The effect of knot clusters on the bending properties of Korean pine (Pinus koraiensis) cross-laminated timber (CLT) was analyzed to increase the utilization of low-quality lumber. The laminae used to manufacture the CLT were classified into five groups, four major layer groups, and one minor layer group, by mechanical grade and knot area ratio (KAR) of the lamina. Out-of-plane bending tests were conducted on CLT made from each layer group. The modulus of elasticity (MOE) of the manufactured CLT was closely correlated with the MOE of each individual major axis lamina. In the case of the modulus of rupture (MOR) of the CLT, the KAR of the laminae used in the major axis layer was more significantly affected than the MOE. The main finding is that the lower fifth percentile MOR value of the CLT specimens with large knots (KAR > 0.5) was higher than the acceptable reference value of E3 grade CLT (ANSI/APA PRG 320) made from a similar lamina grade. Therefore, the use of low-quality lumber to manufacture CLT can be expanded under the condition of limitation of the greater KAR.
Hinweise
Part of this article was presented in proceeding of spring annual conference of the Architectural Institute of Korea (Vol.37 No.1), April 27–28, 2017, Jeju, Korea.
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Introduction
Demand for timber construction materials has increased globally in recent years, not only due to aesthetic preferences and structural advantages, but also because the use of timber reduces carbon emissions. The SOM (2013) reported that hybrid construction systems using both concrete and timber reduce CO2 emissions by 60–75%.
The structural safety of timber buildings is closely related to the performance of the structural engineered wood, such as glued laminated timber or cross-laminated timber (CLT). Every individual piece of structural engineered wood is graded by its visual or mechanical characteristics before being used in construction projects. The grades of structural timber specified in the Korean building code refer to the standards and specification of wood products, as published by the National Institute of Forest Science and the Korean Standards (KS F 3020: 2013 and KS F 3021: 2018). In the KS F 3021, the upper limit for the knot area ratio (KAR) in machine stress rated (MSR) lamina was determined to be 17% for the most outer layer, 25% for the outer layer, and 33% for the inner layer. These are the criteria for layer material in glued laminated timber (GLT), and the criteria for layer material in CLT have not yet been established.
Anzeige
Representative softwood species in Korean forests include red pine, Japanese larch, Pinus rigida, and Korean pine. Korean pine forests spread across an area of 23,308,094 ha in 2016 by statistical annual report for forest industry (Korea Forest Service 2018). Korean pine lumber is primarily used for non-structural purposes, such as appearance grade lumber and furniture, because cutting, drying, planing, and other treatments are relatively easy to perform (Chong and Park 2008). However, knot cluster (Fig. 1) due to the growth characteristics of Korean pine presents a major disadvantage in its utilization as a structural element in engineered wood (Song et al. 2015). Yeh (1996) reported that knots were one of the main factors that reduce the strength of engineered wood products. Oh et al. (2000) found many researchers that had studied variations in mechanical properties based on knots of various species to use timber resources more economically.
Fig. 1
Example of knot cluster in a Korean pine lamina
×
CLT is an emerging engineered wood product made by gluing graded laminae together to manufacture structural panels. The axes of CLT are classified as the major and minor axis. The published quality standards of CLT, found in ANSI/APA PRG 320 (2018), explain that the lamina of the minor axis layer must meet visual grade requirements because the quality of that particular layer affects the bonding properties of CLT. Bending strength is an important design parameter required for structural CLT used in building construction. CLT walls need to meet out-of-plane bending performance requirements against wind and seismic load. Pang and Jeong (2019) reported that the load-carrying capacity of larch CLT increased with the span-to-depth ratio of the specimen in the out-of-plane bending test. In contrast, the load-carrying capacity of Korean pine CLTs did not increase as the span-to-depth ratio increased, and the failure occurred around knots. In an experimental test by Hematabadi et al. (2020), the modulus of rupture (MOR) of CLT made from poplar (Populus alba) increased only 1% (from 41.12 to 42.7 MPa) by increasing span-to-depth ratio from 15 to 25. In a numerical study by Flores et al. (2016), the load-carrying capacity of the CLT decreased by 50% as the span-to-depth ratio increased 2.5 times (from 3.3 to 8.3), since the failure mode (crack formation) was changed due to an increase in the span–depth ratio.
A knot cluster in the Korean pine may cause this reduction in CLT bending capacity. Therefore, to improve the structural performance of Korean pine CLTs, a better understanding of the effects of knot cluster on CLT strength is required. To achieve this understanding, the bending performance of CLT made from Korean pine was investigated as a function of the KAR.
