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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)
Source PublicationActa Mechanica Sinica
2011
Volume27Issue:2Pages:152-163
ISSN0567-7718
AbstractThe 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.
KeywordThrust Measurement Impulse Method Aerodynamic Features Cold Jet Arc-heated Jet
DOI10.1007/s10409-011-0431-2
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Indexed BySCI ; EI
Language英语
WOS IDWOS:000292036300002
DepartmentLHD应用等离子体力学(CPCR)
Classification二类
Citation statistics
Cited Times:9[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/44577
Collection等离子体与燃烧中心(2009-2011)
Corresponding AuthorWu CK(吴承康)
Recommended Citation
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.
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