本文给出一种模型燃气轮机燃烧室中三维气相反应流流场的数值计算结果。
This paper describes the numerical calculations of gaseous reacting flows in a model of gas turbine combustors.
采用数值模拟方法对燃用天然气的某型航改燃气轮机环形燃烧室进行三维流场分析。
The three-dimensional flow field of annular combustor for aero-derivative gas turbine burning gas fuel was numerically simulated.
本文通过中压全尺寸燃气轮机燃烧室空气加湿燃烧实验，研究了加湿度对燃烧特性的影响。
In this paper, an air humidified combustion experiment was carried out using mid-pressure full-dimension gas turbine combustor to determine the effects of humidity on combustion characteristics.
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