Damage behavior in quasi-isotropic CFRP laminates with small fiber orientation angle mismatch

The use of carbon fiber reinforced plastic (CFRP) has contributed in producing light-weighted and strong aircraft structures. However, the low impact resistance of CFRP makes it easier for internal damages to occur. By using thin-ply prepeg with thickness of less than 0.05 mm, laminates with smaller...

Description complète

Enregistré dans:
Détails bibliographiques
Auteurs principaux: Nurul Nabihah A. HAMID, Hayato NAKATANI, Shinji OGIHARA
Format: article
Langue:EN
Publié: The Japan Society of Mechanical Engineers 2016
Sujets:
Accès en ligne:https://doaj.org/article/f49fc274cc2a45589c0632d93820bfd8
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!