Abstract
This work describes a mechanism for the initiation of delamination cracks in Al-Li alloys based on the soft/stiff character of adjacent grains. Small-scale-yielding, crystal plasticity simulations of divider grain configurations (L-T) reveal an elevated mean stress on grain boundaries. This mean stress increase drives a sharp localization of the Rice-Tracey parameter to the grain boundaries - elevation of the RT parameter indicates favorable conditions for void growth and triggering of delamination cracking, in agreement with the fractography of Ritchie and co-workers. Our simulation results and available experimental evidence indicate delamination initiates typically between soft/stiff grain pairs, often Bs (Bunge-convention Euler angles ϕ1=131°, Φ=83°, ϕ2=307°) or S (ϕ1=233°, Φ=151°, ϕ2=105°) orientations. The crystal plasticity results and a simple model of a soft/stiff material interface show that mean stress accumulation is a consequence of the mechanics of such an interface, and not necessarily tied to material inhomogeneities near the GBs (such as precipitate free zones).
Original language | English (US) |
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Pages (from-to) | 70-84 |
Number of pages | 15 |
Journal | Engineering Fracture Mechanics |
Volume | 133 |
DOIs | |
State | Published - Jan 1 2015 |
Keywords
- Aerospace vehicles
- Aluminum alloys
- Delamination
- Intergranular fracture
- Micromechanics
ASJC Scopus subject areas
- General Materials Science
- Mechanics of Materials
- Mechanical Engineering