Zi-Xiang Chen1, Zhong-Feng Zhang1, Wan Syaidatul Aqma2. 1. Furniture and Art College, Central South University of Forestry and Technology, Changsha City 410004, China. 2. School of Biosciences and Biotechnology, Faculty of Science and Technology, Universiti Kebangsaan Malaysia, 43600 Bangi, Selangor, Malaysia.
Abstract
Moldy wood can cause some skin disease. However epoxy resin adhesive (EP) can inhibit mold growth. Therefore, antibacterial EP/wood biocomposites were reinforced and analyzed by the nonlinear finite element. Results show that glass fiber cloth and aluminum foil have the obvious reinforced effect under flat pressure, but this was not the case under side pressure. And when the assemble pattern was presented in 5A way, the strengthening effect was better. The nonlinear finite element showed that the aluminum foil and glass fiber cloth have the obvious reinforced effect. The mutual influence and effect of span, thickness and length on the ultimate bearing capacity of specimen were studied. And the simulation results agreed with the test. It provided a theoretical basis on the preparation of antibacterial EP/wood biocomposites against skin disease.
Moldy wood can cause some skin disease. However epoxy resin adhesive (EP) can inhibit mold growth. Therefore, antibacterial EP/wood biocomposites were reinforced and analyzed by the nonlinear finite element. Results show that glass fiber cloth and aluminum foil have the obvious reinforced effect under flat pressure, but this was not the case under side pressure. And when the assemble pattern was presented in 5A way, the strengthening effect was better. The nonlinear finite element showed that the aluminum foil and glass fiber cloth have the obvious reinforced effect. The mutual influence and effect of span, thickness and length on the ultimate bearing capacity of specimen were studied. And the simulation results agreed with the test. It provided a theoretical basis on the preparation of antibacterial EP/wood biocomposites against skin disease.
This painful viral infection is caused by herpes zoster, the virus that causes chickenpox. After infection with chickenpox, the virus “hides” in the nervous system in a latent or dormant state. Exposure to chickenpox or other stressors may cause a reactivation of the virus, resulting in a shingles outbreak. People over the age of 50 are most likely to suffer from shingles (Xiao et al., 2013).Shingles causes uncomfortable and painful symptoms due to inflammation of the sensory nerves, the nerves responsible for the perception of pain, touch, and temperature. The characteristic shingles rash appears as a band-like strip of red, oozing blisters. The rash typically wraps in a strip around the body and usually occurs on one side of the body. Shingles is contagious if an infected person has close contact with others who have not yet had chickenpox. Nerve pain due to shingles can sometimes persist for weeks to years after the rash heals. This painful, post viral condition is known as post-herpetic neuralgia. Some researches showed the herpes zoster came from moldy wood (Mateen et al., 2015).Insects and mold can damage wood over time. To prevent that damage, wood is often treated with pesticides (Barreto et al., 2010). Treated wood is commonly used to build telephone poles, road signs and marine pilings as well as decks, play structures and raised garden beds (Hernandez et al., 1997). Several wood preservatives are registered with the EPA, each with different uses and potential risks (Yin et al., 2001).Wood preservatives can extend the life of wood and reduce the need for forest resources, but proper use is important (Peng et al., 2011, Peng et al., 2012a, Peng et al., 2012b, Peng and Le, 2012). Some preservatives can slowly leach into the surrounding soil or water. Sometimes, touching the wood can leave a residue on exposed skin. Use the resources below to learn about selecting and using treated wood properly. Wood extractives contain plenty of nutrients and hormones (Qureshi et al., 2015). What’s more, resin can strengthen and inhibit the wood mildew (Rasheed et al., 2015). Therefore, the antibacterial EP/wood biocomposites were reinforced and analyzed by the nonlinear finite element.
