlayer beam calculation model is compared with the results of experiments on a Ushaped thinwalled striptimber composite beam. SUOT [44] and AUT were analyzed by using both the methods described in this paper and the finite element method. From the data, results of two kinds of timber beam are used for discussion here. The general view of SUOT and AUT is shown in Figure 6. Specimens made of timber with identical characteristics to the beams in terms of timber origin, quality, drying time, and moisture content were tested. In this case, loads and displacements were obtained, and with this information, the corresponding stress/strain diagrams were traced. The values of the elasticity modulus, maximum compression strength, and Poisson’s ratio were presented in Section 3.3.
The tests were conducted at two points of load application, and the displacement of the beams at midspan and at the supports was measured by dial gauges to an accuracy of 0.01 mm. Investigating the details of behavior of the effective loaddeflection response of the components was carrying out by several fullscale bending tests in experiments; there was relatively ductile behavior exhibited in loaddeflection curves, and the simulation showed very similar results compared to test results. With regard to the load bearing capacity observed in the results for identical models, the effectiveness of parameters used to predict the behavior of beams with different heights of Ushaped flange provided an adequate estimate.
The experimental results are shown in Figures 10 and 11, and comparison of displacement at midspan between calculation and test or simulation using thin layer theory is listed in Table 1. The data obtained correspond to the loads applied and to the vertical midspan displacements experienced by the beams where the load is applied, up to fracture. With these data, loaddisplacement graphs of the beam were obtained as shown in Figure 7, and the graphs of mean values of the strain under ultimate fracture load are shown in Figures 10 and 11. Figure 10 shows the deformation behavior and strain distribution along the beam, in which the values obtained for the Ushaped member ultimate tensile stress corresponded to coinciding with the maximum compressive stress of timber reached by the reinforcing U shape member. When ultimate load is reached, the tensile stress coinciding with the maximum compressive stress would reach the ultimate point. The structure exhibited a ductile behavior. The loadstrain relationship in Figure 11 presented the longitudinal strain along the loading procedure. The results show that there is no occurrence of separation.
(a)
(b)
(a)
(b)

It can be seen from Table 1 that the results have shown the ultimate load and corresponding ultimate midspan deflection with calculations by equation (12) and the exact value of simulations. The values of ultimate load indicate fracture load, which was adopted from the experimental data in [49], and conclusion by Pellicane [50] can be applied to the material of aluminum alloy when using the algorithm. In this paper, the K value is 0.3482 for SUOT and 0.4527 for AUT. The differences in the results from comparison are less than 5%. The validation is used to check the effectiveness of the numerical model in calculation and simulation of Ushaped member reinforced timber beam. It still needs various experiments for further research and construction application.
5. Conclusions
Accordingly, great effort has been devoted to the development of prototypes of plate strengthening timber hybrid components to be used in composite structure. The Ushaped member combined with timber provides support not only to vertical forces but also to horizontal forces as fractions between interfaces for the failure are triggered by shear slip. Particularly, analysis of timber beams finds that the mild softening part leads the bolts or screws separate before braking by not carrying the vertical load.
Analysis of the mechanical model of interface bondslip behavior between Ushaped member and timber, and shown in the results of finite element calculation, indicates the Ushape member contributes to the bending capacity, and the available height of flange has been found.
The calculation method based on thinlayer beam theory is validated by numerical analysis that can be used to predict the bending capacity of Ushaped sheet reinforced timber.
The results should be treated as qualitative rather than quantitative due to the small range of data. However, the research for the composite system and the Ushaped member reinforced timber beam still needs to be developed.
Data Availability
The data used to support the findings of this study are available from the corresponding author upon request.
Conflicts of Interest
The authors declare that they have no conflicts of interest.
Acknowledgments
This research was supported by the Hainan Natural and Science Foundation (518MS122 and 518QN307) and the China Postdoctoral Science Foundation (2018M630722).
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Copyright © 2019 Hui Liu et al. 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.