DocumentCode
683978
Title
Finite element simulation for the mechanical property of optics cabin
Author
Tianyi Zhang
Author_Institution
Changchun Inst. of Opt., Changchun, China
fYear
2013
fDate
23-25 March 2013
Firstpage
780
Lastpage
782
Abstract
By using finite element simulation software of Patran and MD. Nastran we simulate the mechanical property of optics cabin of missile. The element analysis includes static mechanical and thermal analysis of cabin wall which can simulate the condition as missile flying, modal analysis and overloading analysis for optics system support which reflect the dynamics capability, we obtain distribution of stress and temperature of cabin and top ten natural frequencies. The result of simulation is important reference for structure estimate and optimal design.
Keywords
finite element analysis; missiles; thermal analysis; MD. Nastran; Patran; cabin wall; finite element simulation software; mechanical property; missile flying; modal analysis; optics cabin; optics system support; overloading analysis; thermal analysis; Finite element analysis; Load modeling; Missiles; Optics; Stress; Temperature distribution; Vibrations;
fLanguage
English
Publisher
ieee
Conference_Titel
Information Science and Technology (ICIST), 2013 International Conference on
Conference_Location
Yangzhou
Print_ISBN
978-1-4673-5137-9
Type
conf
DOI
10.1109/ICIST.2013.6747659
Filename
6747659
Link To Document