Residual stress variation and deformation of shot peened glass fiber reinforced composites/aluminum–lithium laminates under thermal shock and thermal fatigue-Reference-Cited by-同舟云学术

Residual stress variation and deformation of shot peened glass fiber reinforced composites/aluminum–lithium laminates under thermal shock and thermal fatigue

Published:2021-09-20 Issue:12 Volume:42 Page:6523-6533
ISSN:0272-8397
Container-title:Polymer Composites
language:en
Short-container-title:Polymer Composites

Author:

Xiang Junxian¹^ORCID,Li Huaguan¹²,Wang Hao¹,Li Hongli¹,Chen Xi¹,Tao Jie¹

Affiliation:

1. College of Materials Science and Technology Nanjing University of Aeronautics and Astronautics Nanjing China

2. Jiangsu Key Laboratory of Advanced Structural Materials and Application Technology Nanjing Institute of Technology Nanjing China

Funder

Qinglan Project of Jiangsu Province of China

National Natural Science Foundation of China

Natural Science Foundation of Jiangsu Province

Publisher

Wiley

Subject

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

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.26318

Reference27 articles.

1. Lay-up optimisation of fibre metal laminates based on fatigue crack propagation and residual strength

2. A review: Fibre metal laminates, background, bonding types and applied test methods

3. Recent developments in advanced aircraft aluminium alloys

4. Reinforcement effects of aluminum–lithium alloy on the mechanical properties of novel fiber metal laminate

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