Abstract
The influence of welding residual stresses in stiffened panels on effective stress intensity factor values and fatigue crack growth rate is studied in this paper. Interpretation of relevant effects on different length scales such as dislocation appearance and microstructural crack nucleation and propagation is taken into account using molecular dynamics (MD) simulations as well as a Tanaka-Mura approach for the analysis of the problem. Mode I stress intensity factors (SIFs), KI, were calculated by the finite element method (FEM) using shell elements and the crack tip displacement extrapolation technique. The total SIF value, Ktot, is derived by a part due to the applied load, Kappl, and by a part due to welding residual stresses, Kres. Fatigue crack propagation simulations based on power law models showed that high tensile residual stresses in the vicinity of a stiffener significantly increase the crack growth rate, which is in good agreement with experimental results.
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Abbreviations
- a :
-
half crack length
- a 0 :
-
initial crack length
- a fin :
-
final crack length
- C :
-
material constant of the Paris equation
- CRSS :
-
critical resolved shear stress
- d :
-
slip band length
- da/dN:
-
crack growth rate
- E :
-
Young’s modulus
- \( F\left(\overrightarrow{r},t\right) \) :
-
interatomic force
- F max :
-
maximum applied force
- F min :
-
minimum applied force
- G :
-
shear modulus
- K :
-
stress intensity factor (SIF)
- K appl :
-
stress intensity factor due to the applied load
- K res :
-
stress intensity factor due to welding residual stresses
- K th :
-
stress intensity factor threshold
- K tot :
-
total stress intensity factor
- m :
-
atomic mass
- m :
-
material constant of the Paris eq.
- N :
-
number of stress cycles for the fatigue crack propagation
- N f :
-
number of stress cycles for fatigue failure
- N g :
-
number of stress cycles required for crack nucleation in a single grain
- N ini :
-
number of stress cycles needed for the initiation of a small crack
- R :
-
stress ratio
- R eff :
-
effective stress intensity factor ratio
- \( U\left(\overrightarrow{r} \, ,t\right) \) :
-
interatomic embedded atom method (EAM) pair potential
- W c :
-
specific fracture energy per unit area
- ΔF:
-
applied force range
- ΔK:
-
stress intensity factor range
- ΔKeff:
-
effective stress intensity factor range
- Δσ:
-
average applied stress range
- \( \Delta \overline{\tau} \) :
-
average shear stress range on the slip band
- σ 0 :
-
yield stress
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Acknowledgments
This work was supported by the Deutsche Forschungsgemeinschaft (DFG) under Grant No. Schm 746/132-1 and as part of the Collaborative Research Centre SFB 716 at the University of Stuttgart and by the Croatian Science Foundation Grant No. 120-0362321-2198. The support is gratefully acknowledged.
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Božić, Ž., Schmauder, S., Mlikota, M., Hummel, M. (2019). Multiscale Fatigue Crack Growth Modeling for Welded Stiffened Panels. In: Schmauder, S., Chen, CS., Chawla, K., Chawla, N., Chen, W., Kagawa, Y. (eds) Handbook of Mechanics of Materials. Springer, Singapore. https://doi.org/10.1007/978-981-10-6884-3_73
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