火箭增程乘波外形导弹弹道特性研究

IMECH-IR > 力学所知识产出(1956-2008)

	火箭增程乘波外形导弹弹道特性研究
Alternative Title	Trajectory Characteristics of Hypersonic Waverider Missile with Rocket Extended Range
	郭迪龙; 张杰; 康宏琳; 王发民
Source Publication	弹道学报
	2006-12-30
Volume	18 Issue:4 Pages:1-3
ISSN	1004-499X
Abstract	基于椭圆锥相交流场，采用非轴对称设计方法生成了一种带火箭增程的乘波外形高超声速导弹，并在给定攻角条件下对乘波外形导弹的弹道进行了仿真。仿真结果表明：导弹的飞行轨迹为波浪形；在满足热防护的条件下，给定乘波外形和初始滑翔速度的导弹存在一个较优的初始滑翔高度；导弹自带增程火箭的点火时间越早，其飞行距离越远。
Keyword	火箭增程乘波外形高超声速导弹升阻比弹道仿真
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:2635593
Citation statistics	Cited Times:2[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/40582
Collection	力学所知识产出(1956-2008)
Corresponding Author	郭迪龙
Recommended Citation GB/T 7714	郭迪龙,张杰,康宏琳,等. 火箭增程乘波外形导弹弹道特性研究[J]. 弹道学报,2006,18,4,:1-3.
APA	郭迪龙,张杰,康宏琳,&王发民.(2006).火箭增程乘波外形导弹弹道特性研究.弹道学报,18(4),1-3.
MLA	郭迪龙,et al."火箭增程乘波外形导弹弹道特性研究".弹道学报 18.4(2006):1-3.

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