A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.
|Publication status||Published - 7 Sep 2015|
|Event||5th CEAS Air & Space Conference 2015: Challenges in European Aerospace - Delft, Netherlands|
Duration: 7 Sep 2015 → 11 Sep 2015
Conference number: 5
|Conference||5th CEAS Air & Space Conference 2015|
|Period||7/09/15 → 11/09/15|