摘要
The oxidation characteristics of RP-3 kerosene/O2 were experimentally tested in the flow reactor under the conditions of the equivalence ratios of 0.5,1.0 and 2.0,the temperature range of 550− 1 200 K,the pressure of 0.1,3.0 MPa. The results showed that,with the increase of equivalent ratio from 0.5 to 2.0,the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species increased. With the increase of pressure from 0.1 MPa to 3.0 MPa,the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species decreased,and the peak mole fraction of alkanes increased while that of alkenes decreased. Meanwhile,the ignition delay characteristics of RP-3 kerosene/O2 were experimentally tested in the shock tube under the conditions of the equivalent ratios of 0.8,and 3.5,the pressure of 0.2,1.0,and 5.0 MPa,the temperature range of 950− 1 500 K. The results showed that, with the increase of the pressure and temperature or the decrease of equivalent ratio from 3.5 to 0.8,the ignition delay time of RP-3 kerosene/O2 was shortened.
| 投稿的翻译标题 | Experiment on the oxidation and ignition delay characteristics of RP-3 kerosene/oxygen |
|---|---|
| 源语言 | 繁体中文 |
| 文章编号 | 20220381 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 39 |
| 期 | 5 |
| DOI | |
| 出版状态 | 已出版 - 5月 2024 |
关键词
- RP-3 kerosene
- flow reactor
- ignition delay time
- oxidation characteristics
- shock tube
学术指纹
探究 'RP-3 航空煤油/O2 的氧化与着火特性试验' 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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