Material and methods
Test materials
Eucalyptus plantation wood veneer, with the format of 1.27 m × 0.64 m × 1.3 mm, the density of about 0.61 g/cm3 and the water content of 5–8% was used.Epoxy resin adhesive double component epoxy adhesive, of which the component A is the milky white to pale yellow viscous liquid and the component B is the yellowish brown to reddish brown viscous liquid. The working life is 1 h (25 °C), curing speed is 2.5–3.5 h (25 °C), tensile shear strength ⩾8 MPa (25 °C × 48 h) (Youngquist et al., 1979).Glass fiber cloth, plain weave, with the warp and weft density of 128 × 68 was used.
Specimen design scheme
The design of the experiment is shown in Table 1. There are 5 groups of solutions in all, and each group has 3 parallel specimens. By comparing the schemes of 1A, 2A, 3A, and 5A, the enhancement effect of glass fiber cloth can be revealed; by comparing the schemes of 1A, 2A, 4A, and 5A, the enhancement effect of aluminum foil can be revealed.
Table 1
Assemble pattern.
Text number
Assemble pattern
1A
Cross assembly of core seven layers wood veneer, parallel assembly of the three layers wood veneers on the two sides
2A
Cross assembly of core seven layers wood veneer, parallel assembly of the three layers wood veneers on the two sides; the half, glass fiber mesh cloth is arranged between the two layers of the wood veneers for reinforce; the other half, aluminum foil is arranged between the two layers of the wood veneers for reinforce
3A
Cross assembly of core seven layers wood veneer, parallel assembly of the three layers wood veneers on the two sides; glass fiber mesh cloth is arranged between the two layers of the wood veneers for reinforce
4A
Cross assembly of core seven layers wood veneer, parallel assembly of the three layers wood veneers on the two sides; aluminum foil is arranged between the two layers of the wood veneers for reinforce
5A
Cross assembly of core seven layers wood veneer, parallel assembly of the three layers wood veneers on the two sides; glass fiber mesh cloth or aluminum foil is arranged between the two layers of the wood veneers for reinforce, wherein the glass fiber grid cloth and aluminum foil distribute at intervals
Test methods
Assembling was done in accordance with the assemble patterns shown in Table 1 , with the double-sided glue consumption of 350 g/cm2.After assembling, it was put into the compressor under the temperature of about 20 °C, and then pressure was raised to 4 MPa. After applying the pressure for 1 h, the power was turned off and the pressure was applied for 23 h, and then the glulam specimens were made with the format of 350 mm × 350 mm. The normal section of glulam is shown in Fig.1. The standard specimens were designed and made according to “The wood structure test method standard” (GB/T 50329-2002) and “Plywood” (GB 9846-2004), and tested. The test specimens of static bending strength and elastic modulus test: length * width = 300 mm * 50 mm, loading to failure at the speed of 10 Pa/s. The span is 270 mm, and the test loading mode referenced “man-made board and the veneer panel physico-chemical properties test method” (GB/T1 7657-1999). The static bending strength refers to the pressure intensity that artificial plate can bear in the stress bending to fracture, with the unit of MPa (Nasreen et al., 2015). The test adopted the type of loading in section and plane which can be seen in Fig. 2.
Figure 1
Normal section of the EP/wood biocomposites.
Figure 2
Test load figure of MOR.
Results and discussion
Analysis of the effect of EP/wood biocomposites
The average of the 3 parallel specimens of each group was calculated. Test results of 5 specimens are shown in Table 2.
Table 2
Test results.
