| 摘要: |
| 通过求解N－S方程，数值计算了扩张圆管内的非平衡流动，并研究了超声速混合和燃烧的强化技术。结果表明，在超声速领域，预旋燃料方式是一种比较有效的强化技术。 |
| 关键词: 超音速冲压喷气发动机 燃烧效率 强化混合+ 数值分析 |
| DOI： |
| 分类号:V235.2 |
| 基金项目:国家自然科学基金 |
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| THE STUDIES OF THE ENHANCEMENTTECHNIQUES OF MIXING ANDCOMBUSTION IN SUPERSONIC FLOWS |
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Chen Jianqiang,Zhang Hanxin,Gao Shuchun
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China Aerodynamics Research and Development Center,Mianyang, 621000
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| Abstract: |
| The viscous nonequilibrium swirling flows in a divergent duct are simulated by solvingN-S equations, and the enhancement techniques of mixing and combustion in supersonic flows areinvestigated. The results show that the swirling of fuel is an effective enhancement method forsupersonic mixing and combustion. |
| Key words: Supersonic combustion ramjet engine Combustion efficiency Enhancement mixing~+ Numerical analysis |
