IMECH-IR  > 高温气体动力学国家重点实验室
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor
Cheng D(程迪); Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军)
Corresponding AuthorWang, Jing(wangjing@imech.ac.cn)
Source PublicationJOURNAL OF AEROSPACE ENGINEERING
2019-09-01
Volume32Issue:5Pages:11
ISSN0893-1321
AbstractWall heat flux distributions under different configurations for a kerosene-fueled supersonic combustor were experimentally studied. The influences of combustion, global fuel equivalence ratio, mass flow rate, total temperature, and inlet Mach number on the wall heat flux of the kerosene-fueled supersonic combustor were systematically presented and analyzed for the first time. Methods to calibrate and validate the in-house-developed heat flux sensors are also presented. The revealed trends would be useful to guide the design of thermal management systems for kerosene-fueled scramjets.
KeywordHeat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor
DOI10.1061/(ASCE)AS.1943-5525.0001076
Indexed BySCI
Language英语
WOS IDWOS:000475509500007
WOS Research AreaEngineering
WOS SubjectEngineering, Aerospace ; Engineering, Civil
Funding ProjectTraining Program of the Major Research Plan of National Natural Science Foundation of China[91641110] ; State Scholarship Fund of China Scholarship Council[201704980059]
Funding OrganizationTraining Program of the Major Research Plan of National Natural Science Foundation of China ; State Scholarship Fund of China Scholarship Council
Classification二类
Ranking1
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/79489
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
Cheng D,Wang J,Lu Y,et al. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor[J]. JOURNAL OF AEROSPACE ENGINEERING,2019,32(5):11.
APA 程迪,王晶,陆阳,李龙,姚卫,&范学军.(2019).Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor.JOURNAL OF AEROSPACE ENGINEERING,32(5),11.
MLA 程迪,et al."Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor".JOURNAL OF AEROSPACE ENGINEERING 32.5(2019):11.
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