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舰载导弹烤燃数值模拟研究
引用本文:齐强,毕世华,段金锋,贺卫东.舰载导弹烤燃数值模拟研究[J].舰船科学技术,2006,28(5):55-58.
作者姓名:齐强  毕世华  段金锋  贺卫东
作者单位:北京理工大学,机电工程学院,北京,100081;中国船舶重工集团公司第七一三研究所,河南,郑州,400450;航天科工集团8359研究所,北京,100039
摘    要:介绍了舰载导弹发射舱相邻舱室起火时火源对舱内导弹的烤燃研究方法,分析了影响烤燃过程的各种因素,建立了一般烤燃传热数学模型,模拟计算了某型导弹烤燃时间—温度的变化过程。提出了改进发射舱内热安全性设计的具体建议,具有工程应用价值。

关 键 词:发射舱  烤燃  热安全  数值模拟
文章编号:1672-7649(2006)05-0055-04
收稿时间:2005-05-11
修稿时间:2005-05-11

Cook-off numerical simulation of shipboard missiles
QI Qiang,BI Shi-hua,DUAN Jin-feng,HE Wei-dong.Cook-off numerical simulation of shipboard missiles[J].Ship Science and Technology,2006,28(5):55-58.
Authors:QI Qiang  BI Shi-hua  DUAN Jin-feng  HE Wei-dong
Institution:1. School of Electromechanical Engineering, Beijing Institute of Technology, Beijing 100081, China; 2. The 713 Research Institute of CSIC, Zhengzhou 400015, China; 3. The 8359 Research Institute of CSSIC, Beijing 100039,China
Abstract:When there was a conflagration in a cabin adjacent to the missile launch compartment,missiles which are in the compartment might be cooked-off.Where,the cook-up process of missiles is analyzed and,the heat transfer model is established,the cook-off time-temperature process is simulated.Finally,some constructive advices are given out to improve launch compartment's thermal safety on practical engineering design.
Keywords:launch compartment  cook-off  thermal safety  numerical simulation
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