空军工程大学学报（自然科学版）2013，Vol.14Issue(2)：32-36,5.DOI:10.3969/j.issn.1009-3516.2013.02.008
燃气射流对多联装导弹发射箱前盖影响
Research on Jet Flow Effecting Former Lid of the Missile Launch Box
摘要
Abstract
Aiming at the problems that the former lid of the missile was easy to be broken by high temperature and high velocity jet flow, by computing sinkage of the whole body and head part of missile, depending on method of computational fluid dynamic, the surface pressure and temperature is analyzed on different missile pose and leave distance. The result of simulation shows the parameter of the former friable lid exits great difference, the conclusion is important to design launch box in the engineering application.关键词
燃气射流/发射箱前盖/计算流体力学Key words
jet flow/ former lid of the missile/ computational fluid dynamic分类
航空航天引用本文复制引用
刘少伟,关娇,王伟,冯刚..燃气射流对多联装导弹发射箱前盖影响[J].空军工程大学学报（自然科学版）,2013,14(2):32-36,5.