Materials and methods
Specimens
Korean pine (Pinus koraiensis), cut from the Gapyeong area of the Gyeonggi Province, was used to build the CLT specimens. The trees were over 30 years old. The size of laminae for CLT manufacturing was 30 mm thick, 100 mm wide, and 3600 mm long. As measured by Korean Standards, the specimens’ air- and oven-dry densities were 0.35 (± 0.07) g/cm3 and 0.40 (± 0.04) g/cm3, with a moisture content of 4.78 (± 1.47)%. The laminae were sorted by the mechanical stress rated machine according to the lamina grade in KS F 3021. A length segment of 2700 mm, which corresponds to the span of the CLT, in a total lamina length of 3600 mm was graded and no finger joints were used. The modulus of elasticity (MOE) distribution of 1400 boards by MSR for laminae is shown in Fig. 2. Approximately, 55% of the total laminae were categorized in E8 and E9 grades. The grade means that the modulus of elasticity (MOE) is not lower than the number (GPa) after the character “E.” The E8 grade means the MOE range is greater than or equal to 8 GPa and less than 9 GPa. The MOE range for the E9 grade is above 9 GPa and less than 10 GPa. These E8 and E9 grade laminae were used for the major axis, while the E7 and lower grade laminae were used for the minor axis of the CLT panel.
Fig. 2
MOE distribution of Korean pine laminae by MSR
×
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The graded structural lumber was used as laminae to form the CLT, according to CLT handbook (Karacabeyli and Douglas 2013). The grading rules of the National Lumber Grading Authority (NLGA 2013) were used to evaluate the maximum KAR (Lam et al. 2005). The KAR is well known to show a good correlation with the strength of lumber (Roblot et al. 2010). The KAR is defined as the ratio of the knot area projected on the cross section versus the total cross-sectional area. Figure 3 shows the concept of KAR and knot size measurement. If the distance between some knots is less than 150 mm in the longitudinal direction, it was calculated as one KAR. In this study, the KAR was calculated by Eq. 1, and detailed information for calculating KAR can be found in ASTM D3737 (2018):
Fig. 3
Knot areas (A, B, and C) projected on the cross-sectional area (thickness × width) to calculate the KAR
The distribution of KAR of the laminae is shown in Table 1. The number of laminae with more than KAR 0.5 was 933 samples, and it was 66.6% of the total laminae. For E-rated structural laminations based on the NLGA grading rules, the KAR should not occupy more than 0.5 of the cross-sectional area (NLGA 2013). Thus, in this study, the laminae were classified into Group A (KAR ≤ 0.5) or Group B (KAR > 0.5) by KAR.
Table 1
KAR distribution of laminae
KARa
0
0~0.1
0.1~0.2
0.2~0.3
0.3~0.4
0.4~0.5
0.5~
Total
No. of laminaeb
1
1
24
80
172
189
933
1400
Ratio (%)c
0.1
0.1
1.7
5.7
12.3
13.5
66.6
100
aKnot area ratio, bnumber of laminae, cnumber of laminae/total number of laminae × 100
The layer composition of the CLT specimens is shown in Table 2. Four types of CLT specimen (E8A, E8B, E9A, and E9B) were manufactured depending on the MSR grade and KAR of the lamina. The first two characters indicate the MSR grade, while the third character indicates the KAR of the outer lamina, where an A means that the KAR is 0.5 or less, and a B means the KAR exceeds 0.5. The ratio of major axis laminae for B groups (20.6% for E8B, 16.8% for E9B) was higher than that for A groups (8.9% for E8A, 9.3% for E9A). The target number of CLT specimens was at least 30, and laminae that were excessively curved or twisted were not used to make CLT. Due to the small number of major axis laminae for A group, the number of CLT specimens for the E8A and E9A group was 20 and 19, respectively.
Table 2
Layer composition of CLT specimens
Classification
E8A
E8B
E9A
E9B
Number of CLT samples
20
30
19
31
Major axis
MSR gradea
E8
E9
KARb
≤ 0.5
> 0.5
≤ 0.5
> 0.5
No. of laminaec
125 (8.9%)d
289 (20.6%)
130 (9.3%)
235 (16.8%)
Minor axis
KAR
≤ E7
No. of laminae
312 (22.3%)
aMSR Machine stress rate, bKAR knot area ratio, cnumber of laminae, dnumber of laminae/total number of laminae × 100
The size of the CLT specimens was 90 mm (thickness) × 300 mm (width) × 2900 mm (length). The CLT specimens contain three layers in total: two major and one minor axis. The two major axis layers consist of three laminae per layer, running parallel to the longitudinal direction of the CLT panel. The minor axis layer was fabricated from 29 laminae, placed perpendicular to the longitudinal direction. A phenol–resorcinol resin (D-40, Oshika Corporation, Japan) adhesive was used to face bond (layer to layer) each layer in the CLT. The amount of adhesive used was 250 g/m2 on both faces, and the pressure and the press time were 0.8 MPa and 24 h at room temperature, respectively.
