Comparison of various thin-walled composite beam models for thermally induced vibrations of spacecraft boom-Reference-Cited by-同舟云学术

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Comparison of various thin-walled composite beam models for thermally induced vibrations of spacecraft boom

Published:2023-09 Issue: Volume:320 Page:117163
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Shen Zhenxing^ORCID,Hao Shengwang,Li Huijian

Funder

National Natural Science Foundation of China

Natural Science Foundation of Hebei Province

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference65 articles.

1. A review on developments of deployable membrane-based reflector antennas;Chandra;Adv Space Res,2021

2. Overview of key technologies and on-orbit verification of China space station;Zhang;Aerosp China,2022

3. Review on thermal and mechanical challenges in the development of deployable space optics;Villalba;J Astron Telesc Inst,2020

4. Mechanics of laminated composite plates and shells: Theory and analysis;Reddy,2003

5. Thermal-structural analysis of large space structures: An assessment of recent advances;Thornton;J Spacecr Rockets,1985

Cited by 1 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. Thin-walled composite beam elements via the absolute nodal coordinate formulation;Multibody System Dynamics;2023-12-12

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