 Original Article
 Open Access
 Published:
Study on inplane shear failure mode of crosslaminated timber panel
Journal of Wood Science volume 68, Article number: 36 (2022)
Abstract
To explore inplane shear failure mode of crosslaminated timber (CLT) panel, this paper carried out relevant research work from the perspective of stress analysis and combined with the crack morphology of the specimen after planar shear. In this study, the load–displacement curve of the hemlock [Tsuga canadensis (L.) Carrière] CLT specimen was obtained by a threepoint bending test or an improved planar shear test, the crack morphology of the CLT vertical layer and the azimuth angle of the crack surface were observed and recorded synchronously. The shear strength values of CLT specimens under the two tests were obtained by corresponding calculation. Then the stress analysis of the CLT vertical layer was combined with the azimuth angle of the crack surface to discuss the failure mode of the CLT vertical layer in planar shear. The results showed that the planar shear strength measured by the threepoint bending test and the improved planar shear test was in good agreement, and the results measured by the improved planar shear test were more dispersed than those measured by the threepoint bending test; Considering the approximation that the inplane shear of the CLT vertical layer could be treated as pure shear, the threepoint bending test was better than the improved planar shear test; For the vertical layer of 63.3% CLT specimens, the azimuth of the crack surface was near the azimuth of the first principal plane obtained by stress analysis; There were two failure modes in the CLT vertical layer inplane shear: tension failure and shear failure.
Introduction
In recent years, in developed countries in Europe and the United States, sustainable bamboobased materials [1, 2], passively controlled structural systems [3], as well as crosslaminated timber (CLT), a new type of building material made from sawn timber as the basic unit, have been widely used in the construction of midrise and highrise residential and public buildings. CLT solves the height limitation of traditional wood structure buildings. It is not only easy to implement factory prefabrication and onsite assembly, but also has the advantages of good dimensional stability, sound insulation, good heat preservation performance, good mechanical properties, convenient construction, low carbon, carbon fixation, and environmental protection [4,5,6]. Although traditional CLT structures suffer high seismic damage in timber components (i.e., CLT walls) subjected to seismic actions, CLT structures are easy to repair after the earthquake [7, 8]. And new seismic devices devoted to avoiding high damage are being studied [9]. However, wood has orthotropic anisotropy material behavior, so the mechanical properties of materials composing the wood are undoubtedly complicated [10,11,12,13]. When CLT is used as a floor slab, beam, or other components that are subjected to outofplane lateral loads, the planar shear strength becomes one of the key factors to control the mechanical performance of CLT [14]. Therefore, it is particularly important to study the failure mode of CLT inplane shear.
Since 2016, the main research topics on CLT have included the following areas: material structure, test methods, loading methods, and failure mechanisms of the CLT vertical layer. First, the research on the material structure applies the following tests: CLT threepoint bending test, improved planar shear test, and fourpoint bending test. The test content is aimed at studying the influence of the number of CLT layers, the thickness of each layer, materials, and processing methods of the vertical and parallel layers on the rolling shear strength, shear modulus, and stiffness of CLT [15,16,17,18]. It should be noted that rolling shear refers to the shear strain behavior of timber in its crosssection. Under the action of shear force, cracks are easy to occur in the transition area of early and late wood, wood ray and pith. This failure is called rolling shear failure [19]. Second, the research on the test methods for testing CLT shear properties (rolling shear strength and shear modulus) includes the similarity of the threepoint bending test and improved planar shear test, and the spantoheight ratio of the test piece [20, 21]. Third, the research on the loading methods includes the specimen damage under fatigue loading and the impact of damage accumulation on CLT rolling shear strength [22]. Fourth, the research on the failure mechanism of the CLT vertical layer includes the torque load test, Monte Carlo simulation, and simulation on the shear block specimen, which showed that the CLT rolling shear failure is brittle [23, 24].
In the previous research [25], the threepoint bending test or the improved planar shear test was carried out on CLT specimen. The load–displacement curve of the specimen and the peak load value of the curve were obtained. When the test was over, the crack morphology of the damaged CLT vertical layer was recorded, and the azimuth angle of the crack surface was measured. These were used to reveal the appearance characteristics of the CLT vertical layer crack initiation and propagation on the load–displacement curve.
