Fracture simulation model for API X80 Charpy test in Ductile-Brittle transition temperatures
Highlights
- •A fracture simulation model for API X80 steel is established in ductile-brittle transition temperatures.
- •Ductile tearing is simulated by stress modified fracture strain model which is one of damage models related with local stress triaxility.
- •Cleavage fracture is simulated by local maximum principal stress criterion based on Weibull stress.
- •The maximum principal stress can computationally replace the Weibull stress.
ABSTRACT
Keywords
Nomenclature
- A, B
- material constant in strain-based failure criteria, see Eq. (1)
- a1, a2
- fitting parameter of ductile-brittle combined failure model, see Eq. (10)
- b1, b2
- fitting parameter of σu, see Eq. (11)
- Dc
- critical damage value
- E
- ECVN
- Charpy impact test energy
- k
- material constant in modified Johnson-Cook model, see Eq. (5)
- Le
- element size
- m
- exponent of the Weibull distribution, see Eq. (9)
- Pf
- cumulative failure probability
- RA
- reduction of area
- T, Tmelt
- temperature and melting temperature (°C)
- V0
- reference volume in fracture process zone
- εep
- εf
- fracture strain
- σ1
- maximum principal stress
- σe
- equivalent stress
- σe,RT
- equivalent stress at room temperature
- σm
- σTS
- σu
- ductile-brittle failure model parameter, Weibull constant, see Eq. (9)
- σw
- Weibull stress
- σy
- yield stress
- API
- American petroleum institute
- RT
- room temperature
- CVN
- Charpy V-notch
- CMOD
- crack mouth opening displacement
- DBTT
- ductile brittle transition temperature
- FE
- finite element
- SENT
- single edge notched tension
- SMFS
- stress modified fracture strain
Abbreviations
1. Introduction
2. Summary of experiments
2.1. Tensile test

Fig. 1. (a) Schematic drawing of the tensile test specimen with the dimensions and (b) engineering stress-strain curve of the tensile test for API X80 steel at room temperature.
Table 1. Tensile properties of X80.
| T [°C] | E [GPa] | σy [MPa] | σTS [MPa] | RA [%] |
|---|---|---|---|---|
| 25 °C | 199 | 570 | 647 | 77.8 |
2.2. Single Edge Notched Tension (SENT) test

Fig. 2. (a) Schematic drawing of the SENT specimen with relevant dimensions and (b) load-CMOD and Δa-CMOD curves of the SENT test for API X80 steel at room temperature.
2.3. Charpy V-Notch Test

Fig. 3. (a) Schematic drawing of the Charpy V-notch test specimens with the dimensions and (b) energy scatter of the Charpy V-notch impact tests depending on temperature.
Table 2. 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 |
3. Ductile tearing simulation damage model
3.1. Stress-modified fracture strain damage model
3.2. Determination of ductile damage model parameters

Fig. 4. (a) FE mesh of the tensile specimen, (b) comparison of experimental engineering stress-strain curve with the simulation at room temperature and simulated tensile curve at 0°C and (c) distribution of the stress triaxiality with plastic strain extracted from the center of the FE mesh for the tensile specimen.

Fig. 5. (a) FE mesh for simulating the SENT test specimen (the minimum element size Le = 0.1 mm) and (b) multi-axial fracture strain locus for B=0 and 0.4 depending on stress triaxiality.

Fig. 6. Comparisons of (a) experimental Δa-CMOD curve, (b) experimental dΔa/dCMOD-CMOD curve and (c) experimental load-CMOD curve with the simulations results with various B values (=0, 0.2 and 0.4).

Fig. 7. Comparison of the experimental fracture surface on the SENT test with the simulated fracture surface.
3.3. Numerical prediction of Charpy energy at upper shelf temperature (0°C)

Fig. 8. (a) FE mesh for simulating the Charpy impact test with the minimum element size of Le = 0.1 mm, (b) the load-displacement curve extracted from the FE analysis at 0°C, and (c) contours of the stress triaxilaity ahead of the growing crack front from the Charpy impact test simulation at 0°C.
4. Cleavage fracture simulation model
4.1. Maximum principal stress criterion

Fig. 9. Comparison of the Weibull stress and the maximum principal stress, resulting from the present FE analysis of the Charpy test.

Fig. 10. (a) Relationship between ln(ECVN/E0) and σ1,max/σy extracted from the simulation of the Charpy tests and (b) cumulative probability of failure depending on σ1,max at -150°C.
4.2. Determination of the maximum principal stress criterion for X80
4.3. Determination of temperature-dependent σu

Fig. 11. (a) cumulative probability of failure depending on σ1,max at -90°C and (b) distribution of σu depending on temperature, determined by two different temperature data.
4.4. Charpy impact energy at Ductile-Brittle transition temperatures

Fig. 12. Prediction of the scatter of the Charpy impact test energies depending on temperature by using Eq. (12).
5. Numerical simulation of interacting ductile tearing and cleavage of Charpy tests at transition temperatures
5.1. FE analysis
- •For a given Charpy impact energy (ECVN) and temperature, determine the maximum principal stress σ1,max using Eq. (10) for the cleavage fracture simulation model
- •Perform fracture simulation using the determined criterion and the ductile fracture simulation model determined in Section 3 to compare with experimental fracture surfaces
- •During simulation, the impact energy can be also obtained and be compared with experimental input

Fig. 13. (a) schematic diagram of the simulation for interacting cleavage and ductile tearing and (b) flow chart of the fracture simulation method.
5.2. Comparison with experimental fracture surface

Fig. 14. (a) Comparisons of experimental fracture surface with the simulation at -60°C (ECVN=223.5J and σ1,max=1,740MPa) and (b) simulated load-displacement curve of the Charpy test. The gray one indicates cleavage fracture, whereas the lighter colour in FE results indicates ductile fracture surface.

Fig. 15. (a) Comparisons of experimental fracture surface with the simulation at -90°C (ECVN=78.7J and σ1,max=1,717MPa) and (b) simulated load-displacement curve of the Charpy test. The gray one indicates cleavage fracture, whereas the lighter colour in FE results indicates ductile fracture surface.

Fig. 16. (a) Comparisons of experimental fracture surface with the simulation at -120°C (ECVN=221.5J and σ1,max=1,824MPa) and (b) simulated load-displacement curve of the Charpy test. The gray one indicates cleavage fracture, whereas the lighter colour in FE results indicates ductile fracture surface.

Fig. 17. (a) Comparisons of experimental fracture surface with the simulation at -150°C (ECVN=13.0J and σ1,max=1,470MPa) and (b) simulated load-displacement curve of the Charpy test. The gray one indicates cleavage fracture, whereas the lighter colour in FE results indicates ductile fracture surface.

Fig. 18. Comparison of the measured Charpy impact energies with predicted ones from FE simulation.
6. Conclusion
CRediT authorship contribution statement
Declaration of Competing Interest
Acknowledgement
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