IMECH-IR  > 高温气体动力学国家重点实验室
Experimental investigation on the cavity-based scramjet model
Gu HB(顾洪斌); Chen LH(陈立红); Zhang XY(张新宇); Gu HB(顾洪斌)
Source PublicationCHINESE SCIENCE BULLETIN
2009
Volume54Issue:16Pages:2794-2799
ISSN1001-6538
AbstractThe present work focused on improving the engine performance with different fuel equivalence ratios and fuel injections. A scramjet model with strut/cavity integrated configurations was tested under Mach 5.8 flows. The results showed that the strut may sreve as an effective tool in a kerosene-fueled scramjet. The integration of strut/cavities also had great effect on stablizing the combustion in a wide range of fuel equivalence ratio. The one-sdimensional analysis method was used to analyze the main characteristics of the model. The two-stage fuel injection should have better performance in increasing the chemical reaction rate in the first cavity region.
KeywordScramjet Combustor Cavity Performance
Subject Area弹性力学与塑性力学
DOI10.1007/s11434-009-0460-4
Indexed BySCI
Language英语
WOS IDWOS:000269212800010
WOS KeywordSUPERSONIC COMBUSTORS; FUEL-INJECTION; FLAME STABILIZATION; PERFORMANCE; FLOW; MECHANISM
WOS SubjectScience & Technology - Other Topics
Citation statistics
Cited Times:15[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/26508
Collection高温气体动力学国家重点实验室
Corresponding AuthorGu HB(顾洪斌)
Recommended Citation
GB/T 7714
Gu HB,Chen LH,Zhang XY,et al. Experimental investigation on the cavity-based scramjet model[J]. CHINESE SCIENCE BULLETIN,2009,54,16,:2794-2799.
APA Gu HB,Chen LH,Zhang XY,&顾洪斌.(2009).Experimental investigation on the cavity-based scramjet model.CHINESE SCIENCE BULLETIN,54(16),2794-2799.
MLA Gu HB,et al."Experimental investigation on the cavity-based scramjet model".CHINESE SCIENCE BULLETIN 54.16(2009):2794-2799.
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