摘要
A system-level modularization numerical model which can deal with the coupling effect of combustion and flow was established for combustion device, with air and kerosene as reactants, of a turbine test rig and its outlet section, and a thermodynamic calculation scheme based on mixture fraction and a mixture fraction equation were put forward. Comparison with simulation results of the model based on mass-flow-rate mixture ratio and experimental results indicates that the mixture fraction-based model can solve the problem of transient simulation stability in the previous research, and reach the accuracy of simulation consistent with experimental results.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 981-986 |
| 页数 | 6 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 33 |
| 期 | 6 |
| 出版状态 | 已出版 - 12月 2012 |
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