Based on the above research, the stress, strain, principal stress, maximum and minimum shear stress of the vertical layer of CLT specimens in CLT threepoint bending test and improved planar shear test were analyzed in this study. It clarified that the vertical layer of the threepoint bending specimen and the planar shear specimen could achieve inplane shear, and could be approximately treated as pure shear. When considering the inplane shear of the CLT vertical layer as pure shear, the threepoint bending test was better than the improved planar shear test. Since the CLT vertical layer had undergone shear deformation in the crosssection of the vertical layer, the CLT vertical layer deformation was referred to as inplane shear in this article, and the rolling shear term was not adopted. The corresponding strength value was called the CLT planar shear strength.
In brief, this study revealed the failure mechanism of CLT inplane shear by combining the principal stress, maximum and minimum shear stress (including value and direction) of CLT vertical layer with the azimuth of crack surface, and put forward two failure modes of CLT inplane shear: shear failure and tensile failure.
Materials and methods
Materials
CLT threepoint bending and improved planar shear specimens were sawed from a 3layered 500 × 1200 × 105 mm hemlock [Tsuga canadensis (L.) Carrière] CLT panel. The component unit of the panel (hemlock timber) was ripcut. The onecomponent polyurethane (PUR) was used as the adhesive, with the sizing amount of 180 g/m^{2}. The elasticity modulus of CLT major strength direction was 1.07 × 10^{4} MPa, and the bending strength was 35 MPa. The above materials and relevant data were provided by Ningbo SinoCanada LowCarbon Technology Research Institute Co., Ltd., China.
Specimen for the CLT threepoint bending test
The specimens of Aseries were as follows: 735 × 305 × 105 mm, 15 pieces, to achieve a threepoint bending load with a spantoheight ratio of 6 (Fig. 1). The specimens of Bseries were as follows: 735 × 210 × 105 mm, 6 pieces, to achieve a threepoint bending load with a spantoheight ratio of 6. The laminar width of the vertical layer of A, Bseries was 140 mm. The average moisture content (MC) of A and Bseries specimens was 12%, and the average density ρ was 475 kg/m^{3}. The widths of Aseries and Bseries were 305 mm and 210 mm, respectively, to explore the influence of the width of the threepoint bending specimens on the CLT planar shear (rolling shear) strength test value. It should be noted that the fiber orientation of the parallel layer is parallel to the length of the specimen, and the fiber orientation of the vertical layer is parallel to the width of the specimen.
Specimen for the CLTimproved planar shear test
The specimens of Cseries were as follows: 270 × 135 × 105 mm (the length of the specimen refers to the length of the interface between the vertical layer and the parallel layer), 9 pieces. The laminar width of the vertical layer of Cseries was 140 mm. The average MC was 14%, and the average density ρ was 431 kg/m^{3}. The design of the CLTimproved planar shear test is shown in Fig. 2. Compared with the planar shear test specified in EN408 [26] and ASTM D2718 [27], the advantage of the improved planar shear test is that there’s no need to paste steel plates on the surface of two parallel layers [28].
Test method
JAW2000 multichannel structure test loading system (maximum test force of 300 kN) and AGIC electronic universal mechanical testing machine (maximum test force of 100 kN) were used to carry out the threepoint bending test and the improved planar shear test (Fig. 3). And the load–displacement curve of the specimen was obtained. The tests were carried out in displacement control by using supporting software, with a loading speed of 0.5 mm/min.
The process of the crack initiation and propagation on the test specimen was observed through video recording synchronized with the load–displacement curve. It was applied to explore the relationship between the initiation and propagation of crack and the characteristics of the load–displacement curve.
The maximum load value from the load–displacement curve was obtained to calculate the CLT planar shear strength τ.
According to ASTM D198 [29], the formula used in the CLT threepoint bending test is as follows:
In Eq. 1: τ is the CLT planar shear strength, MPa; P_{max} is the maximum peak load, N; b is the width of the specimen, mm; h is the thickness of the specimen, mm.
It should be noted that 0.92 in Eq. 1 is the correction factor, which is determined by the location of the maximum interlayer shear stress of CLT panel. It is related to the number of layers of the panel [30].
