摘要
为了研究巡飞器载重能力与火箭弹间的匹配关系,针对折叠式巡飞器普遍采用的串列翼布局,建立了串列翼布局下并列式和重叠式两种机翼折叠装载方案对应的巡飞器任务载重与装载火箭弹空间之间的匹配关系模型,对比分析了两种方案下火箭弹直径随巡飞器任务载重的变化特点,并得出重叠式方案更具载重优势的结论,初步给出了特定条件下两种方案任务载重与火箭弹直径间的对应取值。
In order to study influence of dispension parameters on distribution radius and falling time of submunition striking moving sea-object,point mass ballistic equations is build and then programmed. Analysis of effect of diffent dispension parameters on distribution radius and falling time of submunition is carried out,the results show that the dispension height and velocity of cluster munition are very important parameters,therefore emphasis should be paid on them when designing dispension parameters.
出处
《飞行力学》
CSCD
北大核心
2013年第6期570-573,共4页
Flight Dynamics
关键词
巡飞器
串列翼
火箭弹
匹配关系
loitering monition
tandem wing
cluster munition matching relation
