# Fracture Mechanics Models for Brittle Failure of Bottom Rails due to Uplift in Timber Frame Shear Walls

Authors: Joergen L. Jensen; Giuseppe Caprolu; Ulf Arne Girhammar
Journal: Advances in Civil Engineering
 (2016)

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## Abstract

In partially anchored timber frame shear walls, hold-down devices are not provided; hence the uplift forces are transferred by the fasteners of the sheathing-to-framing joints into the bottom rail and via anchor bolts from the bottom rail into the foundation. Since the force in the anchor bolts and the sheathing-to-framing joints do not act in the same vertical plane, the bottom rail is subjected to tensile stresses perpendicular to the grain and splitting of the bottom rail may occur. This paper presents simple analytical models based on fracture mechanics for the analysis of such bottom rails. An existing model is reviewed and several alternative models are derived and compared qualitatively and with experimental data. It is concluded that several of the fracture mechanics models lead to failure load predictions which seem in sufficiently good agreement with the experimental results to justify their application in practical design.


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## Body

## 1. Introduction

A plastic analysis and design method for light-frame timber shear walls have been presented; see, for example, Källsner and Girhammar [1]. In partially anchored shear walls, the leading stud is not fully anchored against uplift and the corresponding tying down forces will develop instead in the sheathing-to-framing joints along the bottom rail. These tying down forces in the joints will, among other things, introduce crosswise bending of the bottom rail with possible splitting failure along the bottom of the rail. Also, splitting of the bottom rail along the row of the sheathing-to-framing joints can occur.In the European timber code, Eurocode 5 [2], no design recommendations are given regarding these kinds of splitting failure of the bottom rail, although the European Standard EN 594 [3] addresses the problem of cupping of the bottom rail due to uplift of the loaded end.Experimental works devoted to the specific question of anchoring the bottom rail with respect to both shear and tensile forces are very scarce. Prion and Lam [4] pointed out the fact that when designing shear walls, it is important to understand the differences between hold-downs at the leading stud and anchor bolts of the bottom rail. In case of no hold-downs and in order to prevent these brittle failure modes, they discussed the need to use large washers to transfer the eccentric loads from the sheathing through the nails into the bottom rail and to the anchor bolts and foundation. Ni and Karacabeyli [5] presented two methods, one empirical and one mechanics-based, to account for the partial uplift when no hold-down connections are used. Most studies have so far been devoted to the lateral (shear) resistance of anchor-bolt joints between bottom rails and foundations; see, for example, Hirai et al. [6–8] and Namura et al. [9]. Leitch et al. [10], Leitch [11], and Menendez et al. [12] noted the importance of a robust bottom rail connection and its ability to offer secure anchorage, with respect to both lateral (shear) and overturning forces. Duchateau [13] studied the uplift resistance of bottom rails in wood shear walls without hold-downs in order to maintain bottom rail structural integrity. Yeh and Williamson [14] presented an experimental study on the combined shear and uplift resistance of wood structural panel shear walls. In the NAHB report [15], an experimental study is presented, where four types of partially anchored shear walls with varying nail size and spacing and with small round or big square washers were tested. Splitting both along the bottom side and along the edge side of the bottom rail occurred.The problem of splitting of the bottom rail in partially anchored shear walls due to uplift has, with respect to the focus of this paper, previously been studied by Girhammar and Källsner [16], with an empirical approach, and by Serrano et al. [17] and Caprolu et al. [18], with an analytical treatment. In Serrano et al. [19] and Serrano et al. [17], a comparison between a finite element analysis and analytical solutions was made. In Caprolu et al. [18], a comparison was made between the analytical models and experimental results. In the present paper, the models presented in these papers are reviewed and alternative models are derived. Model predictions are compared with experimental data previously presented in Caprolu et al. [20, 21]. For further work, see also Caprolu et al. [22] discussed in Section 4 as the last paragraph.


## 2. Experimental Background

An experimental background based on Caprolu et al. [20, 21] is reviewed here. The aim of this section is to give the essential information needed to understand and evaluate the capabilities of the fracture mechanics models presented.


### 2.1. Test Specimen and Material Properties

The specimen was made up of a bottom rail joined to sheathing by nails. The material properties were as follows:(i)
Bottom rail: spruce (PiceaAbies), C24 according to EN 338 [23].(ii)
Sheathing: hardboard, 8 mm (wet process fibre board, HB.HLA2, EN 622-2 [24], Masonite AB).(iii)
Sheathing-to-timber joints: annular ringed shank nails, 50 × 2.1 mm (Duofast, Nordisk Kartro AB). The holes in the sheathing were predrilled, 1.7 mm.(iv)
Anchor bolt:ϕ 12 (M12). The holes in the bottom rail were predrilled 13 mm.


### 2.2. Test Programme and Setup

Two studies on the splitting failure capacity of bottom rail were carried out, here called study A and study B. Both of them studied bottom rails with single- and double-sided sheathing. The differences between the two studies were for single-sided sheathing. (1) The boundary conditions: details can be found in Caprolu et al. [20, 21]. In study A, the load was applied in a distributed way while in study B a hinge was created allowing the specimen to rotate. (2) The nail spacing in the sheathing-to-framing joints: in study A, the nail spacing was 50 mm for series 1 and 25 mm for series 2 and 3, while in study B it was 50 mm for all specimens. (3) The torque used to tighten the bolts: 40 Nm was applied in study A and 50 Nm in study B. (4) The displacement rate: 2 mm/min was used in study A and, by mistake, 10 mm/min was used in study B. For double-sided sheathing, the only difference between the two studies was the boundary conditions. The main aim of the experimental programme was to study the influence of the distance between the edge of the washer and the loaded edge of the bottom rail, here denoted ass, on the failure load and mode of the bottom rail. The distance was varied changing the washer size and the anchor-bolt position according to Table 1 for specimens with single-sided sheathing, and only the washer size for specimens with double-sided sheathing, where the anchor bolt was kept at the centre of the bottom rail for all tests. The specimens were fixed to a supporting structure and loaded with an uplifting load. Figures 1(a) and 1(b) show the test setup of the experiments for single- and double-sided sheathing, respectively.Table 1
Specification of specimen tested in study A and study B. Notation: SS = single-sided specimens, DS = double-sided specimens,b = width of rail, and s = distance from washer edge to loaded edge of the bottom rail (cf. Figure 1).
Series Set ⁢Study A ⁢Study B Anchor bolt position Size of washer Distances ⁢Number of tests ⁢Number of tests SS DS SS DS [mm] [mm] [mm] 1 1-BC (A)a — — — 16 b/2 60 mm from sheathing 40 × 40 × 15 40 1 10 10 16 16 40 × 40 × 15 40 2 10 10 16 16 60 × 60 × 15 30 3 10 10 16 16 80 × 70 × 15 20 4 10 10 16 16 100 × 70 × 15 10  2 1 10 — 14 — 3b/845 mm from sheathing 40 × 40 × 15 25 2 10 16 60 × 60 × 15 15 3 10 16 80 × 70 × 15 5  3 1 10 — 16 — b/430 mm from sheathing 40 × 40 × 15 10 2 9 16 60 × 60 × 15 0 aSet with boundary conditions as study A.Figure 1
Cross section view of the specimen tested: (a) single-sided sheathing and (b) double-sided sheathing.
(a) (b)In Table1, the test program of studies A and B is specified.


### 2.3. Test Programme and Setup

#### 2.3.1. Failure Modes

Three primary failure modes as shown in Figure2 were found during the experimental programmes:(i)
Mode 1: splitting along the bottom side of the rail according to Figure2(a).(ii)
Mode 2: splitting along the edge side of the rail according to Figure2(b).(iii)
Mode 3: yielding and withdrawal of the nails in the sheathing-to-framing joints according to Figure2(c).Figure 2
(a) Splitting failure along the bottom side of the rail; (b) splitting failure along the edge side of the rail; and (c) yielding and withdrawal of the nails in the sheathing-to-framing joints.
(a)
Mode 1 (b)
Mode 2 (c)
Mode 3The failure mode was found to be mainly dependent on the distances in both studies. For distance s≥20 mm, failure mode 1 was the only failure mode, while for distance s≤20 mm, failure modes 2 and 3 also appeared (for specimens with pith upwards and single-sided sheathing, the limit for exclusion of failure modes 2 and 3 was s≥25 mm).


