Experimental Study on Delamination of Composite Laminates with 0°/45° Interface under Mode I, Mode II and Mixed-mode I/II Loading

Experimental Study on Delamination of Composite Laminates with 0°/45° Interface under Mode I, Mode II and Mixed-mode I/II Loading

High performance carbon-reinforced composite materials have become important aeronautical materials. During the service time, the delamination fracture of composite structures is a common failure mode. In this study, in order to investigate the delamination behaviours of T800/epoxy composite materia...

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Bibliographic Details
Main Authors: WANG Yana, CHEN Xinwen, GONG Yu
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2018-12-01
Series:Journal of Aeronautical Materials
Subjects:
composites
delamination
fracture toughness
mixture ratio
Online Access:http://jam.biam.ac.cn/CN/Y2018/V38/I6/83

Internet

http://jam.biam.ac.cn/CN/Y2018/V38/I6/83

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