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Dislocation Nucleation Mediated Plasticity of FCC Nanowires Read chapter Read first chapter

2019 | OriginalPaper | Chapter

37. Multiscale Fatigue Crack Growth Modeling for Welded Stiffened Panels

Authors : Ž. Božić, Siegfried Schmauder, M. Mlikota, M. Hummel

Published in: Handbook of Mechanics of Materials

Publisher: Springer Singapore

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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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previous chapter Defect Accumulation in Nanoporous Wear-Resistant Coatings Under Collective Recrystallization: Simulation by Hybrid Cellular Automaton Method
next chapter Dislocation Density-Based Modeling of Crystal Plasticity Finite Element Analysis
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Metadata
Title
Multiscale Fatigue Crack Growth Modeling for Welded Stiffened Panels
Authors
Ž. Božić
Siegfried Schmauder
M. Mlikota
M. Hummel
Copyright Year
2019
Publisher
Springer Singapore
Book
Handbook of Mechanics of Materials

Print ISBN: 978-981-10-6883-6

Electronic ISBN: 978-981-10-6884-3

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-981-10-6884-3_73

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