摘要
The incoming air temperature was within the range of 773-1073K. The incoming flow Mach number ranged from 0.20-0.32. The results showed that, the lean blow-off (LBO) fuel/air ratio of integrated cavity-based strut flameholder (ICBSF) was within the range of 0.0013-0.0027 and had a wide lean blow-off limit because of the cavity structure favorable for evaporation and atomization of fuel. LBO fuel/air ratio of ICBSF increased with the increase of incoming flow Mach number and decreased with the increase of flow temperature, similar to that of conventional bluff-body stabilizers. When the temperature of incoming flow was significantly increased, the influence of the incoming Mach number on fuel/air ratio of ICBSF was weakened; similarly, when the incoming Mach number was significantly increased, the influence of the inflow temperature was also weakened.
| 投稿的翻译标题 | Preliminary experiment on the lean blow-off of an integrated cavity-based strut flameholder |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 75-80 |
| 页数 | 6 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 35 |
| 期 | 1 |
| DOI | |
| 出版状态 | 已出版 - 1 1月 2020 |
关键词
- Afterburner
- Blow-off fuel/air ratio
- Combustion experiment
- Integrated cavity-based strut flameholder
- Lean blow-off
指纹
探究 '一体化凹腔支板稳定器贫油熄火性能初步试验' 的科研主题。它们共同构成独一无二的指纹。引用此
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