| 摘要: |
| 用显式有限差分法对超燃发动机（Ｓｃｒａｍｊｅｔ）的燃烧室内流场进行了数值模拟。计算中采用了ＭａｃＣｏｒｍａｃｋ两步显格式、Ｂａｌｄｗｉｎ－Ｌｏｍａｘ代数湍流模型以及两方程、四组分的化学反应模型。为了解决源项的刚性问题，运用点隐式方法对它作了隐式处理。 |
| 关键词: 突扩燃烧室 超音速燃烧 流动分布 数值模拟 |
| DOI： |
| 分类号:V231.2 |
| 基金项目: |
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| NUMERICAL SIMULATIONS OF CHEMICALLY REACTING FLOWS IN SCRAMJET COMBUSTOR |
|
Liang Jianhan, Wang Chengyao
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Dept. of Astronautics, National Univ. of Defense Technology, Changsha, 410073
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| Abstract: |
| Numerical simulations of chemically reacting flows in scramjet combustor have beencompleted, MacCortnack’s two step explicit scheme and Baldwin-Lomax algebric turbulence model areused. The chemistry model is a finite rate two equation model, A point-implicit method is used to treatthe source term. |
| Key words: ump combustion chamber Supersonic combustion Flow distribution Numericalsimulation |