According to EN 408 and reference [28], the formula used in the CLTimproved planar shear test is as follows:
In Eq. 2: τ is the CLT planar shear strength, MPa; P_{max} is the maximum peak load, N; l is the length of the specimen, mm; β is the inclination angle of the specimen, ˚.
The final crack morphology of the specimen was observed and summarized, and the azimuth angle of the main crack surface was measured.
Results and discussion
Test results
CLT crack morphology
The crack morphology of the wood grain on the crosssection of the timber is usually divided into two types: ring shake (Fig. 4a) and heart shake (Fig. 4b). Ring shake includes the crack along the annual ring and the crack along the tangent direction of the annual ring; heart shake refers to the crack along the wood ray. In this research, except for ring shake and heart shake, there was a new crack morphology on the crosssection of the CLT vertical layer under mechanical stress, as shown in Fig. 4c.
CLT crack azimuth angle
The orientation of the crack surfaces of the CLT threepoint bending A, Bseries specimens was symmetrical with respect to the middle of the specimens. The azimuth angle of the crack surface refers to the included angle between the crack direction and the length direction of the specimens, ranging from 0 to 90°.
Table 1 summarizes the vertical layer crack morphologies and crack azimuth angles of the CLT threepoint bending A, Bseries specimens and the CLT planar shear Cseries specimens. For example, A4 (50°) represents the Aseries specimen, the specimen number is 4, and the angle in bracket indicates that the crack azimuth angle is 50°.
From Table 1: the specimens with two cracks were A10 (25°, neither ring shake nor heart shake; 50°, heart shake), B1 (35°, heart shake; 50°, ring shake), B5 (45° and 50°, ring shake), A16 (40°, heart shake; 50°, neither ring shake nor heart shake). The specimen with three cracks was A15 (45°, ring shake; 45°, neither ring shake nor heart shake; and a crack along the wood ray—annual ring—wood ray). The number of specimens with crack azimuth angles between 40° and 50° accounted for 63.3% of the total, and that between 25°–40° or 50°–65° accounted for 23.3%.
Hemlock CLT planar shear strength
Failure tests on the hemlock CLT A, B, Cseries specimens were conducted to obtain the maximum load value of the load–displacement curve, and then the planar shear strength of each hemlock CLT specimen was calculated according to Eq. 1 and Eq. 2. The mean values (peak load and shear strength) are shown in Table 2.
Table 2 shows that the average shear strength of the hemlock CLT tested by the A, Bseries specimens was almost the same, and the relative error was 0.8%. This result showed that in the threepoint bending test, the width of the specimen had virtually no effect on the hemlock CLT shear strength. The planar shear strength of the hemlock CLT tested by the threepoint bending test was quite consistent with that tested by the improved planar shear test, and the relative error was only 5.7%. The dispersion of the CLT shear strength tested by the improved planar shear test was much greater than that tested by the threepoint bending test, and the coefficient of variation of the former was 24.7% while that of the latter was 10.5%.
Stress analysis of the CLT vertical layer
In the test, the vertical layers of the CLT threepoint bending specimen and the CLT shear specimen were subjected to similar forces, which caused the inplane shear in the crosssection of the vertical layer. To explore the mechanism of planar shear and crack failure of the CLT vertical layer, the stress analysis of the vertical layer was applied to obtain the principal stress, the maximum and minimum shear stresses, as well as the normal stress and shear stress on any section. Then the test results of the crack orientation and stress analysis were combined to reveal the failure mode of the CLT vertical layer.
The stress circle is an effective method for stress analysis [31]. The magnitude and direction of the principal stress, the maximum and minimum shear stresses, the normal stress and shear stress on each section can be accurately obtained from the stress circle.
Stress analysis of the vertical layer of the CLT threepoint bending specimen
Part I: Stress component of the vertical layer of the CLT threepoint bending specimen
As shown in Fig. 5, a coordinate system Oxy was established for the CLT threepoint bending specimen. The origin of the coordinates was taken at the center of the beam section at the left support. The horizontal xaxis and the vertical yaxis have positive directions.
For the CLT threepoint bending specimen, three points were taken on the left halfspan: left 1, left 2, and left 3, respectively, located on the upper edge, neutral axis, and lower edge of the vertical layer on the section. Similarly, three points were taken on the right halfspan: right 1, right 2, and right 3. The normal stresses on the points left 1 and right 1 were the maximum compressive stress on the vertical layer of the CLT threepoint bending specimen. And the normal stresses on the points left 3 and right 3 were the maximum tensile stress. The stress state at each point could be obtained by stress analysis in material mechanics: the normal stress was obtained from the bending moment analysis and the shear stress was obtained from the shear force analysis.