Bending performance test
The out-of-plane bending performance of the CLT panel was tested by EN 16351 (2014) as shown in Fig. 4. The four-point bending test was conducted by a 30-ton MTS test system (CN/E45:305). The span distance and crosshead speed were 2700 mm and 10 mm/min, respectively. The modulus of rupture (MOR) and MOE of the CLT were calculated by Eqs. (2) and (3), respectively, according to ASTM D198-09 (2009). The lower fifth percentile value of the MOR for each CLT group was determined by nonparametric lower fifth percentile point estimate according to ASTM D 2915-10 (2010). The test values were arranged in ascending order. Beginning with the lowest value, i/(n + 1) was calculated. The lower fifth percentile value was interpolated by Eq. (4):
MOE: Modulus of elasticity (GPa), P: load at proportional limit, Δ: deflection at proportional limit (mm), L: span distance (mm), a: distance between the support and the loading point (mm), w: width of CLT (mm), t: thickness of CLT (mm).
n: Total number of samples, j: the lowest order of the test value when \(i/\left( {n + 1} \right) \ge 0.05\), i: the order of the test value, xi: ith value.
Results and discussion
Failure mode
The typical failure modes of CLT specimens are shown in Fig. 5. All specimens failed near the knots at the bottom of the major axis layer. Since Korean pine is known to contain a high number of knots, especially knot cluster, this phenomenon was expected. The tension failures occurred abruptly along the grain toward the adjacent minor axis layer. The failure initiated at knots near the bottom major axis layer and then transferred to the rolling shear of the minor axis layer. Blass and Görlacher (2000) also reported that splitting failure in the bottom layer created rolling shear failure across the annual ring due to the low rolling shear stiffness of timber. Ehrhart and Brandner (2018) further investigated the rolling shear properties of hardwood species, which were found to be greater than those of softwood. Therefore, mixed species CLTs composed of both softwood and hardwood (e.g., softwood major axis and hardwood minor axis layers) may improve the bending performance of CLT panels.
Fig. 5
Typical failure modes of CLT specimens by out-of-plane bending (a: side view, b: bottom view, arrow: the location of the loading heads)
×
Probability distributions of bending properties for CLT types
Normal distribution curves of MOR and MOE for four types of CLT panels are shown in Fig. 6 to help visualize the effect of the KAR of the major axis on the bending performance of the panels. Figure 6a shows that the MOR values of E8A and E9A were higher than those of E8B and E9B, respectively. The MOR distribution of the A group (samples with KAR values less than 0.5) was higher than the B group MOR distribution. Although the E8A CLTs were made by E8 grade laminae for the major layer, the MOR distribution of the E8A CLTs was a higher value than the E9B CLTs, which were manufactured with E9 grade laminae. These results indicate that the distribution of MOR is more significantly affected by the KAR than the MOE of the constituent laminae. It should be noted that the KAR was subdivided into two groups based on KAR 0.5, and the MOE was subdivided into E9 and E8 with a difference of 1 GPa.
Fig. 6
Probability density distribution of MOR (a) and MOE (b) for each CLT panel type
×
In contrast, the MOE distribution values of the CLT panels were more strongly affected by changes to lamina MOE than KAR (Fig. 6b). Both of the MOE distributions of the E9 groups were higher values than the E8 groups. When the KAR exceeded 0.5 (B groups), the MOE distributions were more concentrated around the average value than the A groups. The MOE variation for layers with large knots may be smaller than for layers with or without small knots.
The cumulative distribution of MOR in the CLT specimens is shown in Fig. 7. The distributions of E8A (Fig. 7a) and E9A (Fig. 7b) were located more to the right side than the E8B and E9B panels. In particular in the A group, the lower tail of the MOR distributions shifted to higher values, compared to the upper tail. Thus, the lower fifth percentile values were significantly increased by limiting the KAR. In addition, the variation of the MOR also decreased, in a similar fashion to the MOE distributions, by limiting the KAR.