#### 2.3.2. Failure Loads and Crack Development

In Tables2 and 3, the failure load recorded during the experimental studies is listed. Table 2 refers to specimens with pith oriented upwards and Table 3 to specimens with pith oriented downwards. The mean failure load for each set is shown. Further, the mean failure load for each failure mode, according to Figure 2, is listed. In each table, specimens with both single- and double-sided sheathing are included.Table 2
Results from testing of specimens with the pith oriented upwards (PU). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.6 12.6 — — 1 — — — — 2 11.3 11.3 — — 2 25.0 25.0 — — 3 17.0 12.9 21.0 — 3 30.8 30.8 — — 4 24.1 24.3 23.8 — 4 — — — —  2 1 21.5 — 21.5 — — 2 21.2 — 21.2 — 3 28.9 30.6 27.1 —  3 1 19.9 — 19.9 — — 2 27.1 — 27.1 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)b 17.0 17.0 — —  1 1 9.49 9.49 — — 1 17.6 17.6 — — 2 10.6 10.6 — — 2 19.5 19.5 — — 3 17.1 16.8 — 18.7 3 34.0 33.4 35.8 — 4 19.4 19.4 18.1 20.1 4c 39.5 — 37.8 (39.5) 44.5  2 1 12.2 12.2 — — — 2 16.9 16.6 17.5 — 3 22.6 23.2 22.2 —  3 1 18.6 17.9 18.6 18.9 — 2 21.3 — 21.4 20.8 aSeries 1 of study A had a nail distance of 50 mm instead of 25 mm as the other two series of study A. bSet with boundary conditions as in study A. cFor two specimens of this set, it was difficult to establish if the failure mode was mode 2 or 3. The results without parenthesis refer to the case of six results of failure mode 2 and two results of failure mode 3, while the results in parenthesis refer to the case of eight results of failure mode 2.Table 3
Results from testing of specimens with the pith oriented downwards (PD). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.0 12.0 — — 1 22.1 22.1 — — 2 13.5 13.5 — — 2 29.2 29.2 — — 3 17.4 17.4 — — 3 38.6 39.0 — 35.9 4 22.8 22.1 28.6 20.7 4 39.7 39.3 43.4 —  2 1 16.0 16.0 — — — 2 20.7 20.3 23.6 — 3 29.1 30.3 28.0 —  3 1 21.6 21.7 23.1 15.1b — 2 29.2 28.6 29.5 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)c 22.6 22.6 — —  1 1 10.3 10.2 — — 1 20.5 20.5 — — 2 13.5 13.5 — — 2 28.0 28.0 — — 3 18.2 17.9 16.7 19.0 3 39.1 39.5 38.0 — 4 21.8 23.5 20.7 21.4 4 45.8 45.4 47.1 44.2  2 1 14.0 14.0 — — — 2 17.9 19.3 7.70d — 3 23.7 23.5 25.6 21.3  3 1 18.1 15.9 19.5 19.4 — 2 23.8 — 25.4 22.1 aSeries 1 of study A had a nail spacing of 50 mm while the other two series of study A had a nail spacing of 25 mm (except for one specimen in series 3 where the spacing by mistake was 50 mm). bThis specimen had by mistake a nail spacing of 50 mm instead of 25 mm, which is the reason for the ductile failure. cSet with boundary conditions as in study A. dExceptionally low failure load, cause unknown.Since the tests were a collection of data for a future fracture mechanics approach, the crack characteristics, that is, path and length, were studied. It was found that the crack formation depends on the bolt position, the pith orientation, and the annual ring pattern.For specimens with single-sided sheathing and pith upwards (PU), three types of cracks were found for mode 1 and one for failure mode 2, as shown in Figure3. In the same figure, the cracks for double-sided sheathing are also shown, for which two additional types of cracks for failure mode 1 and one additional type for failure mode 2 have been found, with respect to specimens with single-sided sheathing. For failure mode 1, the crack always initiates at the bottom side of the bottom rail, usually in line with the bolt position along the width of the bottom rail, and then it develops in most specimens vertically in a straight line across the annual rings towards the pith (Figure 3(a)) or the crack initiates off the centre and propagates in a straight line towards the pith (Figure 3(b)). In some cases, the crack develops vertically for a certain length and then changes direction following the annual rings (Figure 3(c)). For specimens with double-sided sheathing in Figures 3(d) and 3(e), two additional crack paths are shown: the one in Figure 3(d) occurred only twice and the crack probably propagates in this way because it finds a weaker crack plane, while the crack shape in Figure 3(e) is affected by the pith position. In all other specimens, the pith was on the border of the rail and more or less at the middle of the cross section width. Usually the crack propagates towards the pith.Figure 3
Crack development for bottom rail with pith oriented upwards (PU). (a) Mode 1 crack developing in a straight line, starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line initiating at the bottom surface of the bottom rail at a vertical position close to the edge of the washer and propagating towards the pith; (c) mode 1 crack developing in a straight line for a certain length and then following the annual rings; (d) mode 1 crack developing in an unusual direction, probably due to a weaker crack plane; (e) mode 1 crack developing towards the pith (pith in an unusual position); (f) mode 2 crack starting horizontally and then propagating vertically; and (g) mode 2 crack horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f) (g)The crack for failure mode 2 is always initiated at the nails in the sheathing-to-framing joint and it propagates horizontally for a certain length and then deviates in a more vertical direction across the annual ring (Figure3(f)) or, for double-sided sheathing, following the annual rings (Figure 3(g)).In Figure4, examples of cracks for specimens with pith downwards are shown for specimens with both single and double-sided sheathing. The crack characteristics are similar to those of specimens with pith upwards. The crack starts at the bottom side of the rail and develops vertically in a straight line (Figure 4(a)) or in an oblique line towards the loaded edge of the bottom rail (Figure 4(b)), the latter only for single-sided specimens. In some cases, the crack starts along the annual rings and then it changes in vertical direction across the annual rings (Figure 4(c)) or “jumps” to another annual ring and then follows again its orientation (Figure 4(d)), the latter only in double-sided specimens. In Figure 4(e) an unusual “zig-zag” crack path is shown for a double-sided specimen. For failure mode 2, the crack appears at the line of the nails and propagates horizontally a certain length before it follows the annual rings (Figure 4(f)).Figure 4
Crack development for bottom rail with pith oriented downwards (PD). (a) Mode 1 crack developing in a straight line starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line starting at a location close to the pith and propagating towards the loaded edge of the bottom rail; (c) mode 1 crack first following the annual rings and then propagating in a straight line towards the line of the anchor bolts; (d) mode 1 crack initiating off the centre on the bottom surface of the bottom rail and following an annual ring for a certain length and then jumping to another annual ring and propagating towards the centre of the upper surface of the bottom rail; (e) mode 1 crack propagating in an unusual “zig-zag” line across the annual rings; (f) mode 2 crack development, starting horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f)For most of the specimens, the distance between the position of crack initiation and the edge of the bottom rail, denoted asbcrack1 in Figures 3 and 4, was measured on the end of the bottom rail for failure mode 1. For failure mode 2, the length of the horizontal part of the crack before it changes direction, denoted as bcrack2 in Figures 3 and 4, was measured. In Caprolu et al. [20, 21], the measured bcrack1 and bcrack2 values are listed. In Tables 4 and 5 the measured values for bcrack2 are presented for specimens with pith upwards and downwards, respectively.Table 4
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PU) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided 21.0 15 13 23.8 12 — 21.2 22 27 21.8 20 16 27.1 5 — 19.9 11 — 27.1 20 — — — — — — — 21.9 16 — 20.6 16 14 — — — — — — — — —  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — — — — 17.1 — 18 26.3 26 13 16.5 12 — — — — — — — — — — — — — 15.4 — 17 25.5 — 22 — — — — — — — — — — — — — — — — — — 19.7 22 — — — — — — — — — — — — — — — — — — — 22.2 — 12 — — — — — —  ⁢Double-sided 34.1 17 — 32.4 — 20-20a — 37.4 14 — 38.0 23–15a — — — — 50.0b — 10 — — — 37.8 22–16a — — — — 39.5 — 10 — — — 39.0b — 23-23a — — — 43.8 21 — — — — 35.3 — 16 aHorizontal crack on both edges of the bottom rail. bUncertain whether failure was mode 2 or 3.Table 5
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PD) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — 23.6 20 — 31.4 22 — 20.5 11 — 33.4 18 — — — — — — — — — — 27.1 13 — — — — 29.5 10 — — — — — — — — — — 27.8 17 — — — — 29.4 17 — — — — — — — — — — 25.6 31 — — — — — — —  ⁢Double-sided — — — 43.4 17 18 ⁢—  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — 20.7 21 — 7.70 — 21 24.5 — 39 — — — — — — — — — — — — — — — 28.8 22 — — — — — — — — — — — — — — — — 27.5 18 — — — — — — — — — — — — — — — — 21.5 — 37 — — — — — —  ⁢Double-sided 2/31.5 24–13a 25 47.4 — 20 ⁢— 44.5 15-16a — 46.1 20 — — — — 48.0 10 — — — — 47.2 — 15 aHorizontal crack on both edges of the bottom rail.


## 2.1. Test Specimen and Material Properties

The specimen was made up of a bottom rail joined to sheathing by nails. The material properties were as follows:(i)
Bottom rail: spruce (PiceaAbies), C24 according to EN 338 [23].(ii)
Sheathing: hardboard, 8 mm (wet process fibre board, HB.HLA2, EN 622-2 [24], Masonite AB).(iii)
Sheathing-to-timber joints: annular ringed shank nails, 50 × 2.1 mm (Duofast, Nordisk Kartro AB). The holes in the sheathing were predrilled, 1.7 mm.(iv)
Anchor bolt:ϕ 12 (M12). The holes in the bottom rail were predrilled 13 mm.


## 2.2. Test Programme and Setup

Two studies on the splitting failure capacity of bottom rail were carried out, here called study A and study B. Both of them studied bottom rails with single- and double-sided sheathing. The differences between the two studies were for single-sided sheathing. (1) The boundary conditions: details can be found in Caprolu et al. [20, 21]. In study A, the load was applied in a distributed way while in study B a hinge was created allowing the specimen to rotate. (2) The nail spacing in the sheathing-to-framing joints: in study A, the nail spacing was 50 mm for series 1 and 25 mm for series 2 and 3, while in study B it was 50 mm for all specimens. (3) The torque used to tighten the bolts: 40 Nm was applied in study A and 50 Nm in study B. (4) The displacement rate: 2 mm/min was used in study A and, by mistake, 10 mm/min was used in study B. For double-sided sheathing, the only difference between the two studies was the boundary conditions. The main aim of the experimental programme was to study the influence of the distance between the edge of the washer and the loaded edge of the bottom rail, here denoted ass, on the failure load and mode of the bottom rail. The distance was varied changing the washer size and the anchor-bolt position according to Table 1 for specimens with single-sided sheathing, and only the washer size for specimens with double-sided sheathing, where the anchor bolt was kept at the centre of the bottom rail for all tests. The specimens were fixed to a supporting structure and loaded with an uplifting load. Figures 1(a) and 1(b) show the test setup of the experiments for single- and double-sided sheathing, respectively.Table 1
Specification of specimen tested in study A and study B. Notation: SS = single-sided specimens, DS = double-sided specimens,b = width of rail, and s = distance from washer edge to loaded edge of the bottom rail (cf. Figure 1).
Series Set ⁢Study A ⁢Study B Anchor bolt position Size of washer Distances ⁢Number of tests ⁢Number of tests SS DS SS DS [mm] [mm] [mm] 1 1-BC (A)a — — — 16 b/2 60 mm from sheathing 40 × 40 × 15 40 1 10 10 16 16 40 × 40 × 15 40 2 10 10 16 16 60 × 60 × 15 30 3 10 10 16 16 80 × 70 × 15 20 4 10 10 16 16 100 × 70 × 15 10  2 1 10 — 14 — 3b/845 mm from sheathing 40 × 40 × 15 25 2 10 16 60 × 60 × 15 15 3 10 16 80 × 70 × 15 5  3 1 10 — 16 — b/430 mm from sheathing 40 × 40 × 15 10 2 9 16 60 × 60 × 15 0 aSet with boundary conditions as study A.Figure 1
Cross section view of the specimen tested: (a) single-sided sheathing and (b) double-sided sheathing.
(a) (b)In Table1, the test program of studies A and B is specified.


## 2.3. Test Programme and Setup

### 2.3.1. Failure Modes

Three primary failure modes as shown in Figure2 were found during the experimental programmes:(i)
Mode 1: splitting along the bottom side of the rail according to Figure2(a).(ii)
Mode 2: splitting along the edge side of the rail according to Figure2(b).(iii)
Mode 3: yielding and withdrawal of the nails in the sheathing-to-framing joints according to Figure2(c).Figure 2
(a) Splitting failure along the bottom side of the rail; (b) splitting failure along the edge side of the rail; and (c) yielding and withdrawal of the nails in the sheathing-to-framing joints.
(a)
Mode 1 (b)
Mode 2 (c)
Mode 3The failure mode was found to be mainly dependent on the distances in both studies. For distance s≥20 mm, failure mode 1 was the only failure mode, while for distance s≤20 mm, failure modes 2 and 3 also appeared (for specimens with pith upwards and single-sided sheathing, the limit for exclusion of failure modes 2 and 3 was s≥25 mm).


