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Research on modeling method of honeycomb plate and its application on solar wing
Luo HT(骆海涛)1,2; Fu J(富佳)1,2; Wang, Haonan3; Li, Yuxin3
Department空间自动化技术研究室
Conference Name2019 2nd International Conference on Advanced Electronic Materials, Computers and Materials Engineering, AEMCME 2019
Conference DateApril 19-21, 2019
Conference PlaceChangsha, China
Source Publication2019 International Conference on Advanced Electronic Materials, Computers and Materials Engineering, AEMCME 2019 - Software Engineering and Algorithm
PublisherIOP
Publication PlaceBristol, UK
2019
Pages1-6
Indexed ByEI
EI Accession number20193707413835
WOS IDIOP:1757-8981-563-5-052020
Contribution Rank1
ISSN1757-8981
AbstractAerospace products need to simulate the complicated working conditions through dynamic simulation analysis to ensure the high reliability of product design. In this paper, the equivalent modeling method of honeycomb sandwich plate based on finite element analysis is studied, and the mechanical characteristic parameters of honeycomb core structure are obtained. At the same time, the composite components of satellite solar cell array are modeled and simulated. The modal analysis and frequency response analysis are carried out to provide an important basis for the design and improvement of the structure.
Language英语
Citation statistics
Document Type会议论文
Identifierhttp://ir.sia.cn/handle/173321/25638
Collection空间自动化技术研究室
Corresponding AuthorLuo HT(骆海涛)
Affiliation1.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China
2.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110016, China
3.Institute of Mechanical Engineering and Automation, Northeastern University, Shenyang, Liaoning 110819, China
Recommended Citation
GB/T 7714
Luo HT,Fu J,Wang, Haonan,et al. Research on modeling method of honeycomb plate and its application on solar wing[C]. Bristol, UK:IOP,2019:1-6.
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