Fig. 7
Cumulative distribution for modulus of rupture values of CLT specimens depending on the KAR. Note that a and b are the MOR distributions of CLTs using E8 and E9 major layers, respectively
×
Characteristic values for CLT types
Results of statistical analysis [t test, significant difference (α) = 0.05] between the CLT types are shown in Table 3. Generally, when the p value is less than 0.05, the two types are considered statistically different (Vázquez et al. 2015; Sedighi Gilani et al. 2017). The p value of the MOE between E8A and E8B was greater than 0.05. The p value between E9A and E9B was also greater than 0.05. Thus, when the CLT specimens were made using similar MOE layers, the total MOE of the CLT was not significantly different, even though there were different KAR values in the laminae. However, the p value between all CLT panels made from E8 (E8A + E8B) and those made from E9 (E9A + E9B) laminae were zero. This means that the CLT panels made of different MOE layers did result in significantly different total panel MOE values, regardless of KAR.
When comparing MOR values of different CLT panels, the p values were less than 0.05 in all comparisons. According to the KAR limit (E8A and E8B, and E9A and E9B), the CLT panel’s MOR distributions were significantly different. In addition, the MOR distribution of CLT panels was also significantly different when the MOE of the major layer was varied, without considering the KAR limit. Therefore, these results show that the MOR distribution of CLT was significantly affected by both the lamina MOE and KAR of the major axis layer.
The bending properties of the CLT specimens, sorted by the quality of the major axis layer, are shown in Fig. 8 and Table 4. The average MOR of CLT specimens composed of E8 and E9 major axis layers were 28.2 and 30.1 MPa, respectively. The average MOR of A type CLT, E8A and E9A, was 16.5% and 10.4% higher than the B type CLT, E8B, and E9B, respectively. Interestingly, the fifth percentile value of E8A (25.09 MPa) was 29.7% higher than that of E8B (19.34 MPa). The fifth percentile value of E9A (26.82 MPa) was also 23.7% higher than that of E9B (21.69 MPa). The E9B CLTs were manufactured by E9 grade laminae for the major layer, but the fifth percentile MOR of the E9B CLTs was 14% lower than that of E8A CLTs, which were manufactured with E8 grade laminae for major layer. Thus, these results show that the KAR of the major axis layer of the CLT significantly affected the bending strength of the CLT panel.
Fig. 8
Modulus of rupture (MOR) over modulus of elasticity (MOE) for CLT specimens
Table 4
MOE and MOR values of CLT by the quality of the major axis layer
CLT type
Number of specimens
Modulus of rupture (MPa)
Modulus of elasticity (GPa)
Mean
Fifth percentile (75% confidence)
Mean
E8A
20
30.76 (0.11)a
25.09
7.98 (0.06)
E8B
30
26.41 (0.16)
19.34
8.04 (0.02)
Totalb (E8)
50
28.15 (0.16)
20.73
8.01 (0.04)
E9A
19
31.93 (0.10)
26.82
8.88 (0.05)
E9B
31
28.93 (0.15)
21.69
8.80 (0.04)
Total (E9)
50
30.07 (0.14)
23.13
8.83 (0.05)
aParentheses: coefficient of variation. b“Total” of both A and B
×
For MOE values, the E8 and E9 CLT specimens showed similar results with different KAR groups. The MOE of CLT specimens in E8A (7.98 GPa) was 0.7% lower than that in E8B (8.04 GPa). The MOE of E9A (8.88 GPa) was 0.9% higher than E9B (8.80 GPa). This is an expected result if the different KAR groups within the E8 or E9 grade do not affect the MOE of the CLT specimens. The effect of knot on MOE was not large compared to the effect on MOR. The average MOE of E8 CLTs (8.01 GPa) was similar to the MOE grade of the major layers (E8). The average MOE value of the E9 CLTs (8.83 GPa) was lower than the MOE of the major layers (E9), but the difference was not significant. These results show that the MOE of CLT was influenced by the MOE grade of the major axis layers. Therefore, the MOE grade and KAR of the major axis layer of a CLT panel can be used to predict the bending performance of a CLT panel.
The experimentally measured bending properties were compared with bending performance requirements for CLT grades in published standards. The CLT grades and bending properties for three-layer CLT in ANSI/APA PRG 320 (2018) are provided in Table 5. Since the standard structural properties of CLT provided by the ANSI are presented as a bending moment capacity (N mm) and a bending stiffness (N mm2), to compare with the experimentally measured bending properties, the tabulated bending moment capacity was divided by the sample section modulus (mm3) and converted to MOR (MPa). The tabulated bending stiffness values were divided by the moment of inertia (mm4) of the sample and converted to MOE (MPa). The thickness and width of the three-layer CLT tabulated in ANSI/APA PRG 320 are 105 mm and 1000 mm, respectively. Thus, the section modulus and the moment of inertia of the three-layer CLTs in ANSI/APA PRG 320 are 1,837,500 mm3 and 96,468,750 mm4, respectively. Table 5 shows the MOR and MOE for the CLTs in ANSI/APA PRG 320, which the bending moment capacity and the bending stiffness in ANSI/APA PRG 320 are divided by the section modulus (1,837,500 mm3) and the moment of inertia (96,468,750 mm4), respectively.
