Static tensile and fatigue and testing of aluminium plate with holes and cracks
In an aircraft structure, fatigue failures usually started from the initiation and propagation of cracks from notches or defects. For example, an aircraft usually has a lot of rivet holes. High stress concentrations are usually found on these holes and these are the likely places for the development...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2011
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/46165 |