Text number
Plane compression
Section compression
Width(mm)
Thickness(mm)
Failing load(N)
MOR(MPa)
Elastic modulus(MPa)
Width(mm)
Thickness(mm)
Failing load(N)
MOR(MPa)
Elastic modulus(MPa)
1A
50.60
27.46
1687
17.91
1770.6
26.68
50.46
7305
43.55
2627.0
2A
51.10
28.84
4555
43.40
3725.4
29.22
50.04
7920
43.84
2607.4
3A
50.72
27.70
4005
41.68
3811.5
28.30
52.90
9620
49.20
2948.2
4A
51.18
25.84
3560
42.19
4708.8
26.08
50.50
8050
49.02
3340.3
5A
51.14
25.16
4525
56.61
5407.1
25.48
50.64
9790
60.68
3658.4
From the data of experimental group 1A, 2A, 3A, and 5A we can know that glass fiber cloth played the role of reinforced EP/wood biocomposites. Under the plane compression, the static bending strength and elastic modulus of laminated timber reinforced with glass fiber cloth increased more than 2 times. Among them, the single glass fiber cloth increased the minimum; under the section compression, the failure load, static elastic modulus and bending strength of EP/wood biocomposites reinforced with glass fiber cloth did not increase significantly. From the data of experimental group 1A, 2A, 4A, and 5A we can know that aluminum foil played the role of reinforced EP/wood biocomposites. Under the plane compression, the static bending strength and elastic modulus of EP/wood biocomposites reinforced with aluminum foil increased more than 2 times. When reinforced with aluminum foil alone, the strength of EP/wood biocomposites increased the minimum; under the section compression, the failure load, static elastic modulus and bending strength of EP/wood biocomposites reinforced with aluminum foil did not increase significantly (Liu et al., 2008). We can draw two results from the above analysis: one is that the effect of adding glass fiber cloth, aluminum foil and other reinforcing material is not obvious under the section compression; the other one is that the single enhancement effect of glass fiber cloth and aluminum foil is worse than their composite enhancement effect. At the same time, because the assemble pattern of glass fiber cloth and aluminum foil is different, their enhancement effect is also different (Hashemi et al., 2015). Table 2 shows that the scheme of 5A is the best assemble pattern, namely the composite reinforced way is the cross assembly of core seven layers of wood veneer together with the parallel assembly of the three layers of wood veneers of the two sides; glass fiber mesh cloth or aluminum foil is arranged between the two layers of the wood veneers for reinforcement, wherein the glass fiber grid cloth and aluminum foil are distributed at intervals (Moody, 1970).
The base of nonlinear finite element analysis on glulam
Nonlinear finite element analysis is an effective method for predicting the mechanical performance of materials, and the establishment of failure criterion and constitutive equations is the foundation and key for the nonlinear finite element analysis on mechanical condition of materials.
The failure criterion of glulam
EP/wood biocomposites is the laminated plate formed by overlapping the single plates together in different types. This study used five kinds of experimental components which adopted the cross assembly of core seven layers of wood veneers and were reinforced by aluminum foil, glass fiber grid cloth and the mix of them. Because each of the EP/wood biocomposite layers of fiber alignment is not the same, which may cause the inconsistency of deformation of each layer due to the action of stress, how to decide the final mechanical performance became a very complicated problem. Tsai–Wu tensor criterion is the most comprehensive description of the existing mature standards, and other criteria all can be given by simplifying this criterion according to their own specific loading condition. Tsai–Wu of the original failure criterion boiled down to a higher order tensor polynomial standard, its general form is:In this equation, , and are stress vectors; , , are strength parameters. They are symmetric tensor, and generally can be obtained by experiment. In engineering design, we can usually get the required accuracy by using only the first two of the equation in order to avoid the high experimental expense for determining the tensor coefficients, namely,For one-way slab in state of plane stress, it is written in matrix form as:In the principal direction of coordinates of the material, the change of the direction of shear stress will not affect the strength of the material, so the corresponding strength coefficient of the term of the first degree of shear stress in the equation must be zero, namely,By substituting it in Eqs. (6), (7), (8), (9), (10), (11), (12) and expanding it, you can getIn this formula, strength parameters of the first 5 can be obtained through uniaxial tension–compression test and pure shear test along the principal directions of the material, namelyThe strength coefficient and can be solved by the above formula, namelyBy substituting the solution in guidelines Eqs. (1), (2), (3), (4), (5), (6), (7), you can getSimplifying the above formula, you can get the Hoffman strength criterion, namelyThe remaining coefficient which reflected the interaction of the tension–compression strength of the principal direction 1 and 2, can be obtained by biaxial tensile test instead of uniaxial test.Assuming , substituting it in the Eq. (5), there isWorking out to getObviously, not only depends on basic strength, but is also associated with the biaxial tensile strength. It was noticed that this parameter can be determined by the biaxial tensile test, which is the advantage of Tsai–Wu theory being different from other criteria. But there is also a big problem with that theory, that is, the parameters are very sensitive to the variability of experiment. A minor strength parameter error may lead to a larger variation in parameter value. Therefore, it is necessary to introduce the restrictions on its value (Harvey et al., 1999).On the other hand, the material will be destroyed when the stress increases to a certain extent. So in stress space, the criterion Eq. (5) should be a closed minimal surface which is called the strength envelope. Its intersection with the plane isIt should be a closed curve. According to the nature of the quadratic curve, it should be an ellipse instead of a parabola or hyperbola. It should have the following relationship between the coefficients:NamelyThis is the value range of . For the sake of simplicity, we usually take or 0. The calculated results for most composite materials showed that the difference of the two is less than 10%.
