IMECH-IR  > 力学所知识产出(1956-2008)
On supersonic combustion
Yuan SX(袁生学); Yuan, SX (reprint author), Chinese Acad Sci, Inst Mech, Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Source PublicationScience in China Series A-Mathematics Physics Astronomy
1999
Volume42Issue:2Pages:171-179
ISSN1006-9283
AbstractSome basic concepts and features of supersonic combustion are explained from the view point of macroscopic aerodynamics. Two kinds of interpretations of supersonic combustion are proposed. The difference between supersonic combustion and subsonic combustion is discussed, and the mechanism of supersonic combustion propagation and the limitation of heat addition in supersonic flow are pointed out. The results of the calculation of deflagration in supersonic flow show that the entropy increment and the total pressure loss of the combustion products may decrease with the increase of combustion velocity. It is also demonstrated that the oblique detonation wave angle may not be controlled by the wedge angle under weak underdriven solution conditions and be determined only by combustion velocity. Therefore, the weak underdriven solution may become self-sustaining oblique detonation waves with a constant wave angle.
Subject Area力学
DOI10.1007/BF02876569
Indexed BySCI
Language英语
WOS IDWOS:000078523600007
WOS Research AreaMathematics
WOS SubjectMathematics, Applied ; Mathematics
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/15622
Collection力学所知识产出(1956-2008)
Corresponding AuthorYuan, SX (reprint author), Chinese Acad Sci, Inst Mech, Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Recommended Citation
GB/T 7714
Yuan SX,Yuan, SX . On supersonic combustion[J]. Science in China Series A-Mathematics Physics Astronomy,1999,42,2,:171-179.
APA 袁生学,&Yuan, SX .(1999).On supersonic combustion.Science in China Series A-Mathematics Physics Astronomy,42(2),171-179.
MLA 袁生学,et al."On supersonic combustion".Science in China Series A-Mathematics Physics Astronomy 42.2(1999):171-179.
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