Analyses of supersonic combustion by gas sampling

IMECH-IR > 力学所知识产出(1956-2008)

	Analyses of supersonic combustion by gas sampling
	Chen LH(陈立红); Lin R; Gu HB(顾洪斌); Chang XY(张新宇)
会议录名称	A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
	2005
会议名称	13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
会议日期	May 16, 2005 - May 20, 2005
会议地点	Capua, Italy
摘要	The probe sampling-gas chromatography system has been designed and tested in the direct-connected supersonic combustion facility and the free-jet hypersonic propulsion facility to detect the exhaust components of the scramjet model. The representative distributions were summarized under such conditions: almost completely burned, incompletely burned and without burning. The gas components including H2, O2, N2, CO, CO 2, CH4 and C2H4 can be identified To analyze the component distributions with the corresponding static pressure on the wall, the more detailed information can be achieved. The result can be used for the improvement of combustion. Copyright © 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
关键词	Combustion Efficiency Gas Sampling Probe Sampling Scramjet
ISBN号	1563477297
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/60275
专题	力学所知识产出(1956-2008)
推荐引用方式 GB/T 7714	Chen LH,Lin R,Gu HB,et al. Analyses of supersonic combustion by gas sampling[C]A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference,2005.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
CaEi036.pdf（93KB）	会议论文		开放获取	CC BY-NC-SA	浏览下载