Abstract
The software for calculating the interlaminar stress components around a hole in symmetric composite laminates under in-plane loading is programmed. Interlaminar stresses are obtained on basis of boundary-layer theory. Further, Hashin failure criterion is added to analyze failure regions around the hole. This software programmed with Matlab is useful for analysing composite laminates subjected to in-plane loading with curved free edges in design phase.
| Original language | English |
|---|---|
| Pages (from-to) | 633-637 |
| Number of pages | 5 |
| Journal | Jixie Qiangdu/Journal of Mechanical Strength |
| Volume | 30 |
| Issue number | 4 |
| State | Published - Aug 2008 |
Keywords
- Composite laminates with a hole
- Failure regions around the hole
- Interlaminar stresses distribution around the hole