The methodology for scramjet combustor performance analysis and evaluation is build up.
提出了超燃冲压发动机燃烧室的性能分析评价方法。
The model of combustion fraction for dense phase in circulating fluidized bed combustor has been built up, based on thermal balance, gas analysis and total gas amount.
建立了基于热平衡法、烟气分析法和烟气量法的循环流化床锅炉燃烧室密相区燃烧份额计算数学模型，并分析比较了各种模型的特点。
Numerical analysis results indicate, the out press of combustor decreases with increasing the value;
数值分析结果表明，燃烧器出口压力随着轴向值增大而逐渐减小；
A quasi one dimensional unsteady numerical analysis of supersonic combustor performance has been conducted.
完成了超音速燃烧室内非定常准一维流的数值模拟研究。
Numerical analysis of the kerosene spray supersonic combustion was carried out in the dual-mode supersonic combustor with the CFD software.
利用计算流体力学软件对煤油在所设计的双模态超声速燃烧室内的超声速喷雾燃烧进行了数值模拟。
Numerical analysis of the kerosene spray supersonic combustion was carried out in the dual-mode supersonic combustor with the CFD software.
利用计算流体力学软件对煤油在所设计的双模态超声速燃烧室内的超声速喷雾燃烧进行了数值模拟。
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