Analyses of supersonic combustion by gas sampling
文献类型：会议论文
| 作者 | Chen LH(陈立红) ; Lin R; Gu HB(顾洪斌); Chang XY(张新宇)
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| 出版日期 | 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 |
| 关键词 | Combustion efficiency Gas sampling Probe sampling Scramjet |
| 中文摘要 | 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. |
| 收录类别 | EI |
| 会议录 | A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
 |
| 语种 | 英语 |
| ISBN号 | 1563477297 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60275]  |
| 专题 | 力学研究所_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]. 见:13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference. Capua, Italy. May 16, 2005 - May 20, 2005. |
入库方式： OAI收割
来源：力学研究所
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