The constitutive equation
The constitutive relationship of each layer of EP/wood biocomposites can be included in the nonlinear influence of material with the incremental form of Hooke’s law, namelyIn this formula,l refers to the l layer of the EP/wood biocomposites;is the interlaminar stress increment vector under the assumption that the interlayer of EP/wood biocomposites bonds well;is the interlaminar strain increment vector under the assumption that the interlayer of EP/wood biocomposites bonds well;is the constitutive matrix of the elastic phase, elastic–plastic phase and the subsequent inactive phase for different stress levels. After the superposition of the constitutive equation for each layer, the stress–strain relationship can be formed as following:Among them, is the residual force vector operating on the inside of each layer. is the thickness of the plate of the layer; is the layers of plates.
The nonlinear finite element simulation analysis on glulam
Using the specimen size and the loading conditions which are the same with the experiment, through the comparison of the force and displacement for the whole process, simulating and analyzing the factors that have influence on EP/wood biocomposites, and verifying the rationality of finite element simulation analysis at the same time. Anisotropic characteristics of wood and isotropic characteristics of other materials were used in the analysis (Khaskheli et al., 2015). The constitutive model and main parameters of the primary materials were arranged as follows (see Table 3).
Table 3
Setting value of component thickness and span.
Assemble pattern
l(h = 54)
l(h = 27)
Non-reinforced materials
270
320
370
420
470
270
320
370
420
470
Reinforced with glass fiber and aluminum foil each half
270
320
370
420
470
270
320
370
420
470
Reinforced with glass fiber
270
320
370
420
470
270
320
370
420
470
Reinforced with aluminum foil
270
320
370
420
470
270
320
370
420
470
Reinforced with the interleaving of glass fiber and aluminum foil
270
320
370
420
470
270
320
370
420
470
The engineering parameters of wood and resin adhesiveAnisotropy of wood: Young’s modulus E1 = E2 = E3 = 1000 MPa, Poisson’s ratio NU12 = NU13 = 0.4, NU23 = 0.04, shear modulus G12 = G13 = 100, G23 = 50 (see Fig. 3).
Figure 3
Constitutive relation of GFRP.
The isotropic epoxy resin adhesive: Young’s modulus E = 1,000,000, shear modulus G1 = G2 = 1,000,000, the viscous coefficient for 1.0e–5.The constitutive relations of materials reinforced with glass fiberIsotropy, Young’s modulus 7000 MPa, Poisson’s ratio of 0.22.The constitutive relations of materials reinforced with aluminum foilIsotropy, Young’s modulus 72,000 MPa, Poisson’s ratio of 0.33 (see Fig. 4).
Figure 4
Constitutive relation of aluminum foil reinforcement.
