锥形流乘波体优化设计研究

IMECH-IR > 力学所知识产出(1956-2008)

	锥形流乘波体优化设计研究
Alternative Title	Viscous Optimized Design of Waverider Derived from Cone Flow
	耿永兵; 刘宏; 姚文秀; 王发民
Source Publication	航空学报
	2006
Volume	27 Issue:1 Pages:23-28
ISSN	1000-6893
Abstract	随着马赫数的升高,波阻和摩阻增加,形成升阻比“屏障”,而乘波构型飞行器是克服这一屏障的有效途径.本文在Ma∞=4.0～20.0、高度H=24.0～52.0 km、圆锥角Ac=5°～10°的条件下,以升阻比为目标函数,进行了乘波体的优化设计,讨论了对乘波体优化外形的影响因素,并给出全马赫数范围的优化乘波体外形及其气动力结果.
Keyword	乘波体优化设计空气动力学升阻比
Subject Area	力学
Indexed By	EI ; CSCD
Language	中文
CSCD ID	CSCD:2347784
Citation statistics	Cited Times:10[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/16540
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	耿永兵,刘宏,姚文秀,等. 锥形流乘波体优化设计研究[J]. 航空学报,2006,27,1,:23-28.
APA	耿永兵,刘宏,姚文秀,&王发民.(2006).锥形流乘波体优化设计研究.航空学报,27(1),23-28.
MLA	耿永兵,et al."锥形流乘波体优化设计研究".航空学报 27.1(2006):23-28.

Related Services

Bookmark

Lanfanshu

Similar articles in Bing Scholar

Terms of Use

No data!

Social Bookmark/Share

File name:	144821.pdf
Format:	Adobe PDF

This file does not support browsing at this time

All comments (0)

No comment.

The comment function is only available to registered usersLog In

If you have any objections to this item, please fill out the form below and the administrator will contact you as soon as possible.
Content:
Email：	*
Institution:
Verification Code:	Refresh

Any comments and suggestions are welcomed.
Title:	*
Content:
Email：	*
Verification Code:	Refresh

中国科学院力学研究所机构知识库