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: | , , |
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| Formato: | article |
| Lenguaje: | EN |
| Publicado: |
The Japan Society of Mechanical Engineers
2016
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| Acceso en línea: | https://doaj.org/article/f49fc274cc2a45589c0632d93820bfd8 |
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