首页 | 本学科首页   官方微博 | 高级检索  
     检索      

高温来流下U型脉冲爆震燃烧室燃烧特性试验
引用本文:谭汶昊,郑龙席,卢杰,王凌羿,黄康.高温来流下U型脉冲爆震燃烧室燃烧特性试验[J].航空动力学报,2022,37(3):502-510.
作者姓名:谭汶昊  郑龙席  卢杰  王凌羿  黄康
作者单位:1.西北工业大学 动力与能源学院,西安 710129
基金项目:中央高校基本科研业务费专项资金(G2021KY05114); 中国空气动力研究与发展中心基础和前沿技术研究基金(PJD20170145)
摘    要:为了获得高温来流下气/液两相多循环U型脉冲爆震燃烧室(U-PDC)的燃烧特性,使用汽油/空气为燃料和氧化剂开展了相关试验研究.结果表明:当来流温度为373 K,U-PDC能够在15~38 Hz范围内稳定工作,且随着工作频率提高爆燃向爆震转变(DDT)距离缩短;在室温条件下、工作频率为15~25 Hz时,未能形成充分发展...

关 键 词:脉冲爆震  U型脉冲爆震燃烧室  高温来流  DDT(爆燃向爆震转变)距离  点火起爆时间
收稿时间:2021/4/8 0:00:00

Experiment on combustion characteristics of U-bend pulse detonation combustor under high temperature inlet stream
TAN Wenhao,ZHENG Longxi,LU Jie,WANG Lingyi,HUANG Kang.Experiment on combustion characteristics of U-bend pulse detonation combustor under high temperature inlet stream[J].Journal of Aerospace Power,2022,37(3):502-510.
Authors:TAN Wenhao  ZHENG Longxi  LU Jie  WANG Lingyi  HUANG Kang
Institution:1.School of Power and Energy,Northwestern Polytechnical University,Xi'an 710129,China2.Aerospace Technology Institute,China Aerodynamics Research and Development Center,Mianyang Sichuan 621000,China
Abstract:In order to obtain the combustion characteristics of gas-liquid two-phase multi-cycle U-bend pulse detonation combustor (U-PDC) under high temperature inlet stream,experimental research was carried out by using gasoline and air as fuel and oxidant.The results indicated that the U-PDC can achieve stable operation at the working frequency of 15-38 Hz when the inlet temperature was 373 K,and the deflagration to detonation transition (DDT) distance was shortened when the working frequency increased.When the working frequency was 15-25 Hz,the detonation initiation failed at room temperature.The results showed that high temperature inflow can promote the DDT process.At room temperature and working frequency of 15-25 Hz,due to the uneven distribution of combustible gas in the U-bend detonation tube,the time when the flame was detected outside of the U-bend detonation tube was later than the exit of the U-bend detonation tube.When the inflow temperature increased to 373 K,the phenomenon was obviously improved.In addition,the ignition time of U-PDC was within 3-10 ms,which was greatly affected by ignition delay time.When the working frequency of U-PDC was the same and the inlet stream temperature raised from room temperature to 373 K,the wave velocity increased,and the ignition time decreased. 
Keywords:
本文献已被 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号