### 2.3.2. Failure Loads and Crack Development

In Tables2 and 3, the failure load recorded during the experimental studies is listed. Table 2 refers to specimens with pith oriented upwards and Table 3 to specimens with pith oriented downwards. The mean failure load for each set is shown. Further, the mean failure load for each failure mode, according to Figure 2, is listed. In each table, specimens with both single- and double-sided sheathing are included.Table 2
Results from testing of specimens with the pith oriented upwards (PU). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.6 12.6 — — 1 — — — — 2 11.3 11.3 — — 2 25.0 25.0 — — 3 17.0 12.9 21.0 — 3 30.8 30.8 — — 4 24.1 24.3 23.8 — 4 — — — —  2 1 21.5 — 21.5 — — 2 21.2 — 21.2 — 3 28.9 30.6 27.1 —  3 1 19.9 — 19.9 — — 2 27.1 — 27.1 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)b 17.0 17.0 — —  1 1 9.49 9.49 — — 1 17.6 17.6 — — 2 10.6 10.6 — — 2 19.5 19.5 — — 3 17.1 16.8 — 18.7 3 34.0 33.4 35.8 — 4 19.4 19.4 18.1 20.1 4c 39.5 — 37.8 (39.5) 44.5  2 1 12.2 12.2 — — — 2 16.9 16.6 17.5 — 3 22.6 23.2 22.2 —  3 1 18.6 17.9 18.6 18.9 — 2 21.3 — 21.4 20.8 aSeries 1 of study A had a nail distance of 50 mm instead of 25 mm as the other two series of study A. bSet with boundary conditions as in study A. cFor two specimens of this set, it was difficult to establish if the failure mode was mode 2 or 3. The results without parenthesis refer to the case of six results of failure mode 2 and two results of failure mode 3, while the results in parenthesis refer to the case of eight results of failure mode 2.Table 3
Results from testing of specimens with the pith oriented downwards (PD). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.0 12.0 — — 1 22.1 22.1 — — 2 13.5 13.5 — — 2 29.2 29.2 — — 3 17.4 17.4 — — 3 38.6 39.0 — 35.9 4 22.8 22.1 28.6 20.7 4 39.7 39.3 43.4 —  2 1 16.0 16.0 — — — 2 20.7 20.3 23.6 — 3 29.1 30.3 28.0 —  3 1 21.6 21.7 23.1 15.1b — 2 29.2 28.6 29.5 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)c 22.6 22.6 — —  1 1 10.3 10.2 — — 1 20.5 20.5 — — 2 13.5 13.5 — — 2 28.0 28.0 — — 3 18.2 17.9 16.7 19.0 3 39.1 39.5 38.0 — 4 21.8 23.5 20.7 21.4 4 45.8 45.4 47.1 44.2  2 1 14.0 14.0 — — — 2 17.9 19.3 7.70d — 3 23.7 23.5 25.6 21.3  3 1 18.1 15.9 19.5 19.4 — 2 23.8 — 25.4 22.1 aSeries 1 of study A had a nail spacing of 50 mm while the other two series of study A had a nail spacing of 25 mm (except for one specimen in series 3 where the spacing by mistake was 50 mm). bThis specimen had by mistake a nail spacing of 50 mm instead of 25 mm, which is the reason for the ductile failure. cSet with boundary conditions as in study A. dExceptionally low failure load, cause unknown.Since the tests were a collection of data for a future fracture mechanics approach, the crack characteristics, that is, path and length, were studied. It was found that the crack formation depends on the bolt position, the pith orientation, and the annual ring pattern.For specimens with single-sided sheathing and pith upwards (PU), three types of cracks were found for mode 1 and one for failure mode 2, as shown in Figure3. In the same figure, the cracks for double-sided sheathing are also shown, for which two additional types of cracks for failure mode 1 and one additional type for failure mode 2 have been found, with respect to specimens with single-sided sheathing. For failure mode 1, the crack always initiates at the bottom side of the bottom rail, usually in line with the bolt position along the width of the bottom rail, and then it develops in most specimens vertically in a straight line across the annual rings towards the pith (Figure 3(a)) or the crack initiates off the centre and propagates in a straight line towards the pith (Figure 3(b)). In some cases, the crack develops vertically for a certain length and then changes direction following the annual rings (Figure 3(c)). For specimens with double-sided sheathing in Figures 3(d) and 3(e), two additional crack paths are shown: the one in Figure 3(d) occurred only twice and the crack probably propagates in this way because it finds a weaker crack plane, while the crack shape in Figure 3(e) is affected by the pith position. In all other specimens, the pith was on the border of the rail and more or less at the middle of the cross section width. Usually the crack propagates towards the pith.Figure 3
Crack development for bottom rail with pith oriented upwards (PU). (a) Mode 1 crack developing in a straight line, starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line initiating at the bottom surface of the bottom rail at a vertical position close to the edge of the washer and propagating towards the pith; (c) mode 1 crack developing in a straight line for a certain length and then following the annual rings; (d) mode 1 crack developing in an unusual direction, probably due to a weaker crack plane; (e) mode 1 crack developing towards the pith (pith in an unusual position); (f) mode 2 crack starting horizontally and then propagating vertically; and (g) mode 2 crack horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f) (g)The crack for failure mode 2 is always initiated at the nails in the sheathing-to-framing joint and it propagates horizontally for a certain length and then deviates in a more vertical direction across the annual ring (Figure3(f)) or, for double-sided sheathing, following the annual rings (Figure 3(g)).In Figure4, examples of cracks for specimens with pith downwards are shown for specimens with both single and double-sided sheathing. The crack characteristics are similar to those of specimens with pith upwards. The crack starts at the bottom side of the rail and develops vertically in a straight line (Figure 4(a)) or in an oblique line towards the loaded edge of the bottom rail (Figure 4(b)), the latter only for single-sided specimens. In some cases, the crack starts along the annual rings and then it changes in vertical direction across the annual rings (Figure 4(c)) or “jumps” to another annual ring and then follows again its orientation (Figure 4(d)), the latter only in double-sided specimens. In Figure 4(e) an unusual “zig-zag” crack path is shown for a double-sided specimen. For failure mode 2, the crack appears at the line of the nails and propagates horizontally a certain length before it follows the annual rings (Figure 4(f)).Figure 4
Crack development for bottom rail with pith oriented downwards (PD). (a) Mode 1 crack developing in a straight line starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line starting at a location close to the pith and propagating towards the loaded edge of the bottom rail; (c) mode 1 crack first following the annual rings and then propagating in a straight line towards the line of the anchor bolts; (d) mode 1 crack initiating off the centre on the bottom surface of the bottom rail and following an annual ring for a certain length and then jumping to another annual ring and propagating towards the centre of the upper surface of the bottom rail; (e) mode 1 crack propagating in an unusual “zig-zag” line across the annual rings; (f) mode 2 crack development, starting horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f)For most of the specimens, the distance between the position of crack initiation and the edge of the bottom rail, denoted asbcrack1 in Figures 3 and 4, was measured on the end of the bottom rail for failure mode 1. For failure mode 2, the length of the horizontal part of the crack before it changes direction, denoted as bcrack2 in Figures 3 and 4, was measured. In Caprolu et al. [20, 21], the measured bcrack1 and bcrack2 values are listed. In Tables 4 and 5 the measured values for bcrack2 are presented for specimens with pith upwards and downwards, respectively.Table 4
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PU) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided 21.0 15 13 23.8 12 — 21.2 22 27 21.8 20 16 27.1 5 — 19.9 11 — 27.1 20 — — — — — — — 21.9 16 — 20.6 16 14 — — — — — — — — —  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — — — — 17.1 — 18 26.3 26 13 16.5 12 — — — — — — — — — — — — — 15.4 — 17 25.5 — 22 — — — — — — — — — — — — — — — — — — 19.7 22 — — — — — — — — — — — — — — — — — — — 22.2 — 12 — — — — — —  ⁢Double-sided 34.1 17 — 32.4 — 20-20a — 37.4 14 — 38.0 23–15a — — — — 50.0b — 10 — — — 37.8 22–16a — — — — 39.5 — 10 — — — 39.0b — 23-23a — — — 43.8 21 — — — — 35.3 — 16 aHorizontal crack on both edges of the bottom rail. bUncertain whether failure was mode 2 or 3.Table 5
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PD) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — 23.6 20 — 31.4 22 — 20.5 11 — 33.4 18 — — — — — — — — — — 27.1 13 — — — — 29.5 10 — — — — — — — — — — 27.8 17 — — — — 29.4 17 — — — — — — — — — — 25.6 31 — — — — — — —  ⁢Double-sided — — — 43.4 17 18 ⁢—  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — 20.7 21 — 7.70 — 21 24.5 — 39 — — — — — — — — — — — — — — — 28.8 22 — — — — — — — — — — — — — — — — 27.5 18 — — — — — — — — — — — — — — — — 21.5 — 37 — — — — — —  ⁢Double-sided 2/31.5 24–13a 25 47.4 — 20 ⁢— 44.5 15-16a — 46.1 20 — — — — 48.0 10 — — — — 47.2 — 15 aHorizontal crack on both edges of the bottom rail.


## 2.3.1. Failure Modes

Three primary failure modes as shown in Figure2 were found during the experimental programmes:(i)
Mode 1: splitting along the bottom side of the rail according to Figure2(a).(ii)
Mode 2: splitting along the edge side of the rail according to Figure2(b).(iii)
Mode 3: yielding and withdrawal of the nails in the sheathing-to-framing joints according to Figure2(c).Figure 2
(a) Splitting failure along the bottom side of the rail; (b) splitting failure along the edge side of the rail; and (c) yielding and withdrawal of the nails in the sheathing-to-framing joints.
(a)
Mode 1 (b)
Mode 2 (c)
Mode 3The failure mode was found to be mainly dependent on the distances in both studies. For distance s≥20 mm, failure mode 1 was the only failure mode, while for distance s≤20 mm, failure modes 2 and 3 also appeared (for specimens with pith upwards and single-sided sheathing, the limit for exclusion of failure modes 2 and 3 was s≥25 mm).


