Structural Static/Fatigue/Damage Tolerance Comprehensive Design Optimization of Composite Laminate-Reference-Cited by-同舟云学术

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Structural Static/Fatigue/Damage Tolerance Comprehensive Design Optimization of Composite Laminate

Published:2022-02 Issue:2 Volume:60 Page:998-1012
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ren Qiang¹,Wang Xiaojun²,Shi Shanglu³,Ma Yujia⁴,Wang Jing¹,Ding Xuyun²

Affiliation:

1. Beijing Electro-Mechanical Engineering Institute, 100074 Beijing, People’s Republic of China

2. Beihang University, 100083 Beijing, People’s Republic of China

3. Chengdu Aircraft Design & Research Institute, 610091 Chengdu, People’s Republic of China

4. China Academy of Space Technology–DFH Satellite Company Limited, 100081 Beijing, People’s Republic of China

Funder

Defense Industrial Technology Development Program

National Nature Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060020

Reference37 articles.

1. Effect of high temperature on bond strength of near-surface mounted FRP reinforcement

2. Hygrothermal effects of epoxy resin. Part II: variations of glass transition temperature

3. Swelling and glass transition relations for epoxy matrix material in humid environments

4. Temperature dependence of mechanical and thermal expansion properties of T300/5208 graphite/epoxy

5. YangN.LiangW., Essentials of Proof of Composite Aircraft Structures, Aviation Industry Press, Beijing, 2015, p. 112 (in Chinese).

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Enhancing composite laminate structures with tailored neural networks;MRS Communications;2024-03-07

2. Analysis of thermal stresses in FGM-Matrix medium induced by constant heat flux at the far field;Mechanics of Advanced Materials and Structures;2021-12-15

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