Abstract
Skin-stiffened composites have been extensively used in aerospace to produce lightweight structures. Stringer debonding is one of the most critical types of damage in this type of structure. Implementing a self-healing functionality within the bond line would benefit the service life of the component by repairing it when damage occurs.
| Original language | English |
|---|---|
| Pages | 41-42 |
| Number of pages | 2 |
| Volume | 54 |
| No. | 112 |
| Specialist publication | JEC Composites Magazine |
| Publication status | Published - 1 Apr 2017 |