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 |
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Pages | 41-42 |
Number of pages | 2 |
Volume | 54 |
No. | 112 |
Specialist publication | JEC Composites Magazine |
Publication status | Published - 1 Apr 2017 |