## 2.3.2. Failure Loads and Crack Development

In Tables2 and 3, the failure load recorded during the experimental studies is listed. Table 2 refers to specimens with pith oriented upwards and Table 3 to specimens with pith oriented downwards. The mean failure load for each set is shown. Further, the mean failure load for each failure mode, according to Figure 2, is listed. In each table, specimens with both single- and double-sided sheathing are included.Table 2
Results from testing of specimens with the pith oriented upwards (PU). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.6 12.6 — — 1 — — — — 2 11.3 11.3 — — 2 25.0 25.0 — — 3 17.0 12.9 21.0 — 3 30.8 30.8 — — 4 24.1 24.3 23.8 — 4 — — — —  2 1 21.5 — 21.5 — — 2 21.2 — 21.2 — 3 28.9 30.6 27.1 —  3 1 19.9 — 19.9 — — 2 27.1 — 27.1 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)b 17.0 17.0 — —  1 1 9.49 9.49 — — 1 17.6 17.6 — — 2 10.6 10.6 — — 2 19.5 19.5 — — 3 17.1 16.8 — 18.7 3 34.0 33.4 35.8 — 4 19.4 19.4 18.1 20.1 4c 39.5 — 37.8 (39.5) 44.5  2 1 12.2 12.2 — — — 2 16.9 16.6 17.5 — 3 22.6 23.2 22.2 —  3 1 18.6 17.9 18.6 18.9 — 2 21.3 — 21.4 20.8 aSeries 1 of study A had a nail distance of 50 mm instead of 25 mm as the other two series of study A. bSet with boundary conditions as in study A. cFor two specimens of this set, it was difficult to establish if the failure mode was mode 2 or 3. The results without parenthesis refer to the case of six results of failure mode 2 and two results of failure mode 3, while the results in parenthesis refer to the case of eight results of failure mode 2.Table 3
Results from testing of specimens with the pith oriented downwards (PD). Failure modes are defined in Figure2.
(a)
Study A
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  1a 1 12.0 12.0 — — 1 22.1 22.1 — — 2 13.5 13.5 — — 2 29.2 29.2 — — 3 17.4 17.4 — — 3 38.6 39.0 — 35.9 4 22.8 22.1 28.6 20.7 4 39.7 39.3 43.4 —  2 1 16.0 16.0 — — — 2 20.7 20.3 23.6 — 3 29.1 30.3 28.0 —  3 1 21.6 21.7 23.1 15.1b — 2 29.2 28.6 29.5 —  (b)
Study B
Series Set Mean failure load [kN] Set Mean failure load [kN] Failure mode Failure mode All failure modes (1) (2) (3) All failure modes (1) (2) (3) ⁢Single-sided tests  ⁢Double-sided tests  ⁢— 1-BC (A)c 22.6 22.6 — —  1 1 10.3 10.2 — — 1 20.5 20.5 — — 2 13.5 13.5 — — 2 28.0 28.0 — — 3 18.2 17.9 16.7 19.0 3 39.1 39.5 38.0 — 4 21.8 23.5 20.7 21.4 4 45.8 45.4 47.1 44.2  2 1 14.0 14.0 — — — 2 17.9 19.3 7.70d — 3 23.7 23.5 25.6 21.3  3 1 18.1 15.9 19.5 19.4 — 2 23.8 — 25.4 22.1 aSeries 1 of study A had a nail spacing of 50 mm while the other two series of study A had a nail spacing of 25 mm (except for one specimen in series 3 where the spacing by mistake was 50 mm). bThis specimen had by mistake a nail spacing of 50 mm instead of 25 mm, which is the reason for the ductile failure. cSet with boundary conditions as in study A. dExceptionally low failure load, cause unknown.Since the tests were a collection of data for a future fracture mechanics approach, the crack characteristics, that is, path and length, were studied. It was found that the crack formation depends on the bolt position, the pith orientation, and the annual ring pattern.For specimens with single-sided sheathing and pith upwards (PU), three types of cracks were found for mode 1 and one for failure mode 2, as shown in Figure3. In the same figure, the cracks for double-sided sheathing are also shown, for which two additional types of cracks for failure mode 1 and one additional type for failure mode 2 have been found, with respect to specimens with single-sided sheathing. For failure mode 1, the crack always initiates at the bottom side of the bottom rail, usually in line with the bolt position along the width of the bottom rail, and then it develops in most specimens vertically in a straight line across the annual rings towards the pith (Figure 3(a)) or the crack initiates off the centre and propagates in a straight line towards the pith (Figure 3(b)). In some cases, the crack develops vertically for a certain length and then changes direction following the annual rings (Figure 3(c)). For specimens with double-sided sheathing in Figures 3(d) and 3(e), two additional crack paths are shown: the one in Figure 3(d) occurred only twice and the crack probably propagates in this way because it finds a weaker crack plane, while the crack shape in Figure 3(e) is affected by the pith position. In all other specimens, the pith was on the border of the rail and more or less at the middle of the cross section width. Usually the crack propagates towards the pith.Figure 3
Crack development for bottom rail with pith oriented upwards (PU). (a) Mode 1 crack developing in a straight line, starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line initiating at the bottom surface of the bottom rail at a vertical position close to the edge of the washer and propagating towards the pith; (c) mode 1 crack developing in a straight line for a certain length and then following the annual rings; (d) mode 1 crack developing in an unusual direction, probably due to a weaker crack plane; (e) mode 1 crack developing towards the pith (pith in an unusual position); (f) mode 2 crack starting horizontally and then propagating vertically; and (g) mode 2 crack horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f) (g)The crack for failure mode 2 is always initiated at the nails in the sheathing-to-framing joint and it propagates horizontally for a certain length and then deviates in a more vertical direction across the annual ring (Figure3(f)) or, for double-sided sheathing, following the annual rings (Figure 3(g)).In Figure4, examples of cracks for specimens with pith downwards are shown for specimens with both single and double-sided sheathing. The crack characteristics are similar to those of specimens with pith upwards. The crack starts at the bottom side of the rail and develops vertically in a straight line (Figure 4(a)) or in an oblique line towards the loaded edge of the bottom rail (Figure 4(b)), the latter only for single-sided specimens. In some cases, the crack starts along the annual rings and then it changes in vertical direction across the annual rings (Figure 4(c)) or “jumps” to another annual ring and then follows again its orientation (Figure 4(d)), the latter only in double-sided specimens. In Figure 4(e) an unusual “zig-zag” crack path is shown for a double-sided specimen. For failure mode 2, the crack appears at the line of the nails and propagates horizontally a certain length before it follows the annual rings (Figure 4(f)).Figure 4
Crack development for bottom rail with pith oriented downwards (PD). (a) Mode 1 crack developing in a straight line starting and propagating vertically at the centre of the bottom rail; (b) mode 1 crack developing in an oblique line starting at a location close to the pith and propagating towards the loaded edge of the bottom rail; (c) mode 1 crack first following the annual rings and then propagating in a straight line towards the line of the anchor bolts; (d) mode 1 crack initiating off the centre on the bottom surface of the bottom rail and following an annual ring for a certain length and then jumping to another annual ring and propagating towards the centre of the upper surface of the bottom rail; (e) mode 1 crack propagating in an unusual “zig-zag” line across the annual rings; (f) mode 2 crack development, starting horizontally and then propagating vertically following the annual rings.
(a) (b) (c) (d) (e) (f)For most of the specimens, the distance between the position of crack initiation and the edge of the bottom rail, denoted asbcrack1 in Figures 3 and 4, was measured on the end of the bottom rail for failure mode 1. For failure mode 2, the length of the horizontal part of the crack before it changes direction, denoted as bcrack2 in Figures 3 and 4, was measured. In Caprolu et al. [20, 21], the measured bcrack1 and bcrack2 values are listed. In Tables 4 and 5 the measured values for bcrack2 are presented for specimens with pith upwards and downwards, respectively.Table 4
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PU) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided 21.0 15 13 23.8 12 — 21.2 22 27 21.8 20 16 27.1 5 — 19.9 11 — 27.1 20 — — — — — — — 21.9 16 — 20.6 16 14 — — — — — — — — —  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 1 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — — — — 17.1 — 18 26.3 26 13 16.5 12 — — — — — — — — — — — — — 15.4 — 17 25.5 — 22 — — — — — — — — — — — — — — — — — — 19.7 22 — — — — — — — — — — — — — — — — — — — 22.2 — 12 — — — — — —  ⁢Double-sided 34.1 17 — 32.4 — 20-20a — 37.4 14 — 38.0 23–15a — — — — 50.0b — 10 — — — 37.8 22–16a — — — — 39.5 — 10 — — — 39.0b — 23-23a — — — 43.8 21 — — — — 35.3 — 16 aHorizontal crack on both edges of the bottom rail. bUncertain whether failure was mode 2 or 3.Table 5
Measured failure loads and horizontal crack lengths for failure mode 2 for specimens with the pith oriented downwards (PD) for single- and double-sided sheathing.bcrack2 is the length of the horizontal crack before it changes direction. End 1 and End 2 indicate the two bottom rail ends.
(a)
Study A
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — — — — 23.6 20 — 31.4 22 — 20.5 11 — 33.4 18 — — — — — — — — — — 27.1 13 — — — — 29.5 10 — — — — — — — — — — 27.8 17 — — — — 29.4 17 — — — — — — — — — — 25.6 31 — — — — — — —  ⁢Double-sided — — — 43.4 17 18 ⁢—  (b)
Study B
⁢Series 1 ⁢Series 2 ⁢Series 3 Set 3 Set 4 Set 2 Set 3 Set 1 Set 2 Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] Failure load [kN] b c r a c k 2 [mm] End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 End 1 End 2 ⁢Single-sided — — — 20.7 21 — 7.70 — 21 24.5 — 39 — — — — — — — — — — — — — — — 28.8 22 — — — — — — — — — — — — — — — — 27.5 18 — — — — — — — — — — — — — — — — 21.5 — 37 — — — — — —  ⁢Double-sided 2/31.5 24–13a 25 47.4 — 20 ⁢— 44.5 15-16a — 46.1 20 — — — — 48.0 10 — — — — 47.2 — 15 aHorizontal crack on both edges of the bottom rail.


## 3. Theory

A linear elastic body with a preexisting crack with areaA is considered. The body is subjected to a single-force, P, and the value Pu, which causes the preexisting crack to propagate, is sought. The so-called compliance method of fracture mechanics, which follows from simple energy considerations, leads to [25–30](1)Pu=2GfdCA/dA,where Pu is the failure load, Gf is the fracture energy, A is the crack area, and C is the compliance, that is, the deflection at the loading point for a unit force.Bottom rails in partially anchored shears wall are subjected to uplift forces from the sheathing (see, e.g., Ni and Karacabeyli [5, 31], Girhammar and Källsner [16], and Caprolu et al. [18]) which may result in splitting of the bottom rail. Experiments show (Figure 2) that cracks may form either at the bottom side of the rail and propagate vertically (mode 1) or at the side of the rail and propagate horizontally (mode 2). The first type is presented in Serrano et al. [17] and both types of cracks are treated in Serrano et al. [19] and Caprolu et al. [18], and a fracture mechanics solution based on (1) is derived.In the present paper, the existing fracture mechanics model is reviewed and alternative models also based on (1) are derived and compared with each other and with the experimental data presented in Section 2.


### 3.1. Horizontal Cracking (Mode 2)

#### 3.1.1. Model 1

Figure5 shows the geometry, boundary conditions, and loading conditions assumed in Serrano et al. [19] and Caprolu et al. [18] for a crack propagating horizontally in a bottom rail.Figure 5
Geometry, boundary conditions, and loading conditions used in Caprolu et al. [18] for a horizontal crack.The out-of-plane width of the bottom rail is denoted asb, and the crack is assumed to propagate simultaneously over the entire width, b. The problem considered in Caprolu et al. [18] is reduced to determination and differentiation of the compliance of a simple cantilever beam with depth he, width b, and length a, where a is the crack length. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(2)Ca=4Ebahe3+βsGbahe,where E is the modulus of elasticity, G is the shear modulus, he is shown in Figure 5, and βs is the shear correction factor (usually 6/5 for a rectangular cross section). E and G are the appropriate values for the perpendicular-to-grain direction. It may here be noted that timber has different properties in the tangential and radial directions. This fact may be taken properly into account when using numerical methods like the Finite Element Method (see, e.g., Vessby et al. [32]) but is difficult to handle in simple analytical models. It is further for practical applications usually not possible to know with certainty how the timber is cut and oriented in the structure. It is thus often in analytical models for simplicity assumed that the timber has the same properties in the radial and tangential directions. This assumption will also be applied here.Using (1) with A=ba and the compliance as given by (2), the following expression for the failure load is obtained:(3)Pu=b2GGfhe12G/Ea/he2+βs.It is noted that the solution does not depend on the total depth,h, of the bottom rail.Assuming small crack length (a→0) or assuming that bending deformations can be ignored as compared with the shear deformations (i.e., G/E→0) leads to(4)Pu=b2GGfheβs.Equations (3)-(4) are the same solutions as derived in Caprolu et al. [18].


#### 3.1.2. Model 2

In Gustafsson [33], splitting failure of an end-notched beam as shown in Figure 6 is considered.Figure 6
Geometry of end-notched beam as considered in Gustafsson [33].While the model presented in Caprolu et al. [18] assumes that only shear and bending deformations of the cantilever beam shown in Figure 5 give contributions to the compliance, the model derived in Gustafsson [33] also takes into account contributions from the part of the beam with depth h and from additional rotation of the cantilever due to the fact that the stiffness of the beam with depth h cannot be fully activated in the immediate vicinity of the corner of the notch. The solution given in Gustafsson [33] reads as follows:(5)Pu=bαhGGf/h3/5α1-α+β6G/E1/α-α2,where α and β are defined in Figure 6. It should be noted that (5) is based on (1) and the compliance is determined using simple beam theory and assuming the shear correction factor βs=6/5.Using (5) on a bottom rail as considered in Figure 5, (βh is then the crack length, a) the following failure load is obtained:(6)Pu=bhGGf/h3/51-α/α+a/h6G/E1/α3-1,α=heh.It is noted that (6) takes into account the effect of the total depth, h, of the rail.In the special case of a small crack (a→0) or if assuming that the bending deformations are negligible as compared with the shear deformations (G/E→0), (6) reduces to:(7)Pu=bC1he1-he/h,C1=53GGf.Equation (7) leads to (4), for he/h→0.


