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Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities a
  • ISSN号：0894-1777
  • 期刊名称：Experimental Thermal and Fluid Science
  • 时间：2012.11
  • 页码：90-96
  • 相关项目：超声速气流中缓燃与爆震的传播、相互转化机理及其应用研究
作者： Sun, Ming Bo|Gong, Cheng|Zhang, Shun Ping|Liang, Jian Han|Liu, Wei Dong|Wang, Zhen Guo|
同期刊论文项目
超声速气流中缓燃与爆震的传播、相互转化机理及其应用研究
期刊论文 31 会议论文 6
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Adaptive mesh refinement based numerical simulation of detonation initiation in supersonic combustib
支板喷射超声速湍流燃烧的大涡模拟
Parametric study of detonation initiation using a hot jet in supersonic combustible mixtures
Detonation initiation and propagation in nonuniform supersonic combustible mixtures
静止可燃气热射流爆震起爆块结构自适应网格加密数值模拟
Deflagration-to-Detonation Transition Induced by Hot Jets in a Supersonic Premixed Airstream
Flow patterns and mixing characteristics of gaseous fuel multiple injections in a non-reacting super
A modified blending function for zonal hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation
A hybrid LES (Large Eddy Simulation)/assumed sub-grid PDF (Probability Density Function) model for s
超声速预混气扩张流道热射流起爆研究
超燃发动机燃烧室三维化学反应流场的数值模拟
超声速预混气的热射流起爆过程数值模拟
A dynamic pressure-sink method for improving large eddy simulation and hybrid Reynolds-averaged Navi
Effects of a hot jet for detonation initiation and propagation in supersonic combustible mixtures
Influence analysis of geometrical parameters of detonation initiation with a hot jet by adaptive mes
基于自适应网格加密的超声速可燃气热射流起爆详细反应数值模拟
Numerical study on self-sustained oscillation characteristics of cavity flameholders in a supersonic
超声速燃烧室氢气强迫点火过程实验
来流边界层效应下斜坡诱导的斜爆轰波
并联凹腔火焰稳定器超声速燃烧特性实验研究
气化煤油与乙烯超声速燃烧特性对比
超声速湍流燃烧G/Z方程模型验证
基于超声速气流中凹腔主动喷注的强迫点火方案研究
基于高速摄影图像处理统计分析的点火过程试验
Experimental investigations of detonation initiation by hot jets in supersonic premixed flows