乘波飞行器构型方法研究

IMECH-IR > 力学所知识产出(1956-2008)

	乘波飞行器构型方法研究
Alternative Title	RESEARCH ON WAVERIDER CONFIGURATION METHOD
	王发民; 李立伟; 姚文秀; 雷麦芳
Source Publication	力学学报
	2004
Volume	36 Issue:5 Pages:513-519
ISSN	0459-1879
Abstract	高超声速飞行中,随着马赫数的升高,波阻和摩阻增加,就会形成升阻比"屏障",而乘波飞行器构型是克服这一升阻比屏障的有效方法.本文提出了一种变楔角楔/椭圆锥乘波体构型方法,并基于前体/进气道一体化设计思想,生成了高超声速乘波飞行器构型.经数值计算与实验验证,与传统锥形流场生成的乘波体相比,该方法生成的乘波体不仅具有高升阻比,而且能为发动机提供所需的高温高压均匀来流.
Keyword	乘波飞行器变楔角楔/椭圆锥乘波体气动力升阻比
Subject Area	力学
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:1689925
Citation statistics	Cited Times:17[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/15723
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	王发民,李立伟,姚文秀,等. 乘波飞行器构型方法研究[J]. 力学学报,2004,36,5,:513-519.
APA	王发民,李立伟,姚文秀,&雷麦芳.(2004).乘波飞行器构型方法研究.力学学报,36(5),513-519.
MLA	王发民,et al."乘波飞行器构型方法研究".力学学报 36.5(2004):513-519.

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