Elsevier

International Journal of Mechanical Sciences
国际机械科学杂志

Volume 191, 1 February 2021, 106103
第 191 卷,2021 年 2 月 1 日,106103
International Journal of Mechanical Sciences

Finite element simulation of drop-weight tear test of API X80 at ductile-brittle transition temperatures
API X80 钢在韧脆转变温度下落锤撕裂试验的有限元模拟

https://doi.org/10.1016/j.ijmecsci.2020.106103Get rights and content  获得权利和内容
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Highlights  亮点

  • Simultaneous ductile and cleavage fracture in DWTT (drop-weight tearing test) at ductile-brittle transition temperature can be simulated from presented method.
    通过所提出的方法可以模拟在延性-脆性转变温度下 DWTT(落锤撕裂试验)中同时发生的延性断裂和解理断裂。
  • For simulating ductile fracture, the stress modified fracture strain damage model is used.
    为了模拟延性断裂,采用应力修正的断裂应变损伤模型。
  • For simulating cleavage fracture, the maximum principal stress criterion is applied.
    为了模拟解理断裂,采用最大主应力准则。
  • By incorporating the element size effect on the ductile and cleavage damage models, the numerical simulation method of interacting ductile and cleavage fracture behavior of DWTT for API X80 steel is constructed.
    通过在延性损伤模型和解理损伤模型中引入单元尺寸效应,建立了 API X80 钢 DWTT 交互延性与解理断裂行为的数值模拟方法。

Abstract  抽象的

This paper proposes a method to simultaneously simulate interacting ductile and cleavage fracture in a DWTT (drop-weight tear test). The stress-modified fracture strain (SMFS) damage model is used to simulate ductile fracture and the maximum principal stress criterion is applied to simulate cleavage fracture. By incorporating the element size effect in the ductile and cleavage damage models, the numerical method to simulate the interacting ductile and cleavage fracture behavior in a DWTT is constructed. To validate the proposed method, the simulation results are compared with six API X80 data measurements at temperatures ranging between -97 °C to -20 °C. The comparison of the experimental load-displacement curve and fracture surface with the FE simulation results shows good agreement.
本文提出了一种同时模拟落锤撕裂试验(DWTT)中韧性断裂和解理断裂交互作用的方法。采用应力修正断裂应变(SMFS)损伤模型模拟韧性断裂,采用最大主应力准则模拟解理断裂。通过在韧性和解理损伤模型中引入单元尺寸效应,构建了 DWTT 中韧性断裂和解理断裂交互作用的数值模拟方法。为了验证所提方法的有效性,将模拟结果与-97 ℃至-20 ℃温度范围内的 6 个 API X80 钢种的测量数据进行了比较。实验载荷-位移曲线和断口形貌与有限元模拟结果的对比表明,两者吻合良好。

Keywords  关键词

API X80 drop-weight tear test
Ductile-brittle transition temperature
Interacting ductile and cleavage fracture
Numerical fracture simulation

API X80 落锤撕裂试验;韧脆转变温度;延性断裂与解理断裂交互作用;断裂数值模拟

Abbreviation  缩写

API
American Petroleum Institute
CTOA
crack tip opening angle
CMOD
crack mouth opening displacement
DWTT
drop-weight tear test
FE
finite element
GTN
Gurson-Tvergaard-Needleman
PN
pressed notch
SA
shear area
SENT
single-edge notched tension
SMFS
stress-modified fracture strain

API 美国石油学会 CTO 裂纹尖端张开角 CMOD 裂纹口张开位移 DWTT 落锤撕裂试验 FE 有限元 GTNGurson-Tvergaard-NeedlemanPN 压制缺口 SA 剪切面积 SENT 单边缺口拉伸 SMFS 应力修正断裂应变

Nomenclature  命名法

    A, B  A、B
    material constant in strain-based failure criteria
    基于应变的失效准则中的材料常数
    Dc
    critical damage value  临界伤害值
    Eexp
    experimental drop-weight tear test energy
    EFE
    simulated drop-weight tear test energy
    k
    material constant in the modified Johnson-Cook model, see Eq. (12)
    K
    volumetric energy density, see Eq. (8)
    Le
    element size
    m
    exponent of the Weibull distribution
    T, Tmelt
    temperature and melting temperature ( °C)
    V, V0
    volume and its reference value in fracture process zone
    VD
    total volume of damage elements, see Eq. (8)
    εep
    εf
    fracture strain
    σe
    equivalent stress
    σe,RT
    equivalent stress at room temperature
    σ1, σm
    maximum principal stress and hydrostatic stress
    σy, σTS
    σw
    Weibull stress

