| 摘要: |
| 本文扼要地介绍了航空航天部三十一所1988年11月利用电弧加热器所进行的M=2的超音速气流中横向喷射氢燃料和煤油的点火情况,描述了点火现象的物理特性,并提出了点火准则中的修正系数. |
| 关键词: 超音速流 氢燃料 点火 超音速燃烧 |
| DOI： |
| 分类号: |
| 基金项目: |
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| EXPERIMENTAL RESEARCH ON AUTOIGNITION OF FUEL INJECTED TRANSVERSELY INTO SUPERSONIC AIRSTREAM |
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The 31st Research Institute
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| Abstract: |
| Ignition test of hydrogen and kerosene fuels injected transversely into Mach 2 supersonic airstream heated in a electric arc wind-tennel, carried out by 31st Research Institute, MAS(Nov.1988)is introduced in brief .Physical characteristics of ignition are described and a modified coefficient for ignition criterion is also proposed in this paper. |
| Key words: Supersonic combustion Supersonic flow Ignition Hydrogen fuel |
