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

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...

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Autores principales: Nurul Nabihah A. HAMID, Hayato NAKATANI, Shinji OGIHARA
Formato: article
Lenguaje:EN
Publicado: The Japan Society of Mechanical Engineers 2016
Materias:
carbon fiber reinforced plastics
quasi-isotropic
thin-ply prepreg
orientation angle
tensile loading
low-velocity impact
delamination
damage behavior
Mechanical engineering and machinery
TJ1-1570
Acceso en línea:https://doaj.org/article/f49fc274cc2a45589c0632d93820bfd8
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https://doaj.org/article/f49fc274cc2a45589c0632d93820bfd8

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