High velocity impact response of carbon/epoxy composite laminates at cryogenic temperatures

Composite laminates are subjected to cryogenic temperatures in exposed aircraft structures during flight or in cryogenic tanks. The combination of cryogenic temperatures and high velocity impacts represents a threat to their integrity. This work investigates the behavior of carbon–epoxy laminates un...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Composites. Part A, Applied science and manufacturing Applied science and manufacturing, 2023-05, Vol.168, p.107456, Article 107456
Hauptverfasser:	Pernas-Sánchez, J., García-Rodríguez, S.M., Artero-Guerrero, J.A., López-Puente, J., Costa, J.
Format:	Artikel
Sprache:	eng
Schlagworte:	aircraft carbon Composite computed tomography Cryogenic epoxides flight Impact shear strength temperature X-ray micro-computed tomography
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!