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
Link To Document :
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