建立湍流燃烧的“双流体”数学模型，用于一维湍流预混稳态火焰的描述。
The two-fluid mathematical model of turbulent combustion is built, which to depict steady state one -dimensional turbulent premixed flame.
数值仿真模型中考虑了自燃推进剂雾化机理、高压分解燃烧和预混反应流湍流燃烧等。
The atomization mechanism of hypergolic rocket propellant and decomposition combustion at high pressure and turbulence burning of premixed reactant flow field are considered .
应用概率密度函数非预混模型，对固体火箭冲压发动机补燃室内的湍流燃烧进行了数值模拟。
The numerical simulation of turbulent combustion in the afterburner of solid rocket ramjet was performed by applying the probability density function non -premixed mode.
最后对各种不同组分模拟合成气在三种多旋流模型燃烧室中进行预混燃烧实验研究。
At last this paper introduced the premixed combustion research performed in three multi-swirling models with different constituents of premixed gas.
最后对各种不同组分模拟合成气在三种多旋流模型燃烧室中进行预混燃烧实验研究。
At last this paper introduced the premixed combustion research performed in three multi-swirling models with different constituents of premixed gas.
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