中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Aerodynamics of indirect thrust measurement by the impulse method

文献类型:期刊论文

作者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)
刊名Acta Mechanica Sinica
出版日期2011
卷号27期号:2页码:152-163
通讯作者邮箱ckw@imech.ac.cn
关键词Thrust measurement Impulse method Aerodynamic features Cold jet Arc-heated jet
ISSN号0567-7718
通讯作者吴承康
合作状况其它
中文摘要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.
分类号二类
收录类别SCI ; EI
原文出处http://dx.doi.org/10.1007/s10409-011-0431-2
语种英语
WOS记录号WOS:000292036300002
公开日期2012-01-06
源URL[http://dspace.imech.ac.cn/handle/311007/44577]  
专题力学研究所_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.

入库方式: OAI收割

来源:力学研究所

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