Numerical Model Solution and Analysis of Effect Factors of Boron Ignition and Combustion Behaviors

被引:0
|
作者
Ao W. [1 ]
Quan E. [2 ]
机构
[1] Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi'an
[2] Xi'an Aerospace Propulsion Institute, Xi'an
来源
| 2017年 / Journal of Propulsion Technology卷 / 38期
关键词
Boron; Combustion; Ignition; Kinetic model; Solid propellant;
D O I
10.13675/j.cnki.tjjs.2017.05.028
中图分类号
学科分类号
摘要
The ignition and combustion kinetic model for single boron particles in oxygenated environment containing O2 and H2O was developed. The specific numerical solution method was introduced. Prediction of the models was in good agreement with experimental data. The effects of particle size, initial oxide thickness, ambient pressure, partial pressure of oxygen, partial pressure of water vapor, and ambient temperature on boron ignition and combustion were investigated by numerical calculation. The results were compared with experiment as well. The results show both the ignition and combustion time increase with increasing particle size. The combustion time is found to be in direct proportion to particle size, but this dependency changes to quadratic when the particle size exceeds 20μm. The ignition time increases significantly as the initial oxide layer increases with a growth rate of 65ms/μm. Increased ambient pressure reduces both the ignition and combustion time, whereas the sensitivity is very weak at pressure higher than 3MPa. The ignition time is independent of oxygen partial pressure but decreases with increased water vapor partial pressure. On the contrary, the combustion time is independent of water vapor partial pressure but decreases with increased oxygen partial pressure. Similar effects on the ignition and combustion time as function of ambient temperature are obtained. © 2017, Editorial Department of Journal of Propulsion Technology. All right reserved.
引用
收藏
页码:1180 / 1187
页数:7
相关论文
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