Provisions on the symbol before the stress value: for normal stress, + indicates tensile stress and − indicates compressive stress; For shear stress, + indicates that it rotates counterclockwise around the stress element (e.g., point left 1), and − indicates clockwise. Provisions on stress direction (Table 3, Table 4): when the element rotates counterclockwise along the positive xaxis, it is + , and clockwise is −. The above provisions apply to all stress analyses in this paper.
To ensure that the stress on the CLT vertical layer was elastic stress, half of the maximum load was taken as the load for calculating the stress, as the load–displacement curve was linear when the load was less than half of the maximum value [25]. Therefore, for the Aseries specimens, the maximum tensile (compressive) stress on the vertical layer was calculated with a half load of the average maximum load 61.18 kN (Table 2), which was P = 30.59 kN:
The above formula is from reference [30], in which l, b, h correspond to the relevant parameters of Aseries specimens.
So the normal stresses on the xsection of left 1 and right 1 were −0.1 MPa. The normal stresses on the xsection of left 3 and right 3 were + 0.1 MPa. The points left 2 and right 2 were located on the neutral axis of the vertical layer, so the normal stresses on the xsection of them were 0.
According to Eq. 1, the shear stress of Aseries specimens was 0.66 MPa. So the shear stresses on the xsection of the points left 1, left 2, and left 3 were + 0.66 MPa, and that on the ysection were −0.66 MPa. The shear stresses on the xsection of right 1, right 2, and right 3 were −0.66 MPa, and that on the ysection were + 0.66 MPa.
In Fig. 6, the stress components at left 1 were:
on the xsection: σ_{x} = −0.1 MPa, τ_{xy} = + 0.66 MPa;
on the ysection: σ_{y} = 0, τ_{yx} = −0.66 MPa.
Part II: Stress circle of the vertical layer of the CLT threepoint bending specimen
Based on the stress components on the x, ysections at the point left 1, the stress circle of left 1 was drawn as shown in Fig. 7. The same method can be used to draw stress circles for left 2, left 3, right 1, right 2, and right 3.
Part III: Principal stress of the vertical layer of the CLT threepoint bending specimen
The values of the first principal stress and the third principal stress could be read from the abscissa of E and E_{1}, which were the intersection points of the stress circle and the σaxis. And the corresponding principal direction could be read from the angle \(\angle DCE\).
The stress circle of left 1 (Fig. 7) shows that E (+ 0.613, 0), E_{1} (−0.711, 0), \(\angle DCE =  94.3^\circ\). Therefore, the principal stress and their corresponding principal directions at left 1 were as follows (Fig. 8):
σ_{1} = + 0.613 MPa, direction: −47.2°;
σ_{3} = 0.711 MPa, direction: + 42.8°.
From the stress circles of the points left 2, left 3, right 1, right 2, and right 3, the principal stress and corresponding principal direction could be obtained similarly.
The first principal stresses at the points left 1, left 2, and left 3 of the threepoint bending specimen were the tensile stress, and the angles between their direction (the direction of the normal line outside the first principal plane) and the xaxis were −42.8°, −45° and −47.2°, respectively. The first principal stresses at the points right 1, right 2, and right 3 were also tensile stress, and the angles between their direction and the xaxis were +42.8°, +45°, and +47.2°, respectively.
The value of the angle between the direction of tensile stress and the xaxis on the left halfspan was opposite to that on the right halfspan, indicating that their first principal plane orientation was symmetrical with respect to the middle span. This was consistent with the phenomenon that the azimuth orientation of the crack surface on the vertical layer of the CLT threepoint bending specimen was symmetrical with respect to the middle span.
In addition, there were points on the vertical layer of the CLT threepoint bending specimen. The azimuth angle of their first principal plane only differed by 2.2° from that of the points on the neutral axis, and the difference in the magnitude of the first principal stress between the two was only 7.6%. Therefore, the stress state of the CLT vertical layer in the threepoint bending test could be approximately treated as a pure shear stress state.
