• 校内登录

个人信息 更多+
  • 教师姓名: 黄佐华
  • 教师英文名称: Zuohua Huang
  • 性别: 男
  • 职称: 教授
  • 职务: 教授
  • 博士生导师: 是
  • 硕士生导师: 是
  • 学历: 博士研究生毕业
  • 学位: 博士
  • 所在单位: 能源与动力工程学院 绿色氢电全国重点实验室
  • 电子邮箱:
  • 办公地点: 西安交通大学兴庆校区北二楼四层
  • 联系方式:

论文成果

当前位置: 中文主页 - 科学研究 - 论文成果

The auto-ignition boundary of ethylene/nitrous oxides as a promising monopropellant (PDF)

发布时间:2025-04-30
点击次数:
发布时间:
2025-04-30
论文名称:
The auto-ignition boundary of ethylene/nitrous oxides as a promising monopropellant (PDF)
发表刊物:
Combust Flame
摘要:
C2H4/N2O has recently been proposed as a promising monopropellant for hydrazine replacement. In this work, the auto-ignition capability of argon diluted C2H4/N2O was experimentally investigated first in a rapid compression machine by detecting the light emission and the pressure evolution profiles. The auto-ignition boundary temperature which separates the non-ignition and successful ignition cases were then determined and modeled as a function of pressure and mixture composition. Results show that the auto-ignition temperature decreases with the increase of pressure and increases with the argon dilution fraction and fuel oxidizer ratio. In addition, for successful auto-ignition cases, the ignition delay times were measured and used to validate several recently developed kinetic mechanisms. A mechanism was developed and showed good agreement with the measured ignition delay time as well as the auto-ignition boundary temperature at all test conditions. Finally, the auto-ignition boundary temperatures at practical rocket engine conditions (without dilution) were numerically predicted at various pressure and fuel oxidizer ratio conditions. The model is of merit for designing the cooling system and the local flow residence time to reduce the risk of fuel line explosion and the resonance acoustic induced combustion instability in practical rocket engine.
合写作者:
Yang M, Yang Y, Liao CY, Tang CL, Zhou CW, Huang ZH
卷号:
2020, 221, 64-73
页面范围:
64-73
是否译文:
否
发表时间:
2020-11-15