The division of units and the specimen failure conditions
The failure occurred mainly in midspan and at the end of supports where the stress is concentrative. In order to improve the speed and precision of the numerical analysis, the test specimens were divided into 5 sections. Wherein both ends and the midspan each accounted for 1/10 of the specimen, using smaller units, while the other parts used relatively large units. From the results of numerical analysis, it is very difficult to simulate the fracture failure situation of the specimens which mainly is the glue failure (see Fig. 5).
Figure 5
Component stress unit.
The experiment and the comparison of simulation results
The results of the test and analysis of a section compression and a plane compression in the whole process were compared, as shown in Figs. 6 and 7. The test results showed that from loading to yield, and to the specimen failure, there is some fluctuation in the load-midspan deformation curve (Batool et al., 2015). The failure of the primary timber and reinforced materials has a progressive process and a process of redistribution and transmission of the internal force. The results of finite element numerical analysis are relatively ideal, the load-midspan deformation curve was a straight line from loading to yield. After the yield, the curve showed a horizontal linear development, with almost no decline. From the comparison of the load-midspan deformation curve of the two, the numerical analysis results agreed well with experimental results, especially the relative error in ultimate bearing capacity and ultimate deformation is small, which proved it’s feasible and effective to analyze parameters through numerical simulation analysis (Peng et al., 2013a, Peng et al., 2013b, Peng et al., 2013c).
Figure 6
Load and deformation of sample, 2A under flat pressure.
By using the displacement loading, and controlling the ultimate displacement of the midspan and the experimental test to make they are the same, analyzing the test data of the 10 groups with the numerical simulation method. The comparison of results of the ultimate bearing capacity of numerical analysis and experimental test is shown in Table 4. The results of numerical analysis grew large overall, and the possible reasons are: the constraint condition of supports in numerical simulation is difficult to remain the same as the situation of supports in the experimental test; the constitutive relation of material does not match the actual situation; the contact simulation of colloidal material, reinforced materials and wood veneer has disparity with the actual situation (Spence, 2002).
Table 4
Analysis of simulation values compared with test results.
Flat pressure
Side pressure
Test number
Experimental value
The simulation value
Relative error
Test number
Experimental value
The simulation value
Relative error
1A
1710
1708
0.12%
1A
1421
1625
−14.36%
2A
1702
1917
−12.63%
2A
1679
1893
−12.75%
3A
1687
2193
−29.99%
3A
1685
1790
−6.23%
4A
1258
1545
−22.81%
4A
1687
1657
1.78%
5A
1687
1932
−14.52%
5A
1867
1961
−5.03%
Nonlinear finite element analysis on numerical parameters of glulam
Through the nonlinear finite element analysis on numerical parameters for the assemble thickness of variation tests and the length of specimens, the general variation law was obtained and the displacement loading was used to analyze the ultimate bearing capacity, as shown in Table 5.
Table 5
Finite element simulation results.
Thickness(mm)
Span(mm)
Compression mode
Bearing capacity (N)
1A
2A
3A
4A
5A
27
270
Flat pressure
1421
1679
1685
1687
1867
270
1625
1893
1790
1657
1961
320
1262
1435
1197
1546
1332
370
890
1019
835
1109
941
420
652
746
603
829
687
470
488
561
449
628
515
54
270
6236
7058
6585
7357
6881
320
3906
5386
4846
5673
5220
370
2395
4192
3694
4459
4040
420
1543
3316
2870
3559
3181
470
1053
2661
2266
2880
2543
27
270
Side pressure
1710
1702
1687
1258
1687
270
1708
1917
2193
1545
1932
320
1192
1289
1483
1020
903
370
840
899
1044
703
901
420
388
648
759
504
649
470
311
481
568
372
482
54
270
3418
4018
4433
3191
4033
320
1840
2769
2997
2105
2704
370
875
1930
2108
1452
1878
420
472
1391
1532
1039
1351
470
315
1032
1145
768
1001
Note: Assemble pattern of 1A: full-wooden; assemble pattern of 2A: AL-G; assemble pattern of 3A: G-G; assemble pattern of 4A: AL-AL; assemble pattern of 5A: AL-G-AL-G.