1. Introduction

To transport energy resources such as natural gas or crude oil over long distances, line-pipe steels with higher strengths are being required to endure higher pressures. However, at low temperatures, brittle fractures can gradually occur due to the ductile-brittle transition phenomenon. Because rapid crack propagation can be difficult to control, brittle fractures must be prevented during operation. Thus, sufficient toughness even at low temperatures is also required for safe operation in cold locations. To ensure that these requirements are met, tests must be performed. The drop-weight tear test (DWTT) is a widely used test to evaluate fracture resistance [1,2] and it is commonly known that fracture behavior is well characterized by the DWTT because the thickness of a DWTT specimen is the same as that of a pipe [3,4]. In place of an actual pipe test, the API requires the appearance of a minimum of 85% shear area on the evaluated fracture surface of a DWTT specimen [1,3]. Note that fully ductile tearing is expected in pipe fractures above the temperature showing the minimum 85% shear area from the DWTT test, according to the Battelle criterion [5].
With the continuous development of new materials with high toughness, which can exhibit various fracture characteristics, it is recommended to apply suitable experimental methods in performing DWTTs according to the properties of steel [6,7]. One example of these fracture characteristics is the so-called ‘inverse fracture’, which is defined as a cleavage fracture following an initial ductile fracture [7], [8], [9]. The inverse fracture phenomenon can be observed in high-strength and high-toughness steel. In particular, a DWTT specimen made of high-strength and high-toughness steel can be subject to large plastic deformations prior to crack initiation, and this large plastic deformation with compressive stress at the back side of a bend specimen can change the fracture behavior [10]. Thus, inverse fractures appear more frequently when high energy is required at the time of crack initiation such as in a pressed-notch DWTT specimen [7,9]. Hwang et al. [8] suggest that work hardening caused by the impact of a hammer can produce inverse fractures. Because it is preferable to prevent the occurrence of inverse fractures, the presence of which can reduce the evaluation accuracy of a DWTT [8], a DWTT was conducted with a chevron-notch to reduce the energy for fracture initiation [11,12]. However, it was determined that inverse fractures cannot be completely suppressed even with a chevron-notch DWTT specimen [8,10]. To understand and systematically analyze the inverse fracture phenomenon, numerical simulations of the complex fracture behaviors of a DWTT specimen including the occurrence of the inverse fracture phenomenon can be highly effective.
The finite element (FE) method is used not only to provide a powerful approach to predict deformations and fractures but also to simulate fracture behaviors of DWTT specimens at transition temperatures. Simulating the fracture behaviors of DWTT specimens at transition temperatures requires the simultaneous simulation of interacting ductile fracture and cleavage fracture, which has not been addressed up to now. Most of the works in the literature have considered either ductile tearing simulations or cleavage fracture simulations. For instance, using the crack tip opening angle (CTOA) concept, Fang et al. [4] and Zhen et al. [13] analyzed the ductile fracture behavior during a DWTT for various linepipe steels at room temperature. In other studies, the two-dimensional cohesive zone model was used to simulate stable ductile crack propagation in a DWTT and to determine the CTOA for pipeline steels [14,15]. Later, a similar study was performed using the three-dimensional model by Yu et al. [16] and the simulated absorption energy was compared with the experimental absorption energy. Paermentier et al. [17] simulated the ductile fracture propagation of a DWTT specimen using the Gurson-Tvergaard-Needleman (GTN) model [18], [19], [20]. The above studies performed ductile fracture simulations of DWTT specimens at upper shelf temperatures. In fact, there are many studies that provide an extension of the above ductile fracture simulation techniques that combine cleavage failure probabilities based on the Beremin model [21,22]. Hojo et al. [21] tried to find the temperature-independent Beremin parameters by combining GTN model to predict probability of failure of cracked specimens. Jang et al. [22] characterized ductile and cleavage fracture by combining the GTN and Beremin model. However, there has yet to be published a study that simultaneously simulates interacting ductile and cleavage fractures aside from our previous work. Existing studies have only calculated the cleavage failure probabilities after a certain amount of ductile fracture. Since the Weibull stress can be calculated only by post-processing of simulation results, detailed fracture surface classified by ductile or cleavage cannot be obtained from simulation. In addition, the Weibull stress approach only assumes complete cleavage fracture after exceeding a reference value, and thus cannot accommodate ductile fracture occurrence after cleavage fracture initiation.
In our previous work [23], a numerical method to simultaneously simulate interacting ductile and cleavage fractures has been proposed and applied to simulate API X80 Charpy impact tests at ductile-brittle transition temperatures. To simulate ductile tearing, the stress-modified fracture strain (SMFS) model was applied in which the fracture strain is assumed to be the inverse-exponential function of the stress triaxiality [23], [24], [25], [26], [27], [28], [29], [30]. Although the model is simple, a comparison of the simulation results with cracked pipe test data in our previous works shows that the model is quite effective and the predictions are sufficiently accurate [24,26,27,29,30]. To simulate cleavage fracture, the maximum principal stress criterion was used [23]. It should be noted that although the Weibull stress approach has been popularly used to quantify cleavage fracture [31,[42], [43], [44], [45], [46]], it can be calculated only from post-processing FE results [47], [48], [49], [50] and is, therefore, not suitable for an interacting ductile and cleavage fracture simulation. However, based on the FE analysis of the Charpy impact test, it was shown that the maximum principal stress criterion is equivalent to the Weibull stress [23]. By analyzing the Charpy impact test using FE analysis, the relationship between the Charpy impact test energy and the maximum principal stress was established as a criterion for cleavage fracture, for which the simulated fracture surfaces were in good agreement with the experimental Charpy impact test data at various temperatures, suggesting the validity of the proposed method. The cleavage fracture is also implemented by a user subroutine function when maximum principal stress in a gauss point reaches pre-defined critical value. The fracture is defined by same mechanism on ductile fracture simulation. One notable point is the element size. The element size effect on the FE damage simulation results is relatively well known [[24], [25], [26], [27],29]. This is simply because a damage model depends on the stress and strain states, which are dependent on the element size in the FE analysis. For example, for a given damage model, the predicted crack initiation and growth using a larger element size tend to be delayed. Thus, some parameters in damage models should be adjusted to compensate for the element size effect. Note that in the Charpy impact test simulation of our previous study, the element size of 0.1 mm was used without causing any numerical difficulties because the unnotched ligament size was only 8 mm for the Charpy specimen. However, it is difficult to maintain numerical stability with the use of such a small element when simulating fractures in a larger specimen with a much longer ligament. For this reason, we believe that the element size effect on a damage model is an important problem to solve when performing numerical crack growth modeling for long crack growths.
In this paper, the method to simultaneously simulate interacting ductile and cleavage fractures in our previous work is extended to simulate fractures in the DWTT of API X80. The unnotched ligament area of the present DWTT specimen is approximately 23.7 mm x 71.1 mm, whereas that of the Charpy specimen is 10 mm x 8 mm. Thus the unnotched area of the DWTT specimen is about twenty one times larger than that of the Charpy specimen. In our previous work [23], the 0.1 mm element size in a crack propagation region was used for simulating the Charpy test. The use of the same element size in simulating DWTT test is very difficult due to numerical instability, because twenty one times more elements must be failed in simulating DWTT test than in Charpy test simulation. Therefore the key point to simulate the DWTT test is to develop a damage model that incorporates the element size effect. The validity of the developed element-size-dependent damage model has to be checked by comparing with experiment data. For comparison, six DWTT tests are performed at temperatures ranging between −97 °C to −20 °C. The fracture surfaces, load-displacement curves, and energies obtained from the experimental tests are compared with those from the simulated results. Section 2 explains the materials, mechanical properties, and DWTT test results. The numerical damage models incorporating the element size effect are explained in Section 3. Section 4 compares the simulation results with the DWTT results and the conclusions are presented in Section 5.

