脉冲爆震发动机点火过程离子催化效应数值模拟  

Numerical simulation for ion catalytic effect in ignition process of pulse detonation engine

作　　者：母云涛[1] 王玉清[2] 李立翰[2] 郑殿峰[1] 张会强[3] 

机构地区：[1]北京大学工学院,北京100871 [2]中国航天科工集团公司北京动力机械研究所,北京100074 [3]清华大学航天航空学院,北京100084

出　　处：《航空动力学报》2015年第3期694-700,共7页Journal of Aerospace Power

基　　金：国家自然科学基金(51176001;50676049)

摘　　要：利用气体电离理论推导出氢气-空气混合气体电离后组成成分,理论分析活性基团对燃烧速率及剧烈程度的催化效应,以及不同点火能量、活性基团浓度对缓燃转爆震（DDT）过程的影响.结合氢气-空气燃烧23步化学反应动力学机制,采用FLUENT软件对不同工况下的DDT过程进行模拟,与理论分析结果对比.结果表明：点火温度为2000～2500K时,活性基团的加入,可提高燃烧速率,DDT时间可缩短9.91％～21.08％,DDT距离可缩短3.32％～8.08％,DDT时间和DDT距离的改变幅度随点火温度的升高而增大.点火能量较高时应该考虑气体电离效应.The gas composition was devived using the theory of gas ionization after hy- drogen-air mixed gas ionization. The catalysis effect of active group on combustion rate and intensity was found out with the theoretical analysis, and the influences on deflagration to detonation transition （DDT） process in different ignition energies and different concentra- tions of active group were analyzed. Fully considering the hydrogen-air combustion reaction 23-step kinetics mechanism, the the numerical simulation method was used to study DDT process in different cases by FLUENT, and the theoretical analysis was verified. Results show that when the ignition temperature is in the range of 2000--2500K, the reactive group in the process of ignition can increase the combustion rate; DDT time can be shortened by 9.91 %--21.08%, and DDT distance can be shortened by 3.32%-8.08%. With increase of the ignition temperature, DDT time and DDT distance increase. Gas ionization effect should be considered if ignition energy is high.

关 键 词：脉冲爆震发动机 点火 气体电离 活性基团 催化效应 

分 类 号：V43[航空宇航科学与技术—航空宇航推进理论与工程]