Part IV: Maximum and minimum shear stresses of the vertical layer of the CLT threepoint bending specimen
In Fig. 9, the values of the maximum and minimum shear stresses could be read from the ordinates of the two points F and F_{1} with the largest distance from the stress circle to the σaxis, which were +0.662 MPa and −0.662 MPa, respectively. The maximum shear stress τ_{1} was located on the crosssection that was rotated 2.2° clockwise along the positive xaxis, so the angle was −2.2°. The minimum shear stress τ_{3} was located on the crosssection rotated 87.8° counterclockwise along the positive xaxis, so the angle was +87.8°.
Similarly, for the points left 2, left 3, right 1, right 2 and right 3, the maximum and minimum shear stresses could also be obtained by performing the same analysis.
The stress state (including the first principal stress σ_{1}, the third principal stress σ_{3}, the maximum shear stress τ_{1}, the minimum shear stress τ_{3}) at left 1 is concluded in Table 3.
Stress analysis of the vertical layer of the CLTimproved planar shear specimen
Point B was taken at the interface between the parallel layer and the vertical layer of the CLT shear specimen (Fig. 2). The xsection of point B was located at the interface between the parallel layer and the vertical layer. The xaxis was perpendicular to the xsection through point B, and its positive direction was along the outer normal. The yaxis was perpendicular to the xaxis, and the section perpendicular to the yaxis through point B was the ysection of point B.
The formulas for calculating normal stress and shear stress were as follows:\(\sigma = P\sin \beta /bl\), \(\tau = P\cos \beta /bl\).
Half of the maximum load 47.15 kN (Table 2) measured by the CLT shear test was taken to calculate the normal stress and shear stress at point B on the CLT vertical layer. According to the average value of the CLT planar shear strength 0.625 MPa and the relationship \(\sigma = \tau \tan 15^\circ\)(β = 15°) [25], σ could be obtained as 0.167 MPa. In this case:
on the xsection: σ_{x} = −0.167 MPa, τ_{xy} = −0.625 MPa;
on the ysection: σ_{y} = 0, τ_{yx} = +0.625 MPa.
The stress components on the x, ysections of point B are shown in Fig. 10.
Through drawing the stress circle at point B, the following values could be obtained.
In summary, the stress circle analysis of the vertical layer of the CLT threepoint bending specimen and the CLT shear specimen showed that:

1)
Under the influence of the maximum normal stress on the vertical layer, the first principal stress obtained by the CLT threepoint bending test was 7.6% different from that under pure shear, and the directions of these two differed by 2.2°. The maximum and minimum shear stresses obtained by the bending test were only 0.3% different from that under pure shear, and the angle between the surfaces where the two located differed by 2.2°.

2)
The first principal stress obtained by the CLTimproved planar shear test was 12.5% different from that under pure shear, and the directions of these two differed by 3.8°. The maximum and minimum shear stresses obtained by the shear test were only 0.9% different from that under pure shear, and the angle between the surfaces where the two located differed by 3.8°.
The results of principal stress, maximum and minimum shear stresses obtained by the threepoint bending test and the improved planar shear test showed that the points on the CLT vertical layer of these two tests could be approximated as in a pure shear stress state. Considering the accuracy of the approximation, the threepoint bending test was better than the improved planar shear test.
For both the threepoint bending test and the improved planar shear test, the stress circle of the CLT vertical layer in the pure shear stress state (ignoring the normal stress) was drawn, then the abscissa and ordinate of the specific points on the circumference were obtained. Figure 11 shows the normal stress σ_{α} and shear stress τ_{α} of the points on the CLT vertical layer on the α section in a specific orientation. α is the angle at which the stress element rotates around the positive axisx. Its definition is the same as the stress direction mentioned above.
Failure mode of the CLT vertical layer inplane shear
In material mechanics, the mechanism analysis of the compression failure of castiron cylinders and the torsion failure of castiron circular shafts are two classic examples of combining stress analysis with the orientation of the failure section [32]. Although the compression load of the castiron cylinder produces compression deformation, the failure caused by it is called shear failure, instead of compression failure. And although the torsion of the castiron shaft produces torsional shear deformation, the failure caused by it is called tensile failure, instead of torsional failure. In other words, the type of deformation cannot determine the type of failure. Therefore, in the CLT threepoint bending test and the CLTimproved planar shear test, the inplane shear deformation of the vertical layer could not be simply considered as shear failure.