#### 3.1.3. Model 3

In Jensen [34], a beam loaded perpendicular to the grain by a bolt located close to the edge and close to the end of the beam was considered. Figure 7 defines the geometry.Figure 7
Geometry of beam considered in Jensen [34].Based on the theory for a Timoshenko-beam on a Winkler-foundation, a so-called quasi-nonlinear fracture mechanics solution was derived. The general expression for the failure load does not become simple, but for a small crack length (a→0), the relatively simple solution given as (8) was obtained: (8)
P
u
=
P
0
·
min
⁡
1
2
2
ζ
+
1
+
b
f
t
l
e
P
0
2
ζ
+
1
ζ
+
1
P
0
=
2
b
C
1
h
e
,
C
1
=
5
3
G
G
f
,
ζ
=
C
1
f
t
10
G
E
1
h
e
,where ft is the perpendicular-to-grain tensile strength.The horizontal crack in a bottom rail may be considered a special case of (8), namely, for le→0, which leads to(9)Pu=P0122ζ+1P0=2bC1he,C1=53GGf,ζ=C1ft10GE1he.It is noted that (9), for ft→∞, leads to (4) if βs=6/5.In van der Put and Leijten [35], a linear elastic fracture mechanics model was derived for a simply supported beam loaded perpendicular to grain by a single-load at midspan. The solution given in (10) was obtained, where again h is the beam depth and he is the loaded edge distance:(10)Pu=2bC1he1-he/h,C1=53GGf.It is noted that (10) gives exactly twice the failure load as obtained from (7).It is also noted that (10) for small edge distances (he/h→0) leads to Pu=P0, where P0 is given in (9). P0 may therefore be regarded as a special case of (10). A semiempirical generalized version of (9) may be proposed:(11)Pu=γbC1he1-he/hC1=53GGf,γ=12ζ+1,ζ=C1ft10GE1he.Equation (11) then leads to (7), for G/E→0 or ft→∞.Equations (3)-(4) and (9) do not include the total depth of the bottom rail. This means that cracking is predicted also for situations, where the loaded edge distance is very close to the total depth of the bottom rail. Intuitively, the propensity to splitting should disappear in such situations since the part with depth (h-he) has little stiffness as compared with the part with depth he and thus offers little resistance against following the deflection of the part with depth he. Equations (6)-(7) and (11) take the effect of the total depth of the bottom rail into account and predict infinitely high failure loads for, he/h→0; that is, horizontal splitting is not an issue if the nails are placed sufficiently close to the bottom surface of the bottom rail.


### 3.2. Vertical Cracking (Mode 1)

#### 3.2.1. Model 1

For a crack propagating vertically from the bottom surface of a bottom rail, Serrano et al. [19], Serrano et al. [17], and Caprolu et al. [18] consider a fully clamped beam as shown in Figure 8.Figure 8
Geometry, boundary conditions, and loading conditions used in Serrano et al. [17] and in Caprolu et al. [18] for a vertical crack.The problem is in Serrano et al. [17] again, as in the case of a horizontal crack, reduced to determination and differentiation of the compliance of a simple cantilever beam. Here is a cantilever beam with depth (h-a), width b, and length le. The crack length is a; that is, the crack area again becomes A=ba. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(12)Ca=4Ebleh-a3+βsGbleh-a,where E is the modulus of elasticity, G is the shear modulus, βs is the shear correction factor, and the geometry is given in Figure 8.It should be noted that the compliance as given by (12) is a conservative estimate since the part of the cantilever beam below the crack tip is not considered but in fact gives a contribution to the stiffness.Using (1) with A=ba and the compliance as given by (12), the following expression for the failure load is obtained:(13)Pu=bh-a2GGf/le12G/Ele/h-a2+βs.Assuming a small crack length (a→0) leads to(14)Pu=bh2GGf/le12G/Ele/h2+βs.Assuming that bending deformations can be ignored (G/E→0), (13) leads to(15)Pu=bh-a2GGfleβs.Assuming the small crack length and that bending deformations can be ignored leads to(16)Pu=bh2GGfleβs.


#### 3.2.2. Model 2

The cantilever beam as shown in Figure8 is considered again. However, it is here assumed that the cantilever is not completely rigidly clamped at the end, but a finite rotation occurs. The deflection of the loading point, δ, is then given by(17)δ=δb+δv+δr,where δb is the contribution from bending of the cantilever, δv is the contribution from shear of the cantilever, and δr is the contribution from a rotation at the clamped end of the cantilever. The rotation at the clamped end of the cantilever may be thought of as a simple linear elastic rotational spring with compliance cr, and the deflection due to the rotation is then given by(18)δr=Ple2cr,where cr in general is a function of the crack length, a.The compliance due to bending and shear is again given by (12), and the total compliance thus becomes (19)Ca=4Ebleh-a3+βsGbleh-a+le2cr.Differentiation ofC(a) with respect to a and use of (1) leads to(20)Pu=bh-a2GGf/le12G/Ele/h-a2+bGleh-a2dcra/da+βs.If the following choice is made for the spring compliance,(21)cr=1b12βsGE1h-a2.A particularly simple expression is obtained for the failure load, namely,(22)Pu=bh-a2GGf/le12G/Ele/h-a+βs.The similarity/difference between (22) and (13) is noted.For a small crack length, (22) gives(23)Pu=bh2GGf/le12G/Ele/h+βs.Assuming negligible bending deformations, (22) leads to(24)Pu=bh-a2GGfleβs.And both small crack length and insignificant bending deformations lead to(25)Pu=bh2GGfleβs.Equation (24) is the same as (15), and (25) is the same as (16).


#### 3.2.3. Model 3

In the derivation of the end-notched beam model by Gustafsson [33], the cantilever has been assumed fixed to a rotational spring in exactly the same way as in model 2. However, in Gustafsson [33], the compliance, cr, of the rotational spring was chosen as(26)cr=12bh210GE1-α1-α3α4,where α=1-a/h.The compliance of the spring was also in Gustafsson [33] chosen so as to result in a simple expression for the failure load. However, since the crack propagation considered in Gustafsson [33] makes the length of the cantilever increase, while the crack considered here propagates so that the length of the cantilever is constant but its depth decreases, the influence of crack propagation becomes different in the two cases, and thus different expressions ((21) and (26)) for the spring compliance optimize the simplicity.The spring compliance as given by (26) has been proven to give good results for end-notched beams. If (26) is used in (20), the following expression is obtained for the failure load:(27)Pu=bαh2GGf/le12G/Ele/αh2+18/5G/E4-3α-α3/1-α1-α3le/αh+βs.For a small crack length,α→1, and thus(28)Pu=bh2GGf/le12G/Ele/h2+66/5G/Ele/h+βs.If the deformations from bending are assumed to be negligible as compared with the shear deformations, (27) gives(29)Pu=bαh2GGfβsle.And for small crack length and negligible bending deformations,(30)Pu=bh2GGfβsle.Equation (29) is the same as (15) and (24), and (30) is the same as (16) and (25).


### 3.3. Additional Failure Modes and Modifications

Figure2(c) shows a failure mode (mode 3) where the nails and/or the wood yield and the nails are pulled out of the bottom rail. This failure mode is treated in Caprolu et al. [18] and is outside the scope of the present paper, which focuses on failure of the bottom rail. The models presented in Sections 3.1 and 3.2 consider horizontal and vertical crack propagation, respectively. However, in addition to crack propagation, bending and shear failures of the considered cantilever beams may also occur and cause failure of the bottom rail. Here simplified models will be used.For horizontal crack propagation (mode 2), the following equations should also be considered for bending and shear, respectively:(31)Pu=bhe26aft(32)Pu=23bhefv,where ft is the perpendicular-to-grain tensile strength, and fv the rolling shear strength.For vertical crack propagation (mode 1), the following equations for bending and shear should be considered in addition to the fracture mechanics models:(33)Pu=bh-a26left(34)Pu=23bh-afv.The failure load of the bottom rail subjected to uplift is the minimum value of the failure loads given by (31)–(34) and two selected models (one for horizontal cracking and one for vertical cracking) from Sections 3.1 and 3.2.The fracture mechanics models considered in Sections3.1 and 3.2 are all based on (1) and consider an existing crack of length a. All the derived models predict that the load needed to propagate the crack decreases with increasing crack length, and the maximum load which the bottom rail can sustain is thus obtained from the models by assuming zero crack length. However, it may be relevant to assume a certain minimum or critical value, ac, of the crack length as suggested in Serrano and Gustafsson [30]:(35)ac=E90Gfπft2,whereE90 is the modulus of elasticity in the perpendicular-to-grain direction. Different values of the material properties may be used in (35) for the tangential and radial directions if such distinction is made.In Caprolu et al. [18], (35) was considered together with the models presented in Section 3.1.1 for a horizontally propagating crack (mode 2) and in Section 3.2.1 for a vertically propagating crack (mode 1). The length, le, of the cantilever beam considered in Section 3.2 was introduced as le=s+c as shown in Figure 8, where s is the distance from the loaded edge of the bottom rail to the edge of the washer and c is an additional length in recognition of the fact that the bottom rail may not be fully clamped at the edge of the washer. From (3) and (13), theoretical expressions, le0, were given for the value of le which determines the limit between vertical crack propagation (mode 1) and horizontal crack propagation (mode 2) for general orthotropic conditions and inclusion of (35). For the special case of isotropic conditions (assuming the same material properties in the radial and tangential directions) and assuming zero initial crack length, they determined the limit to(36)le0=βsEh424Ghe+βsEh424Ghe2+βsEh224G33+βsEh424Ghe-βsEh424Ghe2+βsEh224G33.A horizontally propagating crack (mode 2) leads to failure of the bottom rail ifle<le0 and a vertically propagating crack (mode 1) leads to failure if le>le0.Further, in Caprolu et al. [18] c was estimated from experimental data by fitting using (13).


## 3.1. Horizontal Cracking (Mode 2)

### 3.1.1. Model 1

Figure5 shows the geometry, boundary conditions, and loading conditions assumed in Serrano et al. [19] and Caprolu et al. [18] for a crack propagating horizontally in a bottom rail.Figure 5
Geometry, boundary conditions, and loading conditions used in Caprolu et al. [18] for a horizontal crack.The out-of-plane width of the bottom rail is denoted asb, and the crack is assumed to propagate simultaneously over the entire width, b. The problem considered in Caprolu et al. [18] is reduced to determination and differentiation of the compliance of a simple cantilever beam with depth he, width b, and length a, where a is the crack length. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(2)Ca=4Ebahe3+βsGbahe,where E is the modulus of elasticity, G is the shear modulus, he is shown in Figure 5, and βs is the shear correction factor (usually 6/5 for a rectangular cross section). E and G are the appropriate values for the perpendicular-to-grain direction. It may here be noted that timber has different properties in the tangential and radial directions. This fact may be taken properly into account when using numerical methods like the Finite Element Method (see, e.g., Vessby et al. [32]) but is difficult to handle in simple analytical models. It is further for practical applications usually not possible to know with certainty how the timber is cut and oriented in the structure. It is thus often in analytical models for simplicity assumed that the timber has the same properties in the radial and tangential directions. This assumption will also be applied here.Using (1) with A=ba and the compliance as given by (2), the following expression for the failure load is obtained:(3)Pu=b2GGfhe12G/Ea/he2+βs.It is noted that the solution does not depend on the total depth,h, of the bottom rail.Assuming small crack length (a→0) or assuming that bending deformations can be ignored as compared with the shear deformations (i.e., G/E→0) leads to(4)Pu=b2GGfheβs.Equations (3)-(4) are the same solutions as derived in Caprolu et al. [18].


### 3.1.2. Model 2

In Gustafsson [33], splitting failure of an end-notched beam as shown in Figure 6 is considered.Figure 6
Geometry of end-notched beam as considered in Gustafsson [33].While the model presented in Caprolu et al. [18] assumes that only shear and bending deformations of the cantilever beam shown in Figure 5 give contributions to the compliance, the model derived in Gustafsson [33] also takes into account contributions from the part of the beam with depth h and from additional rotation of the cantilever due to the fact that the stiffness of the beam with depth h cannot be fully activated in the immediate vicinity of the corner of the notch. The solution given in Gustafsson [33] reads as follows:(5)Pu=bαhGGf/h3/5α1-α+β6G/E1/α-α2,where α and β are defined in Figure 6. It should be noted that (5) is based on (1) and the compliance is determined using simple beam theory and assuming the shear correction factor βs=6/5.Using (5) on a bottom rail as considered in Figure 5, (βh is then the crack length, a) the following failure load is obtained:(6)Pu=bhGGf/h3/51-α/α+a/h6G/E1/α3-1,α=heh.It is noted that (6) takes into account the effect of the total depth, h, of the rail.In the special case of a small crack (a→0) or if assuming that the bending deformations are negligible as compared with the shear deformations (G/E→0), (6) reduces to:(7)Pu=bC1he1-he/h,C1=53GGf.Equation (7) leads to (4), for he/h→0.