2. Drop-weight tear test (DWTT)

2.1. Material and mechanical properties

The American Petroleum Institute (API) X80 grade steel used in our previous work [23] was used in this study as well. A tensile test was performed at room temperature (25 °C) according to the API 5 L standard [32] for a flat plate test specimen with a width of 38.1 mm, a thickness of 24.2 mm, and a gage length of 50.8 mm, taken from the plate in the hoop direction. The tensile test was loaded with a universal testing machine (UTM Zwick Roell, 1200 kN). The engineering stress-strain curve is shown in Fig. 1(a) with the tensile properties (yield stress, σy, tensile stress, σTS, and elastic modulus, E).
Fig 1
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Fig. 1. (a) Tensile properties (elastic modulus, yield/tensile strength, and reduction of area, RA) and engineering stress-strain curve for API X80 steel at 25 °C and (b) variation in the Charpy impact energy with temperature for API X80 steel at ductile-to-brittle transition temperatures.

Charpy impact tests were also performed at various temperatures using standard specimens with a 10 mm x 10 mm cross-section and a central 45° V-notch of 2 mm depth according to API 5 L [32]. Total ninety-eight specimens were tested from −196 to 0 °C. Variations of the impact energies with temperature are shown in Fig. 1(b) and minimum, averaged and maximum impact energies are summarized in Table 1 for the given temperature, together with the number of tests.

Table 1. Charpy test data with temperature.

T [ °C]−196−150−120−90−60−300
Number of specimens37436633
Averaged ECVN [J]4.3510.7082.27221.80297.80446.63485.43
Minimum ECVN [J]3.424.8210.4778.74207.45380.68478.45
Maximum ECVN [J]5.1639.03221.5334.84344.67472.32492.89
To measure crack growth resistance, a single-edge notched tension (SENT) test was performed at room temperature according to the recommended practice in the DNV RP-F108 [33]. The relevant dimensions of the SENT specimen are shown in Fig. 2(a). The specimen was clamped using hydraulic grips and loaded in the controlled displacement mode and unloaded controlled load mode. The crack mouth opening displacement (CMOD) was measured by a clip gage. Detailed dimensions are shown in Fig. 2(a). After machining 7 mm crack with an EDM, fatigue pre crack was additionally inserted. The total initial crack size is measured by 10.03 mm. To measure the crack extension, the compliance method suggested in the BS 8571 [34] was used [35], [36], [37]. The resulting variations in the load and crack extension (Δa) with the CMOD (crack mouth opening displacement) are shown in Fig. 2(b). Later in Section 3.2, the Δa-CMOD curve is used to determine the damage model for ductile fracture. For this purpose, the experimental data are fitted using a power-law equation which is shown in Fig. 2(b).
Fig 2
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Fig. 2. (a) Schematic illustration of the single edge notched tension (SENT) test specimen with dimensions and (b) experimental load-CMOD and Δa-CMOD curves of the single edge notched tension test for API X80 steel at 25 °C. A power-law fit to the Δa-CMOD curve is also shown and given.

2.2. Drop-weight tear test (DWTT)

A drop-weight tear test (DWTT) of API X80 steel was conducted at various temperatures according to the ASTM E436 [2]. The DWTT and specimen are schematically shown in Fig. 3(a) with the a central 45° pressed notch of 5.08 mm depth. A DWTT testing machine (DWTT-100F) with the maximum energy capacity of 100 kJ was used. To apply sufficient energy to split the DWTT specimen, the hammer fell from a height of 2 m giving ~6 m/s speed at the impact. The anvil was fixed on both sides, and a three point-bending load was applied to the DWTT specimen. Load-load line displacement curves were obtained from the instrumented DWTT system. Total six tests at various temperatures were carried out to observe various characteristics on the fracture surface. The data for the six tests, such as temperature, measured energy, and percentage shear area (SA), are given in Table 2. Note that the tests are numbered according to the temperature and the fracture energy.
Fig 3
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Fig. 3. (a) Schematic illustration of drop-weight tear test and specimen including dimensions and (b) measured experimental load-load line displacement curves of six test cases at various temperatures, summarized in Table 2.

Table 2. Summary of six drop-weight tear test data: temperature T, measured energy Eexp, and measured shear area. The presence of the inverse fracture surface is also indicated.

