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喷注方式对双模态冲压发动机燃烧稳定性的影响
引用本文:李大鹏,潘余,梁剑寒,刘卫东,王振国.喷注方式对双模态冲压发动机燃烧稳定性的影响[J].国防科技大学学报,2006,28(3):10-14.
作者姓名:李大鹏  潘余  梁剑寒  刘卫东  王振国
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
基金项目:高比容电子铝箔的研究开发与应用项目
摘    要:在模拟飞行马赫数Ma=4的直连式试验设备基础上,采用固定几何双模态冲压发动机燃烧室构型,使用液体煤油作为燃料,并用火炬式点火器点火,研究不同喷注方式下的火焰稳定性。试验研究表明:在加热器来流总温、总压较低的条件下,火焰稳定较难实现;煤油喷注方式对双模态冲压发动机燃烧室内燃烧稳定性影响很大。

关 键 词:双模态冲压发动机  燃烧室  燃烧稳定性  煤油
文章编号:1001-2486(2006)03-0010-05
收稿时间:2005/11/16 0:00:00
修稿时间:2005年11月16

Influence of Injection Mode on Flame Stability in Dual-mode Scramjet Combustor
LI Dapeng,PAN Yu,LIANG Jianhan,LIU Weidong and WANG Zhenguo.Influence of Injection Mode on Flame Stability in Dual-mode Scramjet Combustor[J].Journal of National University of Defense Technology,2006,28(3):10-14.
Authors:LI Dapeng  PAN Yu  LIANG Jianhan  LIU Weidong and WANG Zhenguo
Institution:College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:On the basis of direct-connect scramjet test system simulating flight Mach number 4,different injection modes were compared to study the influence of flame stability on fixed geometry dual-mode scramjet combustor fueled with liquid kerosene and ignited with torch-model ignition.It is indicated that the flame is difficult to stabilize in the flow condition of lower total pressure and total temperature.It is also indicated that the flame stability in dual-mode scramjet combustor is greatly influenced by the injection mode of kerosene.
Keywords:dual-mode scramjet  combustor  flame stability  kerosene
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