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)
Source PublicationA Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
2005
Conference Name13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
Conference DateMay 16, 2005 - May 20, 2005
Conference PlaceCapua, Italy
AbstractThe 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.
KeywordCombustion Efficiency Gas Sampling Probe Sampling Scramjet
ISBN1563477297
Indexed ByEI
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/60275
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
Chen LH,Lin R,Gu HB,et al. Analyses of supersonic combustion by gas sampling[C],2005.
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