Test Number123456
T [ °C]−97−97−80−60−20−20
Eexp [kJ]0.601.031.281.9010.514.2
Inverse fractureNoNoNoYesYesYes
Shear Area [%]8.511.419.540.677.969.6
Experimental load-load line displacement curves are shown in Fig. 3(b). Although it is difficult to identify the experimental data for the different conditions in this figure, each curve is compared with simulated results in the later Section 4.2. The fracture energy Eexp can be measured from the load-load line displacement curve and is summarized in Table 2. These values are used to predict the maximum principal stress criteria that cause cleavage fracture in the simulations of the DWTT in the later Section 4.2.
Fig. 4 shows the fracture surfaces from the six DWTTs. According to Hong et al. [3], fracture surfaces can be classified into four regions: (1) cleavage fracture; (2) ductile fracture; (3) delamination; and (4) inverse fracture. In the cases of Tests 1–3 at low temperatures, cleavage fracture is dominant in the central part of the surface, continuing from the initial notch tip to the end of the specimen. A small ductile fracture region is observed only near the surface. With increasing test temperatures, the fraction of cleavage fracture decreases, whereas the fractions of ductile fracture and delamination increase, as shown with Tests 4–6. According to the API RP 5L3 [1], delamination is defined as a cleavage fracture when it is wide because it appears almost in the surface fractured by the cleavage. In contrast, when delamination is deep and shallow, it can be defined as ductile fracture because it is included almost in the ductile fracture surface. According to this definition, the delamination shown in Fig. 4 can be classified mainly as ductile. Inverse (cleavage) fracture is also observed in Fig. 4 with Tests 4 to 6, in which the ductile fracture forming after the cleavage fracture changes back to cleavage fracture. It is located near the hammer impact region (which is classified as a ductile fracture [7]) and appears distinctly at relatively high temperatures. Sung et al. [7] and Hwang et al. [9] pointed out that, in the case of pressed notched DWTT specimens, a high energy is required at the notch to initiate the fracture, resulting in an inverse fracture. Because higher energy is also required to initiate the fracture at a relatively high temperature, the inverse fracture was more clearly observed in Tests 5–6 performed at −20 °C.
Fig 4
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Fig. 4. Fracture surfaces of six drop weight tearing tests at various temperatures. See Table 2 for detailed test information is summarized in Table 2. Fracture surfaces are identified as ductile fracture surface (including hammer impact region), cleavage fracture surface and delamination region.

From the tested fracture surface, the shear area was calculated with the thickness according to the ASTM E436 [2] in the middle region excluding the initial notch tip and the end of the specimen. Note that if the thickness of the DWTT specimen exceeds 19 mm, the length of the section excluded when calculating the shear area should be set to 19 mm and not to the thickness value. Because the thickness of the DWTT specimen used in this study was 23.7 mm, 19 mm was excluded from both sides when calculating the shear area, as shown in Fig. 4. The fracture surface types were manually classified with the photographs and the percentage shear area was calculated by an image analyzer. The calculated shear areas are given in Table 2 and are compared with simulated results in the later Section 4.2.

3. Numerical damage model for simulating the DWTT

3.1. The importance of an element-size-dependent damage model

In our previous work [23] in which the same material was considered, the minimum element size of 0.1 mm was used in the FE model to simulate fractures in the Charpy test at ductile-brittle transition temperatures. The use of a 0.1-mm element size was possible because the ligament length in the Charpy specimen was only 8 mm. However, the fracture simulation of large-scale specimens or pipes can be of practical interest. For instance, the DWTT specimen considered in this paper has the ligament size of approximately 72 mm, which is approximately ten times larger than the Charpy specimen. The length scale of large-scale pipes can be much longer. One of the challenges in simulating fractures in large-scale components is the finite element size used in the simulation. Because the element deletion technique is generally used to simulate fractures, the use of a small element size such as 0.1 mm in the simulation of large-scale components can cause numerical instability. One possible way to improve numerical stability is to use a larger element size. Therefore, because calculated stresses, strains, and damage depend on the element size, the parameters in a damage model can also depend on the element size.
In the following sub-sections, the ductile fracture and cleavage damage models proposed in our previous work [23] are extended to incorporate the element size effect, which is then used to simulate fracture in the DWTT specimen.

3.2. Element-size-dependent ductile damage model

In our previous study [[23], [24], [25], [26],29,30], the stress-modified fracture strain (SMFS) model was used to simulate ductile fracture (tearing), in which the multi-axial fracture strain εf is given by the exponential function of the stress triaxiality [[23], [24], [25], [26],29,30].(1)εf=A·exp[1.5·σmσe]+B
For API X80, the material constants A and B were determined by analyzing the tensile and single-edge-notched tension (SENT) test data using FE simulations and are A = 3.34 and B = 0.4 [23].
The incremental damage is defined as the ratio of increments of equivalent plastic strain to the multi-axial fracture strain as follows:(2)ΔD=Δεepεf
When the accumulated damage reaches a critical damage value Dc(3)ΔD=Δεepεf=Dcthe element is removed using ABAQUS [39] user subroutines to simulate local ductile fracture. In the simulation, when the accumulated damage reached the critical damage value, the equivalent stress was decreased with the slope of −5000 MPa to 10 MPa. The elastic modulus was also reduced to 100 MPa. Finally, to completely remove the element, the “ELEMENT DELETION” option in ABAQUS was applied.
In our model, the fracture strain locus given by Eq. (1) is regarded as one of the material properties and is, therefore, not dependent on the element size. However, the value of Dc is assumed to depend on the element size [[24], [25], [26], [27],29]. In our previous work [23], it was found that Dc=1 for the minimum element size of 0.1 mm to simulate fractures in the Charpy test. The FE mesh for simulating SENT test with Le=0.1 mm in the crack propagation area is shown in Fig. 5 and the comparison between the simulated results and experimental results for the experimental load-CMOD, crack extension(Δa)-CMOD, and dΔa/dCMOD-CMOD curves is shown in Fig. 6(a). Note that for the dΔa/dCMOD-CMOD curve, two experimental data plots are shown: one is the direct differentiation of experimental data (showing large scatter) and the other is the fitted equation given in Fig. 2(b).
Fig 5
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Fig. 5. Three FE meshes used to simulate the single-edge notch tension test with different minimum element sizes in the crack propagation region (Le = 0.5 mm, 0.2 mm, and 0.1 mm).

Fig 6
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Fig. 6. Comparisons of (a) experimental load-CMOD and Δa-CMOD results with the simulation using Le=0.1 mm and (b) dΔa/dCMOD-CMOD results with the simulations using Le=0.1 mm with Dc=0.8, 1.0, and 1.2.