### 3.1.3. Model 3

In Jensen [34], a beam loaded perpendicular to the grain by a bolt located close to the edge and close to the end of the beam was considered. Figure 7 defines the geometry.Figure 7
Geometry of beam considered in Jensen [34].Based on the theory for a Timoshenko-beam on a Winkler-foundation, a so-called quasi-nonlinear fracture mechanics solution was derived. The general expression for the failure load does not become simple, but for a small crack length (a→0), the relatively simple solution given as (8) was obtained: (8)
P
u
=
P
0
·
min
⁡
1
2
2
ζ
+
1
+
b
f
t
l
e
P
0
2
ζ
+
1
ζ
+
1
P
0
=
2
b
C
1
h
e
,
C
1
=
5
3
G
G
f
,
ζ
=
C
1
f
t
10
G
E
1
h
e
,where ft is the perpendicular-to-grain tensile strength.The horizontal crack in a bottom rail may be considered a special case of (8), namely, for le→0, which leads to(9)Pu=P0122ζ+1P0=2bC1he,C1=53GGf,ζ=C1ft10GE1he.It is noted that (9), for ft→∞, leads to (4) if βs=6/5.In van der Put and Leijten [35], a linear elastic fracture mechanics model was derived for a simply supported beam loaded perpendicular to grain by a single-load at midspan. The solution given in (10) was obtained, where again h is the beam depth and he is the loaded edge distance:(10)Pu=2bC1he1-he/h,C1=53GGf.It is noted that (10) gives exactly twice the failure load as obtained from (7).It is also noted that (10) for small edge distances (he/h→0) leads to Pu=P0, where P0 is given in (9). P0 may therefore be regarded as a special case of (10). A semiempirical generalized version of (9) may be proposed:(11)Pu=γbC1he1-he/hC1=53GGf,γ=12ζ+1,ζ=C1ft10GE1he.Equation (11) then leads to (7), for G/E→0 or ft→∞.Equations (3)-(4) and (9) do not include the total depth of the bottom rail. This means that cracking is predicted also for situations, where the loaded edge distance is very close to the total depth of the bottom rail. Intuitively, the propensity to splitting should disappear in such situations since the part with depth (h-he) has little stiffness as compared with the part with depth he and thus offers little resistance against following the deflection of the part with depth he. Equations (6)-(7) and (11) take the effect of the total depth of the bottom rail into account and predict infinitely high failure loads for, he/h→0; that is, horizontal splitting is not an issue if the nails are placed sufficiently close to the bottom surface of the bottom rail.


## 3.1.1. Model 1

Figure5 shows the geometry, boundary conditions, and loading conditions assumed in Serrano et al. [19] and Caprolu et al. [18] for a crack propagating horizontally in a bottom rail.Figure 5
Geometry, boundary conditions, and loading conditions used in Caprolu et al. [18] for a horizontal crack.The out-of-plane width of the bottom rail is denoted asb, and the crack is assumed to propagate simultaneously over the entire width, b. The problem considered in Caprolu et al. [18] is reduced to determination and differentiation of the compliance of a simple cantilever beam with depth he, width b, and length a, where a is the crack length. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(2)Ca=4Ebahe3+βsGbahe,where E is the modulus of elasticity, G is the shear modulus, he is shown in Figure 5, and βs is the shear correction factor (usually 6/5 for a rectangular cross section). E and G are the appropriate values for the perpendicular-to-grain direction. It may here be noted that timber has different properties in the tangential and radial directions. This fact may be taken properly into account when using numerical methods like the Finite Element Method (see, e.g., Vessby et al. [32]) but is difficult to handle in simple analytical models. It is further for practical applications usually not possible to know with certainty how the timber is cut and oriented in the structure. It is thus often in analytical models for simplicity assumed that the timber has the same properties in the radial and tangential directions. This assumption will also be applied here.Using (1) with A=ba and the compliance as given by (2), the following expression for the failure load is obtained:(3)Pu=b2GGfhe12G/Ea/he2+βs.It is noted that the solution does not depend on the total depth,h, of the bottom rail.Assuming small crack length (a→0) or assuming that bending deformations can be ignored as compared with the shear deformations (i.e., G/E→0) leads to(4)Pu=b2GGfheβs.Equations (3)-(4) are the same solutions as derived in Caprolu et al. [18].


## 3.1.2. Model 2

In Gustafsson [33], splitting failure of an end-notched beam as shown in Figure 6 is considered.Figure 6
Geometry of end-notched beam as considered in Gustafsson [33].While the model presented in Caprolu et al. [18] assumes that only shear and bending deformations of the cantilever beam shown in Figure 5 give contributions to the compliance, the model derived in Gustafsson [33] also takes into account contributions from the part of the beam with depth h and from additional rotation of the cantilever due to the fact that the stiffness of the beam with depth h cannot be fully activated in the immediate vicinity of the corner of the notch. The solution given in Gustafsson [33] reads as follows:(5)Pu=bαhGGf/h3/5α1-α+β6G/E1/α-α2,where α and β are defined in Figure 6. It should be noted that (5) is based on (1) and the compliance is determined using simple beam theory and assuming the shear correction factor βs=6/5.Using (5) on a bottom rail as considered in Figure 5, (βh is then the crack length, a) the following failure load is obtained:(6)Pu=bhGGf/h3/51-α/α+a/h6G/E1/α3-1,α=heh.It is noted that (6) takes into account the effect of the total depth, h, of the rail.In the special case of a small crack (a→0) or if assuming that the bending deformations are negligible as compared with the shear deformations (G/E→0), (6) reduces to:(7)Pu=bC1he1-he/h,C1=53GGf.Equation (7) leads to (4), for he/h→0.


## 3.1.3. Model 3

In Jensen [34], a beam loaded perpendicular to the grain by a bolt located close to the edge and close to the end of the beam was considered. Figure 7 defines the geometry.Figure 7
Geometry of beam considered in Jensen [34].Based on the theory for a Timoshenko-beam on a Winkler-foundation, a so-called quasi-nonlinear fracture mechanics solution was derived. The general expression for the failure load does not become simple, but for a small crack length (a→0), the relatively simple solution given as (8) was obtained: (8)
P
u
=
P
0
·
min
⁡
1
2
2
ζ
+
1
+
b
f
t
l
e
P
0
2
ζ
+
1
ζ
+
1
P
0
=
2
b
C
1
h
e
,
C
1
=
5
3
G
G
f
,
ζ
=
C
1
f
t
10
G
E
1
h
e
,where ft is the perpendicular-to-grain tensile strength.The horizontal crack in a bottom rail may be considered a special case of (8), namely, for le→0, which leads to(9)Pu=P0122ζ+1P0=2bC1he,C1=53GGf,ζ=C1ft10GE1he.It is noted that (9), for ft→∞, leads to (4) if βs=6/5.In van der Put and Leijten [35], a linear elastic fracture mechanics model was derived for a simply supported beam loaded perpendicular to grain by a single-load at midspan. The solution given in (10) was obtained, where again h is the beam depth and he is the loaded edge distance:(10)Pu=2bC1he1-he/h,C1=53GGf.It is noted that (10) gives exactly twice the failure load as obtained from (7).It is also noted that (10) for small edge distances (he/h→0) leads to Pu=P0, where P0 is given in (9). P0 may therefore be regarded as a special case of (10). A semiempirical generalized version of (9) may be proposed:(11)Pu=γbC1he1-he/hC1=53GGf,γ=12ζ+1,ζ=C1ft10GE1he.Equation (11) then leads to (7), for G/E→0 or ft→∞.Equations (3)-(4) and (9) do not include the total depth of the bottom rail. This means that cracking is predicted also for situations, where the loaded edge distance is very close to the total depth of the bottom rail. Intuitively, the propensity to splitting should disappear in such situations since the part with depth (h-he) has little stiffness as compared with the part with depth he and thus offers little resistance against following the deflection of the part with depth he. Equations (6)-(7) and (11) take the effect of the total depth of the bottom rail into account and predict infinitely high failure loads for, he/h→0; that is, horizontal splitting is not an issue if the nails are placed sufficiently close to the bottom surface of the bottom rail.


## 3.2. Vertical Cracking (Mode 1)

### 3.2.1. Model 1

For a crack propagating vertically from the bottom surface of a bottom rail, Serrano et al. [19], Serrano et al. [17], and Caprolu et al. [18] consider a fully clamped beam as shown in Figure 8.Figure 8
Geometry, boundary conditions, and loading conditions used in Serrano et al. [17] and in Caprolu et al. [18] for a vertical crack.The problem is in Serrano et al. [17] again, as in the case of a horizontal crack, reduced to determination and differentiation of the compliance of a simple cantilever beam. Here is a cantilever beam with depth (h-a), width b, and length le. The crack length is a; that is, the crack area again becomes A=ba. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(12)Ca=4Ebleh-a3+βsGbleh-a,where E is the modulus of elasticity, G is the shear modulus, βs is the shear correction factor, and the geometry is given in Figure 8.It should be noted that the compliance as given by (12) is a conservative estimate since the part of the cantilever beam below the crack tip is not considered but in fact gives a contribution to the stiffness.Using (1) with A=ba and the compliance as given by (12), the following expression for the failure load is obtained:(13)Pu=bh-a2GGf/le12G/Ele/h-a2+βs.Assuming a small crack length (a→0) leads to(14)Pu=bh2GGf/le12G/Ele/h2+βs.Assuming that bending deformations can be ignored (G/E→0), (13) leads to(15)Pu=bh-a2GGfleβs.Assuming the small crack length and that bending deformations can be ignored leads to(16)Pu=bh2GGfleβs.


### 3.2.2. Model 2

The cantilever beam as shown in Figure8 is considered again. However, it is here assumed that the cantilever is not completely rigidly clamped at the end, but a finite rotation occurs. The deflection of the loading point, δ, is then given by(17)δ=δb+δv+δr,where δb is the contribution from bending of the cantilever, δv is the contribution from shear of the cantilever, and δr is the contribution from a rotation at the clamped end of the cantilever. The rotation at the clamped end of the cantilever may be thought of as a simple linear elastic rotational spring with compliance cr, and the deflection due to the rotation is then given by(18)δr=Ple2cr,where cr in general is a function of the crack length, a.The compliance due to bending and shear is again given by (12), and the total compliance thus becomes (19)Ca=4Ebleh-a3+βsGbleh-a+le2cr.Differentiation ofC(a) with respect to a and use of (1) leads to(20)Pu=bh-a2GGf/le12G/Ele/h-a2+bGleh-a2dcra/da+βs.If the following choice is made for the spring compliance,(21)cr=1b12βsGE1h-a2.A particularly simple expression is obtained for the failure load, namely,(22)Pu=bh-a2GGf/le12G/Ele/h-a+βs.The similarity/difference between (22) and (13) is noted.For a small crack length, (22) gives(23)Pu=bh2GGf/le12G/Ele/h+βs.Assuming negligible bending deformations, (22) leads to(24)Pu=bh-a2GGfleβs.And both small crack length and insignificant bending deformations lead to(25)Pu=bh2GGfleβs.Equation (24) is the same as (15), and (25) is the same as (16).


