International Journal of Mechanical Sciences
国际机械科学杂志
第 191 卷,2021 年 2 月 1 日,106103
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
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
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 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 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
- yield and tensile strength
- σw
- Weibull stress
1. Introduction
2. Drop-weight tear test (DWTT)
2.1. Material and mechanical properties

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.
Table 1. Charpy test data with temperature.
| T [ °C] | −196 | −150 | −120 | −90 | −60 | −30 | 0 |
|---|---|---|---|---|---|---|---|
| Number of specimens | 3 | 74 | 3 | 6 | 6 | 3 | 3 |
| Averaged ECVN [J] | 4.35 | 10.70 | 82.27 | 221.80 | 297.80 | 446.63 | 485.43 |
| Minimum ECVN [J] | 3.42 | 4.82 | 10.47 | 78.74 | 207.45 | 380.68 | 478.45 |
| Maximum ECVN [J] | 5.16 | 39.03 | 221.5 | 334.84 | 344.67 | 472.32 | 492.89 |

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)

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 Number | 1 | 2 | 3 | 4 | 5 | 6 |
|---|---|---|---|---|---|---|
| T [ °C] | −97 | −97 | −80 | −60 | −20 | −20 |
| Eexp [kJ] | 0.60 | 1.03 | 1.28 | 1.90 | 10.5 | 14.2 |
| Inverse fracture | No | No | No | Yes | Yes | Yes |
| Shear Area [%] | 8.5 | 11.4 | 19.5 | 40.6 | 77.9 | 69.6 |

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.
3. Numerical damage model for simulating the DWTT
3.1. The importance of an element-size-dependent damage model
3.2. Element-size-dependent ductile damage model

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. 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.

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. 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.

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

Fig. 10. Dependence of σ1,max/σy 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.

Fig. 11. Schematic illustration of the total volume calculation (VD=A*Le) of the damage elements used in the FE simulation.

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. 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

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.

Fig. 15. Flowchart of fracture simulation.
4.2. Comparisons between the experimental results and simulations

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.

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. 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. 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.

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. 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. Comparison of experimental data with simulation results. The subscript “exp” denotes the experimental values, whereas “FE” denotes the simulation results.
| Test Number | 1 | 2 | 3 | 4 | 5 | 6 |
|---|---|---|---|---|---|---|
| T [ °C] | −97 | −97 | −80 | −60 | −20 | −20 |
| Eexp [kJ] | 0.60 | 1.03 | 1.28 | 1.9 | 10.5 | 14.2 |
| EFE [kJ] | 0.66 | 1.02 | 1.21 | 1.8 | 10.7 | 12.2 |
| Shear Area [%] | 8.5 | 11.4 | 19.5 | 40.6 | 77.9 | 69.6 |
| Simulated Shear Area [%] | 6.2 | 18.1 | 21.0 | 29.9 | 81.1 | 82.6 |

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
CRediT authorship contribution statement
Declaration of Competing Interest
Acknowledgement
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