When a different size of the element is used, a proper Dc value must be chosen. The FE meshes with Le=0.2 and 0.5 mm are also shown in Fig. 5. The effect of the element size (Le) and Dc on simulated dΔa/dCMOD-CMOD results are compared with experimental data in Fig. 7(a) for Le=0.2 mm and in Fig. 7(b) for Le=0.5 mm. For Le=0.2 mm in Fig. 7(a), it can be observed that the use of Dc=0.85 yields nearly similar results compared with the results for Le=0.1 mm in Fig. 6(b), which was presented in our previous work [23]. Although the results using Le=0.5 mm do not match experimental data as well as those using other element sizes, Fig. 7(b) shows that it may be advantageous to use Dc=0.65. Fig. 7(c) and (d) compare the results for the three different element sizes with different values of Dc. It can be observed that the choice of Dc=0.65 for Le=0.5 mm yields a slightly delayed crack initiation and a faster crack growth rate than the other cases with different element sizes but is quite similar to the load-CMOD response, rendering it the most suitable. To further confirm whether such a choice is appropriate, the simulated fracture surface is also compared with experimental results in Fig. 8. For comparison, the simulation result using Le=0.1 mm is also shown where it can be observed that both simulated fracture surfaces using Le=0.1 mm and Le=0.5 mm agree well with experimental data.
Fig 7
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Fig. 7. Effect of Dc on simulated dΔa/dCMOD-CMOD curves for (a) Le=0.2 mm and (b) Le=0.5 mm. (c)-(d) Comparison of experimental dΔa/dCMOD-CMOD, load-CMOD, and Δa-CMOD curves with simulation results using three different element sizes (Le=0.1 mm, 0.2 mm, and 0.5 mm).

Fig 8
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Fig. 8. Comparison of the fracture surface from the FE simulation with the SENT test; (a) Le=0.1 mm and (b) Le=0.5 mm. In each figure, the left side of the figure is experimental data and the right side of the figure is the simulation result. The initial notch tip and final crack front are indicated in the figures.

In the simulated DWTTs presented later in this paper, the element size of 0.5 mm was selected for computational efficiency; thus, the following SMFS model was used:(4)εf=3.34·exp[1.5·σmσe]+0.4,Dc=0.65forLe=0.5mm
To further confirm whether the proposed damage model for the different element sizes is appropriate, the FE simulation for the Charpy V-notch test at 0 °C, performed in our previous work [23] using an element size of 0.1 m, was repeated using different element sizes (0.2 mm and 0.5 mm). The corresponding FE meshes are shown in Fig. 9(a), and the resulting simulation results are compared in Fig. 9(b), which shows that the simulated load-displacement curve and impact energy follow a similar trend, supporting the efficacy of the element-size-dependent ductile damage model used in this paper.
Fig 9
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Fig. 9. (a) FE meshes for simulating the Charpy impact test performed at 0 °C with three different minimum element sizes (Le=0.1 mm, 0.2 mm, and 0.5 mm) and (b) the effect of the minimum element size on simulated load-load line displacement curves.

3.3. Element-size-dependent cleavage fracture model

In our previous work [23], to simulate cleavage fracture, we applied the maximum principal stress criterion, which is equivalent to the Weibull stress approach [31]. The definition of the Weibull stress is given by(5)σw=(1V0V(σ1)mdV)1mwhere σ1 is the maximum principal stress distributed on a fracture process zone V, the Weibull parameter m is the material constant, and V0 is an arbitrarily chosen reference volume. Although the Weibull stress is a widely-used criterion to characterize cleavage fracture, it can be calculated only by post-processing the finite element (FE) analysis. Thus, it is difficult to simulate the combined ductile and cleavage fracture behavior. To overcome this problem, the maximum principal stress criterion within an element was proposed and shown to be equivalent to the Weibull stress criterion(6)σw(V0)(1V0i=1ne(σ1i)mVi)1m(VV0)1mσ1,maxwhere σ1,max denotes the maximum principal stress over V. The Weibull stress is proportional to the largest maximum principal stress within the fracture process zone V. The reference volume can be conveniently assigned to satisfy V/V0=1 [23], which makes the Weibull stress numerically equal to the largest maximum principal stress. Therefore, the maximum principal stress can be applied to verify the element-wise cleavage fracture.
In our previous paper [23], the following relationship between the maximum principal stress and the fracture energy of API X80 was suggested by the FE simulation of Charpy impact test data:(7)σ1,maxσy(T)={0.40·ln(EE0)+1.83forln(EE0)2.070.10·ln(EE0)+2.45forln(EE0)2.07where E0=4.82 J (the minimum Charpy energy tested at −150 °C). Eq. (7) is shown in Fig. 10(a). In Eq. (7), the temperature-dependent yield stress value should be used for σy. Note that the constants in Eq. (7) were determined for the element size of 0.1 mm.
Fig 10
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Fig. 10. Dependence of σ1,maxy on the normalized fracture energy calculated from the Charpy impact test simulation: (a) normalized with respect to constant E0 (=4.82 J) and (b) normalized with respect to Eq. (8), E0=K*VD.

To incorporate the element size effect on the maximum principal stress criterion to simulate cleavage fracture, E0 in Eq. (7) is re-defined as(8)E0=K·VDwhere K is the volumetric energy density [J/mm3] and VD denotes the total volume of damage elements in the FE simulation. In the FE analysis, a fracture is simulated by removing the elements in the first layer in front of the notch tip, as shown in Fig. 11. The volume VD is the total volume of the first layer elements. For instance, when the element size of Le is used for the Charpy specimen, the volume VD can be calculated as VD=2*Le*A where A is the un-notched (un-cracked) area. The factor 2 is introduced for the symmetry condition along the crack propagation line; two elements are removed as crack growth. For the Charpy specimen, A=(8 × 10) mm2. Thus, with an element size of 0.1 mm, VD=(2 × 0.1 × 8 × 10) mm3 and with an element size of 0.5 mm, VD=(2 × 0.5 × 8 × 10) mm3. The constant K in Eq. (8) can be determined as K = 4.82 J/(2 × 0.1 × 8 × 10) mm3=0.30125 J/mm3. Note that E0=4.82 J was assumed for Le=0.1 mm in our previous paper [23].
Fig 11
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Fig. 11. Schematic illustration of the total volume calculation (VD=A*Le) of the damage elements used in the FE simulation.

