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Theoretical analysis of effects of boundary layer bleed on scramjet thrust
Yue LJ(岳连捷); Xu XK(徐显坤); Zhang XY(张新宇); Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Source PublicationSCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY
2013-10
Volume56Issue:10Pages:1952-1961
ISSN1674-7348
AbstractThe effects of boundary layer bleed on the scramjet thrust are studied in the present paper. A theoretical model is developed to evaluate the thrust increment and influencing factors. The thrust increment resulting from the bleed is dominated by the rise in total pressure recovery and bleed mass flow rate. The bleed mass flow rate exerts stronger impact on the engine thrust than the total pressure. According to current bleed design, it is a severe challenge for the engine to enhance its total pressure to maintain the original thrust when there is no bleeding. Furthermore, the initial total pressure recovery, fuel mass addition, combustion efficiency and area ratio of engine exit to entrance can affect the contributions of the bleeding to the thrust increment. The scramjet needs a higher rise in total pressure recovery to counteract the negative effect of bleed mass loss at higher initial total pressure recovery or larger area ratio of engine exit/entrance. More heat release results in a little lower demand on the rise in total pressure recovery for maintaining the scramjet thrust. These results will aid in understanding the fundamental mechanism of bleeding on engine thrust.
KeywordScramjet Boundary Layer Bleed Theoretical Analysis Engine Thrust
Subject Area内流
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Indexed BySCI ; EI
Language英语
WOS IDWOS:000324643000020
Funding OrganizationNational Natural Science Foundation of China [90716014, 91216115]
DepartmentLHD高超声速推进技术
Classification二类/Q3
Citation statistics
Cited Times:3[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/47494
Collection高温气体动力学国家重点实验室
Corresponding AuthorYue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Recommended Citation
GB/T 7714
Yue LJ,Xu XK,Zhang XY,et al. Theoretical analysis of effects of boundary layer bleed on scramjet thrust[J]. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY,2013,56(10):1952-1961
APA Yue LJ,Xu XK,Zhang XY,&Yue, LJ .(2013).Theoretical analysis of effects of boundary layer bleed on scramjet thrust.SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY,56(10),1952-1961.
MLA Yue LJ,et al."Theoretical analysis of effects of boundary layer bleed on scramjet thrust".SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY 56.10(2013):1952-1961.
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