Table 5
Lamina requirements and bending properties for CLT grades (ANSI/APA PRG 320-2012)
CLT grades
Requirements for lamina
Bending properties for three-layer CLT
Major layer
Minor layer
MOR (MPa)
MOE (GPa)
E1
Grade: 1950f-1.7E
Species: Spruce-pine-fir
MOR of lamina: 28.2 MPa
MOE of lamina: 11.7 GPa
Grade: No.3
Species: Spruce-pine-fir
MOR of lamina: 7.0 MPa
MOE of lamina: 9.0 GPa
22.86a
11.28b
E2
Grade: 1650f-1.5E
Species: Douglas fir–larch
MOR of lamina: 23.9 MPa
MOE of lamina: 10.3 GPa
Grade: No.3
Species: Douglas fir–larch
MOR of lamina: 4.6 MPa
MOE of lamina: 10.0 GPa
19.59c
9.93d
E3
Grade: 1200f-1.2E
Species: Eastern softwoods, Northern species, or Western woods
MOR of lamina: 17.4 MPa
MOE of lamina: 8.3 GPa
Grade: No.3
Species: Eastern softwoods, Northern species, or Western woods
MOR of lamina: 4.5 MPa
MOE of lamina: 6.5 GPa
14.15e
8.00f
aTabulated bending moment capacity (42 × 106 N mm) divided by its section modulus (1,837,500 mm3). bTabulated bending stiffness (1088 × 109 N mm2) divided by the moment of inertia of major layer (96,468,750 mm4). cTabulated bending moment capacity (36 × 106 N mm) divided by its section modulus (1,837,500 mm3). dTabulated bending stiffness (958 × 109 N mm2) divided by the moment of inertia of major layer (96,468,750 mm4). eTabulated bending moment capacity (26 × 106 N mm) divided by its section modulus (1,837,500 mm3). fTabulated bending stiffness (772 × 109 N mm2) divided by the moment of inertia of major layer (96,468,750 mm4)
In this study, the MOE values of the major layer for E8 group CLT specimens (E8A and E8B) were 8.0–9.0 GPa, and the MOE values of the minor layer for the E8 groups were less than 7.0 GPa. Thus, the measured bending properties of the E8 groups were compared with E3 grade CLT materials.
The MOE of E8A (7.98 GPa) and E8B (8.04 GPa) was similar to the MOE of E3 grade CLT (8.0 GPa). As mentioned above, this shows that the MOE of the CLT panel was strongly influenced by the MOE of the major axis layer used in fabrication. The MOR value of E8A (KAR ≤ 0.5) was 25.09 MPa, 77.3% higher than E3 grade CLT (14.15 MPa). The MOR of E8B (KAR > 0.5) was 19.34 MPa, 36.7% higher than E3 grade CLT. Despite the significant presence of knots (KAR > 0.5) in the major axis layer laminae, the MOR of the experimental panels met the requirements for the E3 grade.
When lumber is used repeatedly, the effect of increasing bending strength is well known (Green and Hernandez 1998). This effect is often applied to member design by applying a repetitive member factor (AWC 2018). In CLT, when a specific graded lamina is repeatedly used in the major axis layer, there is more freedom in lamina material choice, due to this improved strength benefit.
Conclusion
To analyze the effects of the KAR on the bending properties of CLT, out-of-plane bending tests were conducted with CLT specimens with major axis layers manufactured from laminae with two different MOE grades and two different KAR limitations. The results of these tests indicate that:
1.
The tension failure mode of Korean pine CLT occurred mainly from knots at the bottom of the major axis layers. The tension failure then caused a rolling shear failure in the minor axis layers.
2.
The MOE grades and KAR limitation of major axis layers were the key factors affecting the bending properties of the CLT. Specifically, the effect of the major axis KAR on the MOR of the CLT was greater than the effect on the MOE.
3.
The variation of the MOR values for the B group (KAR > 0.5) was wider than the A group (KAR ≤ 0.5). Although the lower fifth percentile values of MOR for the B group were lower than those measured from the A group, the fifth percentile values found in the B group still satisfied the MOR criteria for the E3 grade according to ANSI/APA PRG 320. Thus, it may be sufficient to use lower-quality lumber to manufacture CLT. The efficient use of previously unused lumber can be improved by manufacturing a CLT under the condition of limitation of the greater KAR.
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