Combining Eqs. (7) and (8) gives(9)σ1,max(E)σy(T)={0.40·ln(EK·VD)+1.83forln(EK·VD)2.070.10·ln(EK·VD)+2.45forln(EK·VD)2.07
The simulation results of the Charpy test using different element sizes of Le=0.1 mm, 0.2 mm, and 0.5 mm are compared with Eq. (9) as shown in Fig. 10. In Fig. 10(a), the constant value of E0 (=4.82 J) is used, whereas in Fig. 10(b), the proposed value of E0 (=KVD) is used. Note that the calculated E0=4.82 J for Le=0.1 mm, E0=9.84 J for Le=0.2 mm, and E0=24.1 J for Le=0.5 mm. These results show that the use of the proposed Eq. (8) gives predictions less sensitive to the element size, although the results using the largest element size Le=0.5 mm consistently show less accuracy than those using smaller element sizes. This is because the 0.5-mm element size may be too large for the Charpy specimen where the unnotched ligament is only 8 mm. Therefore, to use an element size of 0.5 mm to predict fracture behavior in a DWTT, the constants in Eq. (9) should be slightly modified as follows:(10)σ1,max(E)σy(T)={0.37·ln(EK·VD)+1.66forln(EK·VD)1.890.10·ln(EK·VD)+2.17forln(EK·VD)1.89
The two lines in Eq. (10) are shown in Fig. 10(b) as dotted lines. For the present purpose, determining Eq. (10) is sufficient, but, in principle, the constants in Eqs. (9) and (10) can be found as a function of the element size. Note that for the DWTT data considered in this work, only the first equation is relevant.
To further investigate the applicability of the 0.5-mm element size, two Charpy tests at 150 °C and −90 °C, producing the Charpy impact energies of ECVN=13.0 J and 78.7 J, respectively, were simulated using two different element sizes, Le=0.1 mm and 0.5 mm. The resulting fracture surface and calculated energies are compared with experimental data in Fig. 12, Fig. 13. The gray color in the figures indicates the simulated cleavage fracture surface. The locations and sizes of the cleavage fracture from the simulations using the two different element sizes are similar. As shown in Fig. 12(a), the calculated fracture energy is ECVN=11.6 J for Le=0.1 mm at −150 °C, which is approximately 11% lower than the measured value of ECVN=13.0 J. In Fig. 12(b), the calculated value is ECVN=13.9 J for Le=0.5 mm, which is 7% higher than the measured value. The corresponding results at −90 °C are shown in Fig. 13.
Fig 12
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Fig. 12. Comparison of the simulated fracture surface with the Charpy test at −150 °C (with experimental energy ECVN=13.0 J); (a) results using Le=0.1 mm (simulated energy ECVN=11.6 J) and (b) results using Le=0.5 mm (simulated energy ECVN=13.9 J). In the simulated surface, the dark gray color indicates cleavage fracture, whereas the lighter color in the FE results indicates a ductile fracture surface.

Fig 13
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Fig. 13. Comparison of the simulated fracture surface with the Charpy test at −90 °C (experimental energy ECVN=78.7 J); (a) results using Le=0.1 mm (simulated energy ECVN=104.4 J) and (b) results using Le=0.5 mm (simulated energy ECVN=78.2 J). In the simulated surface, the dark gray color indicates cleavage fracture, whereas the lighter color in the FE results indicates a ductile fracture surface.

4. Simulation of DWTT and comparison with test data

4.1. FE model and analysis of DWTT specimen

The DWTTs at various temperatures were simulated using the presented method incorporating the element size effect and compared with experimental data. For numerical stability and efficiency, the element size of 0.5 mm was used along the crack propagation surface in the FE model of the DWTT specimen. The calculations terminated when smaller sizes for the elements such as 0.1 mm or 0.2 mm were used. The quarter model consisting of eight-noded solid elements (C3D8 in ABAQUS) was used for all DWTT simulations. The FE mesh is shown in Fig. 14 with 19,312 elements and 22,951 nodes.
Fig 14
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Fig. 14. FE mesh used to simulate the DWTT test with the minimum element size of Le=0.5 mm in the crack propagation region.

