Combustor相关论文
The effects of pressure oscillation on aerodynamic characteristics in an aero-engine com-bustor are investigated. A comb......
Experimental Investigations of the Flow Field Structure and Interactions between Sectors of a Double
Effect of venturi angle and main stage swirl intensity on flow field and interactions were investigated using PIV.The re......
Experimental Investigations of the Flow Field Structure and Interactions between Sectors of a Double
In this paper,the flow field characteristics of a double-swirl low-emission combustor were analyzed by using Particle Im......
The experimental studies and numerical simulation were conducted on the effects of the dome fuel distribution ratio on t......
为降低生物质直接燃烧过程污染物排放，提高燃烧效率，在给料量为12kg／h的低NOx生物质粉体燃烧器中进行燃烧实验，探究燃烧温度、过量空气......
为探究吕家坨井田地质构造格局,根据钻孔勘探资料,采用分形理论和趋势面分析方法,研究了井田7......
介绍三维进气道和超声速燃烧冲压式喷气发动机(SCRAMJET)模型一项实验研究的结果.Scramjet模型由进气道和燃烧室组成,此模型组件的......
Pressure drop and cut size measurements are reported for a full scale cyclone operating within a 58 MWth CFB-combustor u......
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Turbulent combustion remains to be one of most complicated technologies due to the complexities of turbulence and combus......
对设计的基于贫油预混蒸发(LPP)的多点喷射低污染燃烧室头部方案,对其性能进行了数值研究.头部为中心分级燃烧,设计为同心圆式主、......
根据微燃机燃烧室国内外实际技术水平及技术基础,对烟气循环富氧燃烧微燃机燃烧室进行了设计,并对所设计燃烧室进行模拟计算,根据......
针对实际飞行中主燃烧室稳定性评估,提出了工程化的燃烧室负荷参数,建立了基于来流参数的发动机主燃烧室稳定性表征方法;通过Gastu......
开发一款燃烧天然气的中小型地面燃气轮机燃烧室,并对该燃烧室采用单筒燃烧室压力模化试验进行燃烧特性分析。结果表明:在设计工况......
为研究SMC模式下火箭混合比对RBCC发动机性能的影响规律,完成了氢/氧火箭推力室中心布局、二元定几何结构模型发动机飞行马赫数Ma0......
