• 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