### 3.2.3. Model 3

In the derivation of the end-notched beam model by Gustafsson [33], the cantilever has been assumed fixed to a rotational spring in exactly the same way as in model 2. However, in Gustafsson [33], the compliance, cr, of the rotational spring was chosen as(26)cr=12bh210GE1-α1-α3α4,where α=1-a/h.The compliance of the spring was also in Gustafsson [33] chosen so as to result in a simple expression for the failure load. However, since the crack propagation considered in Gustafsson [33] makes the length of the cantilever increase, while the crack considered here propagates so that the length of the cantilever is constant but its depth decreases, the influence of crack propagation becomes different in the two cases, and thus different expressions ((21) and (26)) for the spring compliance optimize the simplicity.The spring compliance as given by (26) has been proven to give good results for end-notched beams. If (26) is used in (20), the following expression is obtained for the failure load:(27)Pu=bαh2GGf/le12G/Ele/αh2+18/5G/E4-3α-α3/1-α1-α3le/αh+βs.For a small crack length,α→1, and thus(28)Pu=bh2GGf/le12G/Ele/h2+66/5G/Ele/h+βs.If the deformations from bending are assumed to be negligible as compared with the shear deformations, (27) gives(29)Pu=bαh2GGfβsle.And for small crack length and negligible bending deformations,(30)Pu=bh2GGfβsle.Equation (29) is the same as (15) and (24), and (30) is the same as (16) and (25).


## 3.2.1. Model 1

For a crack propagating vertically from the bottom surface of a bottom rail, Serrano et al. [19], Serrano et al. [17], and Caprolu et al. [18] consider a fully clamped beam as shown in Figure 8.Figure 8
Geometry, boundary conditions, and loading conditions used in Serrano et al. [17] and in Caprolu et al. [18] for a vertical crack.The problem is in Serrano et al. [17] again, as in the case of a horizontal crack, reduced to determination and differentiation of the compliance of a simple cantilever beam. Here is a cantilever beam with depth (h-a), width b, and length le. The crack length is a; that is, the crack area again becomes A=ba. The compliance of such a cantilever beam, if taking flexural as well as shear deformations into account, is given by(12)Ca=4Ebleh-a3+βsGbleh-a,where E is the modulus of elasticity, G is the shear modulus, βs is the shear correction factor, and the geometry is given in Figure 8.It should be noted that the compliance as given by (12) is a conservative estimate since the part of the cantilever beam below the crack tip is not considered but in fact gives a contribution to the stiffness.Using (1) with A=ba and the compliance as given by (12), the following expression for the failure load is obtained:(13)Pu=bh-a2GGf/le12G/Ele/h-a2+βs.Assuming a small crack length (a→0) leads to(14)Pu=bh2GGf/le12G/Ele/h2+βs.Assuming that bending deformations can be ignored (G/E→0), (13) leads to(15)Pu=bh-a2GGfleβs.Assuming the small crack length and that bending deformations can be ignored leads to(16)Pu=bh2GGfleβs.


## 3.2.2. Model 2

The cantilever beam as shown in Figure8 is considered again. However, it is here assumed that the cantilever is not completely rigidly clamped at the end, but a finite rotation occurs. The deflection of the loading point, δ, is then given by(17)δ=δb+δv+δr,where δb is the contribution from bending of the cantilever, δv is the contribution from shear of the cantilever, and δr is the contribution from a rotation at the clamped end of the cantilever. The rotation at the clamped end of the cantilever may be thought of as a simple linear elastic rotational spring with compliance cr, and the deflection due to the rotation is then given by(18)δr=Ple2cr,where cr in general is a function of the crack length, a.The compliance due to bending and shear is again given by (12), and the total compliance thus becomes (19)Ca=4Ebleh-a3+βsGbleh-a+le2cr.Differentiation ofC(a) with respect to a and use of (1) leads to(20)Pu=bh-a2GGf/le12G/Ele/h-a2+bGleh-a2dcra/da+βs.If the following choice is made for the spring compliance,(21)cr=1b12βsGE1h-a2.A particularly simple expression is obtained for the failure load, namely,(22)Pu=bh-a2GGf/le12G/Ele/h-a+βs.The similarity/difference between (22) and (13) is noted.For a small crack length, (22) gives(23)Pu=bh2GGf/le12G/Ele/h+βs.Assuming negligible bending deformations, (22) leads to(24)Pu=bh-a2GGfleβs.And both small crack length and insignificant bending deformations lead to(25)Pu=bh2GGfleβs.Equation (24) is the same as (15), and (25) is the same as (16).


## 3.2.3. Model 3

In the derivation of the end-notched beam model by Gustafsson [33], the cantilever has been assumed fixed to a rotational spring in exactly the same way as in model 2. However, in Gustafsson [33], the compliance, cr, of the rotational spring was chosen as(26)cr=12bh210GE1-α1-α3α4,where α=1-a/h.The compliance of the spring was also in Gustafsson [33] chosen so as to result in a simple expression for the failure load. However, since the crack propagation considered in Gustafsson [33] makes the length of the cantilever increase, while the crack considered here propagates so that the length of the cantilever is constant but its depth decreases, the influence of crack propagation becomes different in the two cases, and thus different expressions ((21) and (26)) for the spring compliance optimize the simplicity.The spring compliance as given by (26) has been proven to give good results for end-notched beams. If (26) is used in (20), the following expression is obtained for the failure load:(27)Pu=bαh2GGf/le12G/Ele/αh2+18/5G/E4-3α-α3/1-α1-α3le/αh+βs.For a small crack length,α→1, and thus(28)Pu=bh2GGf/le12G/Ele/h2+66/5G/Ele/h+βs.If the deformations from bending are assumed to be negligible as compared with the shear deformations, (27) gives(29)Pu=bαh2GGfβsle.And for small crack length and negligible bending deformations,(30)Pu=bh2GGfβsle.Equation (29) is the same as (15) and (24), and (30) is the same as (16) and (25).


## 3.3. Additional Failure Modes and Modifications

Figure2(c) shows a failure mode (mode 3) where the nails and/or the wood yield and the nails are pulled out of the bottom rail. This failure mode is treated in Caprolu et al. [18] and is outside the scope of the present paper, which focuses on failure of the bottom rail. The models presented in Sections 3.1 and 3.2 consider horizontal and vertical crack propagation, respectively. However, in addition to crack propagation, bending and shear failures of the considered cantilever beams may also occur and cause failure of the bottom rail. Here simplified models will be used.For horizontal crack propagation (mode 2), the following equations should also be considered for bending and shear, respectively:(31)Pu=bhe26aft(32)Pu=23bhefv,where ft is the perpendicular-to-grain tensile strength, and fv the rolling shear strength.For vertical crack propagation (mode 1), the following equations for bending and shear should be considered in addition to the fracture mechanics models:(33)Pu=bh-a26left(34)Pu=23bh-afv.The failure load of the bottom rail subjected to uplift is the minimum value of the failure loads given by (31)–(34) and two selected models (one for horizontal cracking and one for vertical cracking) from Sections 3.1 and 3.2.The fracture mechanics models considered in Sections3.1 and 3.2 are all based on (1) and consider an existing crack of length a. All the derived models predict that the load needed to propagate the crack decreases with increasing crack length, and the maximum load which the bottom rail can sustain is thus obtained from the models by assuming zero crack length. However, it may be relevant to assume a certain minimum or critical value, ac, of the crack length as suggested in Serrano and Gustafsson [30]:(35)ac=E90Gfπft2,whereE90 is the modulus of elasticity in the perpendicular-to-grain direction. Different values of the material properties may be used in (35) for the tangential and radial directions if such distinction is made.In Caprolu et al. [18], (35) was considered together with the models presented in Section 3.1.1 for a horizontally propagating crack (mode 2) and in Section 3.2.1 for a vertically propagating crack (mode 1). The length, le, of the cantilever beam considered in Section 3.2 was introduced as le=s+c as shown in Figure 8, where s is the distance from the loaded edge of the bottom rail to the edge of the washer and c is an additional length in recognition of the fact that the bottom rail may not be fully clamped at the edge of the washer. From (3) and (13), theoretical expressions, le0, were given for the value of le which determines the limit between vertical crack propagation (mode 1) and horizontal crack propagation (mode 2) for general orthotropic conditions and inclusion of (35). For the special case of isotropic conditions (assuming the same material properties in the radial and tangential directions) and assuming zero initial crack length, they determined the limit to(36)le0=βsEh424Ghe+βsEh424Ghe2+βsEh224G33+βsEh424Ghe-βsEh424Ghe2+βsEh224G33.A horizontally propagating crack (mode 2) leads to failure of the bottom rail ifle<le0 and a vertically propagating crack (mode 1) leads to failure if le>le0.Further, in Caprolu et al. [18] c was estimated from experimental data by fitting using (13).