According to the assemble pattern of the test 1A, the relationships between the length and thickness of glued timber members with the whole wood veneer are shown in Fig. 8. Fig. 8 shows that while the thickness remains the same, the bearing capacity decreased gradually with the increase of the member length; while the length remains the same, the bearing capacity increased with the increase in the thickness of the member, and the thicker, the greater the gap between flat pressure and side pressure, which is consistent with the stress nephogram. Simulation results show that in EP/wood biocomposites for bridges, the plane compression mode should be chosen, which is consistent with the experimental results (Peng et al., 2014a, Peng et al., 2014b) (see Fig. 9).
Figure 8
Relations between length, thickness and load of wooden glulam.
Figure 9
Mise stress diagram of wooden glulam with span 270 mm.
In terms of the assemble pattern of 2A, the relationship between the length and thickness of glass fiber cloth reinforced glulam member and the stress is shown in Fig. 10. Fig. 10 shows that while the thickness is the same, the bearing capacity decreased gradually with the increase in member length; while the length is the same, the bearing capacity increased with the increase in the thickness of the member, and for the thickness of 27 mm, the bearing capacity under side pressure is larger than that under flat pressure, while the bearing capacity under flat pressure is two times that under side pressure for the thickness of 54 mm. The simulation results showed that the flat pressure mode should be chosen for the EP/wood biocomposites used in long-span bridges, which is consistent with the experimental results; and the side pressure mode should be chosen for the EP/wood biocomposites used in short-span bridges. Compared with the Fig. 8, glass fiber cloth possesses the enhancement effect, which is in agreement with the result of the experiment.
Figure 10
Relations between length, thickness and load of wood–GFRP glulam.
In terms of the assemble pattern of 3A, the relationship between the length and thickness of aluminum foil reinforced glulam member and the stress was shown in Fig. 11. Fig. 11 shows that while the thickness is the same, the bearing capacity decreased gradually with the increase of member length; while the length is the same, the bearing capacity increased with the increase of the thickness of the member, and for the thickness of 27 mm, the bearing capacity under side pressure is nearly equal to that under flat pressure, while the bearing capacity under flat pressure is more than two times that under side pressure for the thickness of 54 mm. The simulation results showed that the flat pressure mode should be chosen for the EP/wood biocomposites used in bridges, which is consistent with the experimental results. Compared with the Fig. 8, aluminum foil possesses the enhancement effect, which is in agreement with the result of the experiment. Compared with the Fig. 10, the enhancement effect of aluminum foil is better than that of glass fiber cloth, which differs from the experimental results. It is because the simulation results are based on the amalgamation of the bonding interface of aluminum foil and epoxy resin. Meanwhile, it also showed that the bearing capacity of EP/wood biocomposites will get a promotion by improving the fusion of the bonding interface of aluminum foil and epoxy resin (Wang et al., 2003).
Figure 11
Relations between length, thickness and load of wood–aluminum glulam.
In terms of the assemble pattern of 4A, the relationship between the length and thickness of glass fiber cloth and aluminum foil composite glulam member and the stress was shown in Fig. 12. Fig. 12 shows that while the thickness is the same, the bearing capacity decreased gradually with the increase in member length; while the length is the same, the bearing capacity increased with the increase in the thickness of the member, and for the thickness of 27 mm, the bearing capacity under side pressure is nearly equal to that under flat pressure, while the bearing capacity under flat pressure is nearly two times that under side pressure for the thickness of 54 mm. The simulation results showed that the flat pressure mode should be chosen for the EP/wood biocomposites used in long-span bridges, which is consistent with the experimental results; and the side pressure mode should be chosen for the EP/wood biocomposites used in short-span bridges. Compared with the Fig. 10 and the Fig. 11, when the thickness is 27 mm, the bearing capacity of the two is almost the same under flat pressure; when the thickness is 54 mm, aluminum foil reinforced effect > aluminum foil and glass fiber composite reinforced effect > glass cloth reinforced effect. Under the side pressure, glass cloth reinforced effect > aluminum foil and glass fiber composite reinforced effect > aluminum foil reinforced effect.