The numerical simulation of the DWTT at ductile-brittle transition temperatures was performed. For the tensile properties, the temperature-dependent properties proposed in Canada [38] were used and can be expressed as(11)σ=σe,RT(1λ|T|*k);λ={1:T=TroomT*|T|*:TTroom,T*=TTroomTmeltTroomwhere σe,RT indicates the equivalent stress at room temperature. The values of k and Tmelt are assumed to be 0.81 and 1500 °C, respectively [38]. The strain rate effect on the tensile properties is not considered in this work.
To simulate the DWTT conditions, a hammer and anvil were modeled as a rigid shell constrained to a reference point, as shown in Fig. 14. The impact load was applied to the reference point using the velocity control option offered in ABAQUS/Implicit [39]. At impact, the experimental hammer speed of 6 m/s was used in the analysis with the large geometry change option. All degrees of freedom for the anvil were fixed, and the hammer could move only vertically. The increment in the dynamic analysis was limited to move the hammer by 60 mm after 0.01 s with the automatic adjustment of the time increment. The mass density of 7900 kg/m3 was assigned to the DWTT specimen.
During the analysis, ductile and brittle fractures were simulated as follows. To simulate ductile fracture, the incremental ductile damage is calculated at the Gauss point in an element by Eqs. (1) and (2), given in Section 2.1. When the accumulated damage reaches the critical damage value (for the element size of 0.5 mm, the critical value was Dc=0.65), the elastic modulus and equivalent stress are reduced to small values to simulate ductile fracture. Detailed information is provided in our previous paper [23]. To simulate cleavage fracture, the maximum principal stress σ1,max should be calculated using Eq. (10) for the given experimentally-measured DWTT energy. Note that the unnotched ligament area of the DWTT specimen is A = 1685.5 mm2, and thus Eo=K•VD=507.77 J was used based on the element size of 0.5 mm. When the maximum principal stress calculated at the Gauss point in an element exceeds the criterion σ1,max, the technique used to simulate ductile fracture is also applied to simulate cleavage fracture, namely, the elastic modulus and equivalent stress are reduced to small values. The flowchart of fracture simulation is shown in Fig. 15. In each increment, the maximum principal stress and the plastic damage according to Eq. (2) is calculated. If the maximum principal stress is greater than σ1,max but the accumulated plastic damage does not satisfy the ductile fracture criterion, Eq. (3), this element is assumed to be failed by cleavage and the element is removed by reducing the stresses and elastic modulus to small values, as described above. On the other hand, if the maximum principal stress is less than σ1,max and the accumulated plastic damage satisfies the ductile fracture criterion, this element is assumed to be failed by ductile and the element is removed by reducing the stresses and elastic modulus to small values. When the maximum principal stress is less than σ1,max and the accumulated plastic damage does not satisfy the ductile fracture criterion, the accumulated plastic damage is updated and saved for the next increment. It should be noted that ductile and cleavage fracture is assumed to be independent, and thus the accumulated plastic damage does not affect the cleavage fracture.
Fig 15
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Fig. 15. Flowchart of fracture simulation.

From the FE simulation, the following data are obtained and compared with the experimental data. The first is the load-displacement curve, under which the calculated area is used to determine the DWTT energy, which is also compared with the experimental value (used as input for the FE analysis). The second is the fracture surface from which the shear area (percentage ductile fracture area) can be calculated and also compared with the experimental data. Finally, the occurrence of inverse fracture (or abnormal fracture) in the simulation is similarly evaluated.

4.2. Comparisons between the experimental results and simulations

Fig. 16 compares the fracture surface of the DWTT results at −97 °C with the simulation results. The experimentally-measured energy Eexp, given in the captions, is used to calculate the maximum principal stress with Eq. (10). The calculated σ1,max is also given in the captions. In Fig. 16(a), the fracture surfaces from the experiment and FE simulation are compared. The experimental fracture surface is divided into two fracture modes: ductile and cleavage fracture, according to Sung et al. [7]. In the simulated surface, the black color indicates cleavage fracture, whereas the lighter color indicates ductile fracture. In both the experiment and simulation, cleavage fracture started and continued from the center of the notch tip to the end of the specimen. Ductile fracture only appears on the specimen surface due to the lower plastic constraint. The predicted load-load line displacement curve is compared with experimental data in Fig. 16(b), showing good agreement. Note that the experimental data contain oscillations due to the impact of the hammer. The calculated fracture energy for Test 1 was EFE=0.66 kJ, which is only 10% greater than the measured fracture energy Eexp=0.6 kJ.
Fig 16
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Fig. 16. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −97 °C (Test 1, Eexp=0.60 kJ and σ1,max=1097 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

The corresponding results for Test 2 are shown in Fig. 17. This test was performed at −97 °C, similar to Test 1, but it produced a higher energy than Test 1 (Eexp=1.03 kJ compared with Eexp=0.60 kJ for Test 1). In the experiment, the fracture surface is quite similar to that of Test 1 but shows more ductile fracture area near the specimen surface. Tani et al. [51] investigated relationships between the Charpy energy and a distance triggering brittle fracture. They showed that the variable distribution of the distance of brittle fracture initiation factors caused the scatter of the Charpy impact energy. In the DWTT test, such brittle fracture initiation factors could exist, which in turn produce the scatter in DWTT energies and fracture surfaces. Thus it would be quite difficult to simulate fracture surfaces in cleavage-dominant cases. Fig. 18 compares the test data at −80 °C (Eexp=1.28 kJ) with the simulation results. Again, the fracture surface is similar but demonstrates more ductile fracture. It can be observed that for both the experimental and simulated cases, the fracture surfaces and load-displacement curves agree well. Additionally, the predicted fracture surfaces are similar to experimental fracture surfaces, and the predicted energies are close to the measured energies: EFE=1.02 kJ for Test 2 and EFE=1.21 kJ for Test 3.
Fig 17
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Fig. 17. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −97 °C (Test 2, Eexp=1.03 kJ and σ1,max=1220 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

Fig 18
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Fig. 18. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −80 °C (Test 3, Eexp=1.28 kJ and σ1,max=1253 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

Fig. 19 compares the simulation results with the experimental data at −60 °C (Test 4) with a measured energy of Eexp=1.9 kJ. It can be observed that the fracture surface from the experiment includes one more region (delamination) in the ductile fracture area. Babinsky et al. [40] suggested that delamination occurs as a result of brittle fracture, and Joo et al. [41] suggested that the maximum principal stress may promote delamination for API X80 steel. Thus, the delamination can be considered as cleavage fracture. In the simulation, both the cleavage fracture in the center region and the ductile fracture on the specimen surface can be simulated well. Furthermore, the delamination region inside the ductile fracture region can be successfully predicted as cleavage fracture, as shown in Fig. 19(a). The predicted load-load line displacement curve is compared with the experimental data in Fig. 19(b), showing good agreement. In addition, the predicted energy (EFE=1.8 kJ) is very close to the measured energy Eexp=1.9 kJ.
Fig 19
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Fig. 19. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −60 °C (Test 4, Eexp=1.9 kJ and σ1,max=1323 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

