Aerodynamics of indirect thrust measurement by the impulse method

doi:10.1007/s10409-011-0431-2

IMECH-IR > 等离子体与燃烧中心(2009-2011)

	Aerodynamics of indirect thrust measurement by the impulse method
	Wu CK(吴承康); Wang HX(王海兴); Meng X(孟显); Chen X(陈熙); Pan WX(潘文霞); Wu CK(吴承康)
发表期刊	Acta Mechanica Sinica
	2011
卷号	27 期号:2 页码:152-163
ISSN	0567-7718
摘要	The aerodynamic aspects of indirect thrust measurement by the impulse method have been studied both experimentally and numerically. The underlying basic aerodynamic principle is outlined, the phenomena in subsonic, supersonic and arc-heated jets are explored, and factors affecting the accuracy of the method are studied and discussed. Results show that the impulse method is reliable for indirect thrust measurement if certain basic requirements are met, and a simple guideline for its proper application is given.
关键词	Thrust Measurement Impulse Method Aerodynamic Features Cold Jet Arc-heated Jet
DOI	10.1007/s10409-011-0431-2
URL	查看原文
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000292036300002
课题组名称	LHD应用等离子体力学(CPCR)
论文分区	二类
引用统计	被引频次：12[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/44577
专题	等离子体与燃烧中心(2009-2011)
通讯作者	Wu CK(吴承康)
推荐引用方式 GB/T 7714	Wu CK,Wang HX,Meng X,et al. Aerodynamics of indirect thrust measurement by the impulse method[J]. Acta Mechanica Sinica,2011,27,2,:152-163.
APA	Wu CK,Wang HX,Meng X,Chen X,Pan WX,&吴承康.(2011).Aerodynamics of indirect thrust measurement by the impulse method.Acta Mechanica Sinica,27(2),152-163.
MLA	Wu CK,et al."Aerodynamics of indirect thrust measurement by the impulse method".Acta Mechanica Sinica 27.2(2011):152-163.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
Q-1.pdf（4130KB）	期刊论文	出版稿	开放获取	CC BY-NC-SA	浏览下载