Study on the failure mechanism of <scp>1060‐H112</scp> aluminum alloy‐carbon/glass fiber laminate-Reference-Cited by-同舟云学术

Study on the failure mechanism of 1060‐H112 aluminum alloy‐carbon/glass fiber laminate

Published:2022-11-05 Issue:2 Volume:44 Page:850-862
ISSN:0272-8397
Container-title:Polymer Composites
language:en
Short-container-title:Polymer Composites

Author:

Deng Yunfei¹,Wang Ruiwen²^ORCID,Liang Xupeng²,Peng Jie²,Wei Gang²

Affiliation:

1. Key Laboratory of Civil Aviation Aircraft Airworthiness Certification Technology Civil Aviation University of China Tianjin People's Republic of China

2. College of Aeronautical Engineering Civil Aviation University of China Tianjin People's Republic of China

Publisher

Wiley

Subject

Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.27136

Reference32 articles.

1. Progressive failure analysis of perforated aluminium/CFRP fibre metal laminates using a combined elastoplastic damage model and including delamination effects

2. Low velocity impact response of fibre-metal laminates – A review

3. Applications of fiber-metal laminates

4. Designing for damage tolerance in aerospace: A hybrid material technology

5. Delamination and fatigue crack growth behavior in Fiber Metal Laminates (Glare) under single overloads

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