Figure 12
Relations between length, thickness and load of wood–GFRP–aluminum glulam.
In terms of the assemble pattern of 5A, the relationship between the length and thickness of glass fiber cloth and aluminum foil composite glulam member and the stress is shown in Fig. 13. Fig. 13 shows that while the thickness is the same, the bearing capacity decreased gradually with the increase of member length; while the length is the same, the bearing capacity increased with the increase in the thickness of the member, and for the thickness of 27 mm, the bearing capacity under side pressure is nearly equal to that under flat pressure, while the bearing capacity under flat pressure is nearly two times that under side pressure for the thickness of 54 mm. The simulation results showed that the flat pressure mode should be chosen for the EP/wood biocomposites used in long-span bridges, which is consistent with the experimental results; and the side pressure mode should be chosen for the EP/wood biocomposites used in short-span bridges. Compared with the Fig. 10 and the Fig. 11, when the thickness is 27 mm, the bearing capacity of the two is almost the same under flat pressure; when the thickness is 54 mm, aluminum foil reinforced effect > aluminum foil and glass fiber composite reinforced effect > glass cloth reinforced effect. Under the side pressure, glass cloth reinforced effect > aluminum foil and glass fiber composite reinforced effect > aluminum foil reinforced effect. Compared with the Fig. 12, when the thickness is 27 mm, the bearing capacity of the two is almost the same under flat pressure; when the thickness is 54 mm, reinforced effect of the semi-assembling of glass fiber and aluminum foil is superior to reinforced effect of the cross-assembling of glass fiber and aluminum foil. Under the side pressure, reinforced effect of the semi-assembling of glass fiber and aluminum foil is almost equal to the reinforced effect of the cross-assembling of glass fiber and aluminum foil, which is different from the experimental results. The specific reasons need to be further studied (Wang et al., 2013).
Figure 13
Relations between length, thickness and load of wood–GFRP–aluminum glulam.
In summary, aluminum foil and glass fiber cloth both possess the enhancement effect; the span of specimen increased, then the ultimate bearing capacity decreased; the thickness of assemble specimen is large, the ultimate bearing capacity is large too; while the thickness of specimens is different from each other, the length increased, then the gap of the ultimate bearing capacity of specimens reduced gradually, which indicates that the thickness and length have interactive effects on the ultimate load capacity. This is consistent with the experimental results (Sultana et al., 2015).
Conclusion
Under the flat pressure, reinforced effect of glass fiber, aluminum foil is not obvious; Under the side pressure, glass fiber cloth or aluminum foil single reinforced effect is worse than aluminum foil and glass fiber composite reinforced effect; at the same time, the enhancement effect of glass fiber cloth, aluminum foil is also different while the assemble pattern is different, wherein the scheme of 5A is the best assemble pattern, namely the composite reinforced way is the cross assembly of core seven layers of wood veneer together with the parallel assembly of the three layers of wood veneers of the two sides; glass fiber mesh cloth or aluminum foil is arranged between the two layers of the wood veneers for reinforcement, wherein the glass fiber grid cloth and aluminum foil are distributed at intervals (Javed et al., 2015).Through the nonlinear finite element analysis, we got the failure criterion equation of glulam: , the relationship between the coefficients is: , and the constitutive relation equation of glulam layers is: .The finite element simulation results of nonlinear showed that aluminum foil and glass fiber cloth both possess the enhancement effect; the span of specimen increased, then the ultimate bearing capacity decreased; the thickness and length of assemble specimen is large, the ultimate bearing capacity is large too, and the thickness and length have interactive effect on the ultimate load capacity. This is consistent with the experimental results (Khan et al., 2015).