CLT vertical layer crack azimuth angle in the range of 40°–50°
A total of 30 threepoint bending specimens and planar shear specimens were tested. After the test, there were 19 specimens with crack azimuth angles of the vertical layer between 40° and 50°, accounting for 63.3% of the total number (Table 1).
The principal stress analysis of the CLT vertical layer showed that when the threepoint bending test achieved the CLT vertical layer inplane shear, the first principal stress was tensile, and the orientation of its action surface (first principal plane) was between −42.8° and −47.2° on the left halfspan, and between + 42.8° and + 47.2°on the right halfspan. The signs reflected that the first principal plane of the vertical layer was symmetrical on the left halfspan and right halfspan. When the improved planar shear test achieved the CLT vertical layer inplane shear, the first principal stress was also the tensile stress, and the orientation of its action surface was + 48.8° or −48.8°. This showed that whether it was a threepoint bending test or an improved planar shear test, the azimuth angle of the first principal plane of each point on the CLT vertical layer was between 40° and 50°, which indicated that the CLT vertical layer was cracked under planar shear. The agreement between the azimuth angle of the crack surface and the azimuth angle of the first principal plane of the CLT vertical layer reached 63.3%.
For the local stress σ_{α} and τ_{α} on the crack surface of the vertical layer with the crack angle in the range of 40–50°, σ_{α}/σ_{1} changed from 0.98 to 1, τ_{α}/τ_{1} changed from 0.17 to 0 (Fig. 11). Although the vertical layer was approximately in pure shear and underwent shear deformation, since τ_{α} was very small, it could not cause the vertical layer to crack along the α plane, so the corresponding failure could not be called shear failure. On the other hand, σ_{α} was very large, almost equal to the first principal stress, and it was also tensile stress. Based on these two findings, it could be considered that the failure of CLT was related to the stretching of the horizontal wood grain of the vertical layer. And within this angle range, the failure mode of CLT was tensile failure.
According to the above analysis, the failure mode of C1 specimen (Fig. 12) could be explained as follows.
There were two cracks on the vertical layer of the CLT shear specimen C1. One of the cracks was at the interface, and the wood chips were clearly visible on the cracked interface, so the crack occurred along the interlayer rather than the glue layer. The azimuth angle of another crack was 40°, so it was under tensile failure.
CLT vertical layer crack azimuth angle in the range of 0°–22.5° or 67.5°–90°
The local stress σ_{α} and τ_{α} on the crack surface on the vertical layer with crack angle in the range of 0°–22.5° or 67.5°–90° changed as follows: σ_{α}/σ_{1} changed from 0 to 0.71, τ_{α}/τ_{1} changed from 1 to 0.71. When τ_{α} was large, and the vertical layer cracked along the action plane of the shear stress, the CLT failure could be considered as shear failure. The corresponding specimens were as follows: A13 (with an azimuth angle of 78°) and B4 (with an azimuth angle of 85°).
CLT vertical layer crack azimuth angle in the range of 22.5°–40° or 50°–67.5°
The specimens with the vertical layer crack angle within this range were: A7 (25°, along the wood ray), A8 (65°, along the wood ray), A10 (25°, neither along the annual ring nor along the wood ray), A18 (30°, along the annual ring tangent, connecting the wood ray), B1 (35°, the wood grain was not clear), B2 (60°, the annual ring line was blurred), C8 (two cracks: 30°, along the wood ray; 30°, along the annual ring), C9 (two cracks: 60°, along the wood ray; 55°, along the annual ring), 9 pieces in total. It should be noted that the definition of direction here is related to the crack morphology. For example, “along the wood ray” means the same as “heart shake”. See the definitions of different crack morphologies for more details.
For the local stress of the vertical layer crack angle within this range, τ_{α}/τ_{1} decreased fastly from 0.71 to 0.17, and the value was not very large. Therefore, it cannot be called shear failure. σ_{α}/σ_{1} changed from 0.71 to 0.98. Although σ_{α} was relatively large and slowly increased as the azimuth angle increased, it was not certain that this phenomenon was due to tensile failure. This situation just reflected the limitation of applying stress analysis for the failure of the vertical layer with the crack angle in the range of 22.5°–40° or 50°–67.5°. Perhaps it was necessary to combine the characteristics of wood as an anisotropic material and make further analysis of the microstructure of the wood.
