引用本文:
【打印本页】   【HTML】 【下载PDF全文】   查看/发表评论  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 1095次   下载 792 本文二维码信息
码上扫一扫!
分享到: 微信 更多
进气掺氢对爆轰波参数影响的试验研究
白桥栋,翁春生
(南京理工大学瞬态物理国家重点实验室,江苏南京210094)
摘要:
为研究氢气对气液两相脉冲爆轰发动机内爆轰参数的影响,对进气掺氢的脉冲爆轰发动机进行了试验研究,实现了发动机的稳定工作。研究发现,进气中掺混氢气对爆轰波参数有较大影响,氢气进气压力为0.1MPa时,掺氢后爆轰波的峰值压力和速度均明显提高,爆轰波速度由1045.9m/s升高至1846.2m/s,发动机尾部位置上爆轰峰值压力从1.9MPa上升至4.5MPa,爆轰波后平台压力提高了0.2~
关键词:  脉冲爆轰发动机  爆轰波  燃烧转爆轰  氢气中图分类号:V238文献标识码:A文章编号:1001-4055(2015)12-1915-06DOI:10.13675/j.cnki.tjjs.2015.12.023
DOI:
分类号:V238
基金项目:国防预研项目。
ExperimentalStudyofEffectsofHydrogenAdditiononDetonationWaveParameters
BAIQiao-dong,WENGChun-sheng
(NationalKeyLaboratoryofTransientPhysics,NanjingUniversityofScienceandTechnology,Nanjing210094,China)
Abstract:
Toinvestigatetheeffectsofhydrogenonthedetonationwaveparameters,theexperimentalstudywasconductedforthegas-liquidpulsedetonationenginewithhydrogenadditionandthestableworkingpro.cessofpulsedetonationenginewasachieved.Theexperimentalresultsshowthatthehydrogenadditionhassignif.icantinfluenceonthedetonationwaveparameters,thedetonationpressureandvelocityincreaseobviouslywithhydrogeninletpressureof0.1MPa,thedetonationwavevelocityincreasesfrom1045.9m/sto1846.2m/s,andthedetonationpeakpressurealsoincreasesfrom1.9MPato4.5MPaattheexitofthePDE.Meanwhile,thedeto.nationplatformpressureincreasesby0.2~0.6MPa.Thedetonationvelocityincreaseswhenthehydrogeninletpressurerisingfrom0.1MPato0.22MPa.Thedistanceofdeflagrationtodetonationtransitioncanbeshortenwithhydrogenaddition.Thedetonationwavecanbefullydevelopedinpulsedetonationenginewithfewerobstacles(5obstades)withhydrogenaddition,thustheDDTdistancecanbereduced,butwhenthenumberofobstaclesislessthanfive,thepulsedetonationenginecannotworkregularly.Theexperimentalresultsarehelpfultoim.provethecomprehensiveperformanceofthePDE.
Key words:  Pulseddetonationengine  Detonationwave  Deflagrationtodetonationtransition  Hydrogen