Loading…
Crack growth across colony boundaries in binary lamellar TiAl
The crack growth across a boundary between two colonies, i.e. regions of differing lamellar orientation, in two-phase lamellar Ti–Al is studied computationally to quantify the influence of such boundaries on toughening, as observed in recent in-situ fracture studies. The model represents the lamella...
Saved in:
Published in: | Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2002-06, Vol.329, p.532-537 |
---|---|
Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Summary: | The crack growth across a boundary between two colonies, i.e. regions of differing lamellar orientation, in two-phase lamellar Ti–Al is studied computationally to quantify the influence of such boundaries on toughening, as observed in recent in-situ fracture studies. The model represents the lamellar Ti–Al as γ-phase lamellae, modeled as bulk elastic-viscoplastic material, interspersed with α
2-phase lamellae for which either the α
2 phase or α
2–γ interface are considered as weak planes for fracture. Computationally, dynamic plane-strain analyses of the crack propagation are carried out. Fracture in both phases is accommodated using a cohesive surface formulation that permits crack growth and nucleation to evolve naturally. Results show that the lamellar misorientation across a boundary, the thickness of the boundary region, and the spatial offset between successive weak lamellae, all play a role in inhibiting crack propagation across the boundary. The γ phase plasticity has a comparatively small influence on the toughening. The enhancements in applied stress intensities required to nucleate cracks across the colony boundary are comparable to those observed experimentally when the weak-plane spacing is comparable to the spacing of microcracks and crack plane offsets observed experimentally. |
---|---|
ISSN: | 0921-5093 1873-4936 |
DOI: | 10.1016/S0921-5093(01)01504-0 |