Abstract
In this paper, a Material Failure Process Analysis code (MFPA) was employed to investigate the interaction of end effect zone of specimen with the wing crack propagation inside the brittle specimen containing pre-existing flaws under uniaxial compression comparing with the experimental results. The numerical results show that the shorter the distance between the pre-existing flaw and the specimen's end, the slower the crack propagation process and the shorter wing propagation length is, and vice versa. In addition, the end effect zone was also influenced by the wing crack propagation.
© 2007 Trans Tech Publications Ltd, Switzerland
© 2007 Trans Tech Publications Ltd, Switzerland
| Original language | English |
|---|---|
| Pages (from-to) | 1049-1052 |
| Journal | Key Engineering Materials |
| Volume | 353-358 |
| Issue number | PART 2 |
| DOIs | |
| Publication status | Published - 2007 |
| Event | Asian Pacific Conference for Fracture and Strength (APCFS'06) - Sanya, Hainan Island, China Duration: 22 Nov 2006 → 25 Nov 2006 |
Bibliographical note
Publication details (e.g. title, author(s), publication statuses and dates) are captured on an “AS IS” and “AS AVAILABLE” basis at the time of record harvesting from the data source. Suggestions for further amendments or supplementary information can be sent to [email protected].Research Keywords
- Crack
- End effect
- Numerical simulation
- Pre-existing cracks
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