The simulation results at −20 °C are compared with experimental data in Fig. 20 for Test 5 and in Fig. 21 for Test 6. Note that the measured energies are quite high: Eexp=10.5 kN for Test 5 and Eexp=14.2 kJ for Test 6. The experimental load-displacement curves show a rather smooth decrease from the maximum load due to the larger proportion of ductile fracture. The simulation can well predict not only the maximum load but also the slope of the load drop. The predicted energies are relatively close to the experimental values: EFE=10.7 kJ for Test 5 and EFE=12.2 kJ for Test 6. Due to the high absorbed energy, more ductile fracture surface can be observed compared with the previous cases. The cleavage fracture initiates from the notch tip, propagates for a short distance, and then changes to ductile fracture. The initial cleavage fracture surface in Fig. 20(a) shows a triangle shape in both experiment and simulation. Hong et al. [3] performed DWTT tests with various specimen thicknesses for API X70 and X80 steel, and observed a triangle shape for the initial cleavage fracture surface for the pressed notch DWTT tests. After ductile fracture propagation with small delamination and cleavage fracture surfaces, the fracture in the center of the specimen becomes cleavage fracture. This phenomenon is referred to as the “inverse fracture” in the literature (see for instance Hwang et al. [9]). As shown in Figs. 20(a) and 21(a), the inverse fracture pattern can be also predicted in the simulation.
Fig 20
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Fig. 20. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −20 °C (Test 5, Eexp=10.5 kJ and σ1,max=1648 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

Fig 21
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Fig. 21. Comparisons of simulated fracture surface and load-load line displacement curve with the experimental results at −20 °C (Test 6, Eexp=14.2 kJ and σ1,max=1714 MPa); (a) fracture surface and (b) load-displacement curve. In the simulated surface, the cleavage fracture surface is shown in black and the ductile fracture surface in light gray.

Table 3 summarizes the main results of the experiment and FE simulation, which are also presented in Fig. 22 in graphical form. The DWTT energies predicted by the simulation are very close to those measured in the experiments, except in Test 6 where the predicted energy is approximately 14% lower than the experimental value, a difference of which is still small for predictions at ductile-brittle transition temperatures. Typically, for shear area predictions, differences tend to be larger. However, the maximum difference between experimental values and predicted values for the shear area is within 18% (observed in Test 6), which can be regarded as a good prediction since large shear area cases are usually more relevant.

Table 3. Comparison of experimental data with simulation results. The subscript “exp” denotes the experimental values, whereas “FE” denotes the simulation results.

Test Number123456
T [ °C]−97−97−80−60−20−20
Eexp [kJ]0.601.031.281.910.514.2
EFE [kJ]0.661.021.211.810.712.2
Shear Area [%]8.511.419.540.677.969.6
Simulated Shear Area [%]6.218.121.029.981.182.6
Fig 22
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Fig. 22. Comparison of (a) experimental DWTT energy Eexp with the simulation results for EFE, and (b) measured experimental shear area with the simulation results.

5. Conclusion

This paper proposes a method to simultaneously simulate interacting ductile and cleavage fracture in which the simulation results are compared with six API X80 DWTT data at temperatures ranging between −97 °C to −20 °C. This method is an extension of our previous method for simulating the Charpy impact test [23] by incorporating the element size effect on the ductile and cleavage damage models, which is a crucial aspect in the present method for the fracture simulation of larger-scale structures. For the ductile damage model, the stress-modified fracture strain (SMFS) model that was used in our previous work is incorporated with the element size effect by introducing the element-size-dependent critical damage model in this work. For the cleavage damage model in our previous study, a maximum principal stress criterion was proposed and the relationship between the maximum principal stress and Charpy impact energy was established. In this work, the energy is re-defined using the element-size-dependent volume with the relationship determined to be a function of the element size.
From the DWTT, the load-displacement curve and absorbed energy are measured. Using the measured energy, the cleavage fracture criterion is determined and the DWTT simulation is performed. The simulated load-displacement curves and absorbed energies are in good agreement with all six test data. Furthermore, the simulation is shown to reproduce experimental fracture surfaces of not only ductile and cleavage fracture surfaces but also inverse fracture surfaces. The good agreement between experimental values and simulated values in this study indicates the effectiveness and accuracy of the proposed method in simultaneously simulating interacting ductile and cleavage fracture for large-scale specimens or pipes. The key point to make simulating interacting ductile and cleavage fracture for large-scale specimens or pipes possible is to properly incorporate the element size effect into a damage model. When the fracture area to be simulated becomes larger, the element size used in simulation needs to be adjusted because the use of a small element can cause numerical instability due to the fact that the number of elements to be failed increases substantially. Although there are some methods available to minimize the element size effect in damage analyses such as non-local approach, the method proposed in this paper is more straightforward and easily implemented. For ductile fracture simulation, for instance, the authors have already shown the effectiveness of the present approach in simulating long ductile tearing in full-scale piping components [26,27,29].
Finally, the proposed method can offer an effective tool to investigate the variables that contribute to the occurrence of inverse fractures in high-strength pipeline materials. For instance, the effects of the presence of a Chevron notch, material strength and ductility, specimen width, and loading conditions on the occurrence of inverse fractures can be evaluated using the method proposed in this work.

CRediT authorship contribution statement

Ji-Su Kim: Conceptualization, Methodology, Formal analysis, Writing - original draft, Visualization. Yun-Jae Kim: Validation, Writing - review & editing, Supervision, Project administration. Myeong-Woo Lee: Software, Formal analysis. Ki-Seok Kim: Investigation, Resources. Kazuki Shibanuma: Validation, Writing - review & editing.

Declaration of Competing Interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Acknowledgement

This work was supported by POSCO [2017R240], and the Korea Agency for Infrastructure Technology Advancement [17IFIP-B067108-05].

References

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