Effect of Impact Damage and Open Hole on Typical Mechanical Properties of CYCOM 7701/7781 Fiberglass Epoxy Composite Lamina

Effect of Impact Damage and Open Hole on Typical Mechanical Properties of CYCOM 7701/7781 Fiberglass Epoxy Composite Lamina

CYCOM 7701/7781 fiberglass epoxy fabric prepreg was used to fabricate the composite lamina specimens through medium temperature curing process. The specimens were categorized into three groups. The tensile strength of unnotched and open-hole specimens, the compressive strength of unnotched and open-...

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Bibliographic Details
Main Author: GUAN Qingyu
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2018-10-01
Series:Journal of Aeronautical Materials
Subjects:
composites
fiberglass
7781 fabric
open hole
impact
mechanical property
Online Access:http://jam.biam.ac.cn/CN/Y2018/V38/I5/132

Internet

http://jam.biam.ac.cn/CN/Y2018/V38/I5/132

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