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 :
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