| 超燃发动机燃烧室流场的数值模拟 |
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| 引用本文： | 梁剑寒,王承尧. 超燃发动机燃烧室流场的数值模拟[J]. 推进技术, 1996, 17(1): 13-17 |
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| 作者姓名： | 梁剑寒 王承尧 |
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| 作者单位： | 国防科技大学航天技术系 |
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| 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。
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| 关 键 词： | 突扩燃烧室，超音速燃烧，流动分布，数值模拟 |
NUMERICAL SIMULATIONS OF CHEMICALLY REACTING FLOWS IN SCRAMJET COMBUSTOR |
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| Liang Jianhan and Wang Chengyao. NUMERICAL SIMULATIONS OF CHEMICALLY REACTING FLOWS IN SCRAMJET COMBUSTOR[J]. Journal of Propulsion Technology, 1996, 17(1): 13-17 |
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| Authors: | Liang Jianhan and Wang Chengyao |
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| Affiliation: | Dept. of Astronautics, National Univ. of Defense Technology, Changsha, 410073;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. |
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| Keywords: | ump combustion chamber Supersonic combustion Flow distribution Numericalsimulation |
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