• DocumentCode
    2860902
  • Title

    Simulation of Resistant Shock Capability of Missile Launcher Based on DDAM

  • Author

    Jiang Tao ; You Wen-li ; Zhou Fang-yi ; Wang Wei-li

  • Author_Institution
    Naval Aeronaut. & Astronaut. Univ., Yantai, China
  • fYear
    2009
  • fDate
    11-13 Dec. 2009
  • Firstpage
    1
  • Lastpage
    3
  • Abstract
    Simulation is the important method for shock-resistant ability design of shipboard equipment. And shipboard equipment shock-resistant ability is the one of important factor of ship life ability. Four-missile launcher resistant shock ability has been evaluated by American navy dynamic design analysis method (DDAM). The four-missile launcher has maximal value of displacement at Z direction, and has maximal value of mises stress at X direction because Four-missile launcher has less stiffness at Z direction and has bigger stiffness at X direction. In order to decrease the value of mises stress at X direction, could decrease stiffness of X direction suitably.
  • Keywords
    digital simulation; finite element analysis; military computing; missiles; ships; Ansys program; dynamic design analysis method; finite element method; missile launcher; resistant shock capability simulation; shipboard equipment; shock-resistant ability design; Aerodynamics; Aluminum alloys; Design methodology; Electric shock; Fatigue; Marine equipment; Marine vehicles; Missiles; Stress; Underwater vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computational Intelligence and Software Engineering, 2009. CiSE 2009. International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-4507-3
  • Electronic_ISBN
    978-1-4244-4507-3
  • Type

    conf

  • DOI
    10.1109/CISE.2009.5366036
  • Filename
    5366036