As the tensile property of wood ray was worse than that of nearby wood fibers, it can be considered that the failure of cracks of the following six specimens was caused by tensile stress: A7, A8, A18, C8 (30°, along the wood ray), C7, C9 (60°, along the wood ray). However, the reason for the failure of cracks of the following specimens could not be determined yet: A10, B1, B2, C8 (30°, along the annual ring), C9 (55°, along the annual ring).
In summary, the specimens with the azimuth angle of the crack surface of 40°–50° accounted for 63.3% of the total number. The specimens with the azimuth angle of 22.5°–40° or 50°–67.5° along wood rays accounted for 20%. These two cases account for 83.3% of the total number of specimens, indicating that the failure of the specimens was related to the transverse tensile property of the crosssection of the vertical layer. The specimens with the azimuth angle of 0°–15° or 75°–90° along wood rays only accounted for 6.7%, and the failure mode of them was shear failure.
Conclusions
According to the crack morphologies and shear strength test results of the threepoint bending test and improved planar shear test, this paper carried out the research on the inplane shear failure mode of CLT panel. The stress state of the CLT vertical layer was determined by analyzing the principal stress, maximum and minimum shear stresses of the point on the vertical layer through stress circle. And the failure mechanism of the vertical layer was comprehensively analyzed by combing planar stress state and crack azimuth angle. The main conclusions were as follows:

1.
The planar shear strength of CLT measured by the threepoint bending test was highly consistent with that measured by the improved planar shear test. The dispersion of CLT shear strength obtained by the improved planar shear test was greater than that measured by the threepoint bending test.

2.
CLT vertical layer inplane shear of the threepoint bending test and improved planar shear test could be treated as pure shear. For the accuracy of the approximation, the threepoint bending test was better than the improved planar shear test.

3.
For the CLT vertical layer in the threepoint bending test and improved planar shear test, the orientation of the crack surface was in good agreement with that of the first principal plane, and the number of coincided specimens accounted for 63.3% of the total.

4.
There were two failure modes in the CLT vertical layer inplane shear: tensile failure and shear failure. In this study, 83.3% of the specimens were under tensile failure and 6.7% of the specimens were under shear failure.
In this paper, the planar shear strength test and failure mechanism analysis of threelayer CLT panel with equal thickness were carried out. In the future, it is planned to carry out relevant research on threelayer CLT panel with unequal thickness and five, sevenlayer CLT panel, so as to improve the systematicness and integrity of the research on the inplane shear failure mechanism of CLT panel. The reason why the coefficient of variation of the threepoint bending test was smaller than that of the improved planar shear test needs to be further explored. Moreover, the crack morphologies of some specimens in this paper have not been fully explained. In the followup study, it will be further analyzed combined with the orthotropy characteristic of wood and the mesostructure of wood.
Availability of data and materials
The datasets used and analyzed during this study are available from the corresponding author upon reasonable request.
Abbreviations
 CLT:

Crosslaminated timber
 MC:

Moisture content
 PUR:

Polyurethane
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Acknowledgements
The authors would like to thank Mr. Gongxun Ma (Nanjing Tech University, China) for his assistance with the theoretical support.
Funding
This work was sponsored by the Science and Technology Project for Policy Guidance of Jiangsu Province (SZLYG 2020016).
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YZ contributed to experiments, data analysis, and writing the manuscript. ZS contributed to experiments. HL contributed to data analysis. YL contributed to manuscript review and editing. ZW designed this study and contributed to manuscript revision and funding acquisition. All authors read and approved the final manuscript.
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Zhou, Y., Shen, Z., Li, H. et al. Study on inplane shear failure mode of crosslaminated timber panel. J Wood Sci 68, 36 (2022). https://doi.org/10.1186/s10086022020452
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DOI: https://doi.org/10.1186/s10086022020452
Keywords
 Crosslaminated timber (CLT)
 Inplane shear
 Threepoint bending test
 Improved planar shear test
 Crack morphology
 Stress circle
 Failure mode