Performance of the fuel injector in supersonic combustor
文献类型：会议论文
| 作者 | Wei Z(卫喆) ; Chen LH(陈立红); Gu HB(顾洪斌); Li F(李飞); Gu SL(顾声龙); Chang XY(张新宇)
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| 出版日期 | 2009 |
| 会议名称 | 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference |
| 会议日期 | October 19, 2009 - October 22, 2009 |
| 会议地点 | Bremen, Germany |
| 关键词 | Concentration profiles Engine design Fuel injectors Fuel-air mixing Gas sampling Ramp injector Scramjet combustors Scramjet test Supersonic combustors |
| 通讯作者 | Wei, Z. (weizhejiji@yahoo.com.cn) |
| 中文摘要 | Enhancing the fuel-air mixing is critical for scramjet combustor performance. The performance of four different aerodynamic ramp injectors was reported in this paper. The experiments were conducted in a direct-connected scramjet test facility. The concentration profiles were obtained by gas sampling and chromatogram analysis. The pictures of the flow field were obtained by using laser scatter. It would be used to analyze the flow field generated by the aerodynamic ramp, then optimize the layout of the injectors. The results would offer some useful information for engine design. Copyright © 2009 by the American Institute of Aeronautics and Astronautics, Inc. |
| 收录类别 | EI |
| 会议录 | 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
 |
| 语种 | 英语 |
| ISBN号 | 9781600867408 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60456]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 推荐引用方式 GB/T 7714 | Wei Z,Chen LH,Gu HB,et al. Performance of the fuel injector in supersonic combustor[C]. 见:16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen, Germany. October 19, 2009 - October 22, 2009. |
入库方式： OAI收割
来源：力学研究所
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