## 4. Discussion

While the crack path is predetermined for problems such as end-notched beams or splitting of beams loaded perpendicular to grain by bolted connections where the crack propagates along the grain, this is not the case in a bottom rail as considered here. The models presented in Sections3.1 and 3.2 assume that the crack propagates either horizontally or vertically, but it is in fact very likely that the direction of the crack propagation changes as the crack grows. For instance, at any stage of the propagation of a horizontal crack as considered in Section 3.1, the crack may change direction and start propagating vertically (as considered in Section 3.2) if this requires less energy.For simplicity, consider the simplest models for horizontal and vertical crack propagation, that is, the models given in Sections3.1.1 and 3.2.1 and first presented in Serrano et al. [19] and Caprolu et al. [18]. Assume that a horizontal crack has been initiated and grown to the length,a, as shown in Figure 5. At what length will the crack start to grow vertically (if at all at any crack length)? The solution is given by taking (3) as it is and setting it equal to (14), in which le=a and h=he. These equations lead to the solution that the crack will start propagating in the vertical direction when a=he. Figure 9 illustrates the problem. According to (3), the horizontal crack will propagate at decreasing load levels until a=he, then the crack will start propagating vertically. Figure 9 shows the failure load per mm of the length of the bottom rail given as a function of the horizontal crack length, a, using h=45 mm, he=22.5 mm, E=400 MPa, G=70 MPa, Gf=0.30 N/mm, and βs=6/5. The material properties are those used in Serrano et al. [19] and Caprolu et al. [18]. Using (3) and (14), the point where the horizontal crack starts propagating vertically is a=he and is independent of the geometry and material properties of the bottom rail. The same exercise may be done using other models for the horizontal and vertical crack propagation, but an explicit expression can in general not be given for the point, where the horizontal crack starts propagating vertically.Figure 9
Example of propagation of initial horizontal crack in bottom rail and possible change to vertical propagation.In Serrano et al. [19] and Caprolu et al. [18], the perpendicular-to-grain tensile strength is assumed to be ft=2.5 MPa. If further assuming the (rolling) shear strength fv=3 MPa, inclusion of (31)-(32) leads to Figure 10 for the initially horizontally propagating crack also considered in Figure 9.Figure 10
Example of propagation of horizontal crack including possible bending and shear failure modes and change of crack propagation direction.According to Figure10, the horizontal crack will propagate to a length of 8.5 mm, and then bending failure will occur in the cantilever as given by (31).If the perpendicular-to-grain tensile strength is assumed to beft=4.5 MPa (instead of 2.5 MPa), then (31) leads to a curve very close to the curve corresponding to the vertical crack in Figure 10 and intersects with the horizontal crack curve at a=22.5 mm (for experimental results and discussion on the tensile strength value, see, e.g., Gustafsson [28], Boström [36], Holmberg [37], and Siimes [38]). The perpendicular-to-grain tensile strength of wood is always a debatable property partly due to the fact that different testing standards may lead to significantly different values, partly due to the fact that the strength is volume dependent. For a more detailed discussion, see the appendix.In the experimental programs, the length of the horizontal part of the crack before it changes direction has been measured for some of the specimens and is given in Tables4 and 5. The crack lengths were measured on the ends of the bottom rail as illustrated in Figure 11 for specimens with single- and double-sided sheathing.Figure 11
Examples of length of horizontally propagating cracks measured on the test specimens.
(a) (b) (c) (d)All test specimens had bottom rails withh=45 mm and he=22.5 mm. Accordingly, (3) and (14) predict that the crack will change to propagating in the vertical direction after having propagated 22.5 mm horizontally. Though the measured figures given in Tables 4 and 5 are roughly in agreement with this prediction, the experimental results are too scarce and the variation is too large to make any firm conclusions about agreement between theory and experiments. Further, as illustrated in Figure 10, the change of direction of the crack may not only be due to vertical crack propagation, but also due to bending failure of the cantilever beam considered in the models. The perpendicular-to-grain tensile strength of wood is associated with significant variation, and, as illustrated in Figure 10, this may lead to significant variation in the length of the horizontal crack. It is further uncertain how much the washers influence the measured horizontal cracks. The influence of the washers is not considered in any of the models presented in Section 3.1 for horizontally propagating cracks. Finally, it should be noted that the fracture models presented are all idealized models, which, for example, assume that the load is applied as a point load at the edge of the bottom rail. In reality, the load on the bottom rail is transferred by the nails over a certain length in the horizontal direction. This may have some significant effects, which are not considered in the models.It should, however, be noted that (14) for the vertical crack propagation and (31) for the bending failure of the cantilever predict infinitely high failure loads for an initially horizontal crack a=0 (le=0), and (3) and (32) will thus determine the failure load of the bottom rail for a horizontally propagating crack. For most practical applications, the shear failure will not be relevant either.A crack, which starts propagating vertically at the bottom side of the rail, will usually not change direction and start propagating horizontally if the timber is considered homogeneous and isotropic (i.e., no distinction is made between radial and tangential directions). For real orthotropic and inhomogeneous materials, the crack may, however, follow different paths as exemplified by Figures3(c) and 4(e). Figure 10 indicates that shear failure will usually not occur for horizontal cracks and is even more unlikely for vertical cracks. The failure of the rail in case of a vertically propagating crack is therefore realistically the minimum of vertical crack propagation and bending of the cantilever, that is, for instance, Min Equation (13); Equation (33).Figure12 shows a vertical crack propagation using the material properties that apply to Figure 9 and three different values of ft (=2 MPa, 3 MPa, or 4 MPa). Here the total depth of the bottom rail is assumed to be 45 mm and the vertical crack is assumed to initiate 45 mm from the loaded edge.Figure 12
Example of propagation of vertical crack including possible bending failure and the possibility for the crack to change to propagation in the horizontal direction.For the vertical crack, the bending capacity as given by (33) takes on a finite value for zero crack length and may thus overrule the fracture mechanics solution for crack propagation depending on the value of the perpendicular-to-grain tensile strength. For the example considered in Figure 12, bending failure will occur if ft=3 MPa or less; vertical crack propagation will occur if ft=4 MPa or above.Figure12 also included (3) in the following form(37)Pu=b2GGfhe12G/Ele/he2+βs,where le is the distance from the loaded edge of the rail to the crack tip and he=h-a, a being the distance of the crack tip above the bottom side of the rail. Equation (37) thus gives the load at which the crack will propagate horizontally at any stage of a vertically propagating crack.The use of (3) and (13) for an initially assumed vertical crack at the bottom surface of the bottom rail leads to the fact that the crack will continue its vertical propagation if it initiates a distance le>h from the loaded edge. Assuming le<h leads to horizontal crack propagation until le=h, and then the crack will propagate vertically. Horizontal crack propagation along the bottom side of the rail is physically not meaningful but may be interpreted in the way that (3) and (13) exclude vertical crack initiation closer to the loaded edge than the depth of the rail. This prediction seems to be roughly in agreement with the experimental observations (Figures 3 and 4). However, the alternative models for horizontal crack propagation as presented in Sections 3.1.2 and 3.1.3 predict infinitely high failure loads for he=h; that is, a horizontal crack will not propagate near the bottom surface of the bottom rail.In Figure13, (14), (23), and (28), which correspond to Models 1, 2, and 3, respectively, are for vertical crack propagation (mode 1) compared with the experimental data. Figure 13(a) refers to specimens with single-sided sheathing, while Figure 13(b) refers to specimens with double-sided sheathing. All three equations are based on the assumption that failure occurs for a→0. The following material properties were used: h=45 mm, E=400 MPa, G=70 MPa, Gf=0.30 N/mm, and βs=6/5 (for experimental results on fracture energy values, see, e.g., Smith et al. [29], Reiterer et al. [39], and Larsen and Gustafsson [40]). The effective length, le=s+c, has been used with c=20 mm which is roughly the value determined from the experimental data by minimization of the error using (13) and (35) as described in Caprolu et al. [18] for all specimens considered. The total load applied on the 900 mm long bottom rail is plotted as a function of the distance s. For double-sided sheathing, the theoretical expressions have been multiplied by two.Figure 13
Comparison between theory and experiments for vertical cracking of a bottom rail assuming zero initial crack length. (a) Specimens with single-sided sheathing and (b) specimens with double-sided sheathing. PD = pith downwards, PU = pith upwards.
(a) (b)Equations (23) and (28) lead to better agreement with the experimental data than does (14). Equations (23) and (28) differ from (14) by taking into account an additional rotation of the cantilever at the clamped end. It may be argued that the additional contribution, c, to the length of the cantilever accounts for the same effect as the additional rotation and should not be included when using (23) and (28). However, since the washer only has a very limited extension in the length direction of the bottom rail, it is not reasonable to expect that any 2D model should result in perfect agreement with tests without some kind of empirical adjustment. Use of le=s+c, c=20 mm, seems to render very good results together with (23) and (28) though the value of c has been optimized for use with (13).Figure14 compares (13) and (22) with the experimental results. Figure 14(a) refers to specimens with single-sided sheathing, while Figure 14(b) refers to specimens with double-sided. Here the initial crack length as given by (35) has been used. The same material properties as used in Figure 13 apply, and further ft=2.5 MPa has been assumed. Again le=s+c, c=20 mm, has been assumed.Figure 14
Comparison between theory and experiments for vertical cracking of a bottom rail assuming a finite initial crack length. (a) Specimens with single-sided sheathing and (b) specimens with double-sided sheathing. PD = pith downwards, PU = pith upwards.
(a) (b)While (13) in general seems to slightly overestimate the failure load for c=20 mm, (22) in general slightly underestimates the failure load. Equation (13) with the use of (35), (23), and (28) leads to approximately equally good agreement with the experimental data.In Figure15, (4), (7), and (11), which correspond to Models 1, 2, and 3, respectively, are for horizontal crack propagation (mode 2) compared with the experimental data. Figure 15(a) refers to specimens with single-sided sheathing, while Figure 15(b) refers to specimens with double-sided sheathing. All three equations are based on the assumption that failure occurs for a→0. The same material properties as used in Figure 14 together with h=45 mm and he=22.5 mm are used here.Figure 15
Comparison between theory and experiments for horizontal cracking of a bottom rail. (a) Specimens with single-sided sheathing and (b) specimens with double-sided sheathing. PD = pith downwards, PU = pith upwards.
(a) (b)Equation (11) gives a slightly better prediction of the failure load than does (4). Equation (3) used together with (35) gives very precisely the same failure load as (11). Here it may for practical reasons be recommended to use the simpler (4). It is, however, again emphasized that (11) takes into account the total depth of the bottom rail while (3)-(4) do not. If the theory is applied to bottom rails with larger depths and the sheathing is nailed to the bottom rail close to the bottom of the bottom rail, it may be significant to take into account this effect.In Caprolu et al. [22], another comparative study concerning the different models presented in this paper was presented but it compares them with other detailed experimental results, including parameter tests. The experimental study was divided into three parts with specimens matched to each other: (1) first the splitting capacity and failure mode of bottom rails subjected to uplift were studied; (2) then material properties such as tensile strength perpendicular to the grain were studied; and (3) fracture energy was determined by testing specimens cut from the specimens belonging to study (1). The experimental results were compared with the present models, using as input values results from (2) and (3). Almost all tested models did show good agreement with the test results.


## 5. Conclusions

New alternative analytical models based on fracture mechanics were presented and compared with an existing model for determination of the failure load of bottom rails subjected to uplift in partially anchored timber frame shear walls. All the models presented are based on the compliance method of fracture mechanics, and the compliance is determined using simple beam theory. Beam theory is formally not applicable to situations where the beam length is short as compared with the beam depth as is often the case in the applications to fracture problems. However, the compliance according to the simple beam theory has previously shown remarkably good results when used in fracture mechanics analysis of, for example, end-notched beams and bolted connections loading beams perpendicular to the grain.In addition to the formal problems associated with the use of beam theory for very short beams, the bottom rail analysis also includes the difficulty that it is a 3D-problem. This is due to the fact that the bottom rail is anchored to the foundation by means of anchor bolts with washers placed along the length of the bottom rail with spacing relatively large as compared with the cross section dimensions of the bottom rail. The analytical models are 2D-models, and the boundary conditions assumed in the 2D-models cannot be valid for all positions along the bottom rail. However, in spite of the seemingly oversimplified analysis, several of the models presented in this paper were found capable of giving failure load predictions in surprisingly good agreement with the experimental data. The only minor empirical adjustment made in the models is assuming that the length of the beam considered in the models for analysis of a vertically propagating crack is the distance from the loaded edge of the bottom rail to the nearest edge of the washer plus an empirically estimated length of 20 mm.For vertically propagating cracks, the existing model was found to produce excellent predictions if assuming a certain initial crack length as estimated theoretically. A new alternative model was found to produce equally good predictions if assuming that the failure load is obtained for zero crack length.For horizontally propagating cracks, the experimental data show considerably larger variation and the goodness of the models is harder to estimate. However, a new model based on a semiempirically modified quasinonlinear fracture mechanics approach was found to produce equally good predictions as the existing model. The new model has previously been applied with considerable success to analysis of splitting in beams loaded perpendicular to the grain by bolted connections and has the advantage of taking into account the total depth of the bottom rail. This effect may become significant if bottom rails with larger depths are to be analysed.In addition to failure load prediction, the capability of the simple analytical models to predict the crack propagation including change of direction of the crack was explored. The predictions seem roughly in agreement with the available experimental data. However, lack of sufficient experimental data and the large variation in the available data does not allow for any firm conclusions to be drawn.A final comparison between failure modes, with respect to the crack length, shows that the models are able to reflect the tests results with respect to the failure modes.


## 6. Code Implications

When partially anchored shear walls are used, it is necessary to specify the design of the anchoring of the bottom rail. Eurocode 5 does not give any recommendations concerning these things. The testing standard EN 594 recommends that washers of 50 mm diameter should be used for a 90 mm wide and 38 mm thick framing. For other widths and thicknesses of the timber framing, recommendations are needed in Eurocode 5.It is important to establish design rules with respect to splitting failure of the bottom rail. There is a clear relationship between the failure loads versus the distance from the edge of the washer to the loaded edge of the bottom rail.The results of this study and the study by Caprolu et al. [22] show that the failure load of the bottom rail subjected to uplift is, for vertical splitting failure, the minimum value of the failure loads given by (33) due to bending and (13) or (23) due to vertical cracking and, for horizontal splitting failure, by (31) due to bending and (3) or (11) due to horizontal cracking.



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*Source: 9402650-2016-09-20.xml*