| 双模态冲压发动机燃烧室流场数值模拟研究 |
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| 引用本文： | 武渊,田维平,乐发仁,余贞勇.双模态冲压发动机燃烧室流场数值模拟研究[J].固体火箭技术,2003,26(4):41-44. |
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| 作者姓名： | 武渊 田维平 乐发仁 余贞勇 |
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| 作者单位： | 中国航天科技集团公司四院四十一所,西安,710025 |
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| 摘 要： | 在三维、粘性、湍流及有化学反应的Navier-Stokes方程基础上，通过有限化学反应速率／涡扩散模型模化湍流燃烧，对以H2为燃料的双模态冲压发动机燃烧室流场进行了研究，分析了空燃比、燃料入射角、飞行马赫数对燃烧室工作模态的影响，并分析了燃烧室隔离段的作用。
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| 关 键 词： | 双模态冲压发动机 燃烧室 流场 数值模拟 飞行马赫数 超音速燃烧 |
| 文章编号： | 1006-2793(2003)04-0041-04 |
| 修稿时间： | 2002年9月23日 |
Study on numerical simulation of the dual-mode scramjet combustor |
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| WU Yuan,TIAN Wei-ping,YUE Fa-ren,YU Zhen-yong//The st Institute of the Fourth Academy of CASC,Xi'an ,China..Study on numerical simulation of the dual-mode scramjet combustor[J].Journal of Solid Rocket Technology,2003,26(4):41-44. |
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| Authors: | WU Yuan TIAN Wei-ping YUE Fa-ren YU Zhen-yong//The st Institute of the Fourth Academy of CASC Xi'an China |
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| Institution: | WU Yuan,TIAN Wei-ping,YUE Fa-ren,YU Zhen-yong//The 41st Institute of the Fourth Academy of CASC,Xi'an 710025,China. |
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| Abstract: | On the basis of 3-D viscous, turbulent and reactive Navier-Stokes numerical equation, the finite-rate chemistry/eddy-dissipation model for modeling the turbulent combusion is established. The fluid dynamic mechanisms of the dual-mode scramjet combustor using hydrogen as the fuel is studied. The effects of the ratio of the air to fuel, fuel injection angle and flight Mach number on the dual-scramjet working mode are analyzed, and the function of the isolator is analyzed too. |
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| Keywords: | supersonic combustion dual-scramjet~+ flow field simulation Navier-Stokes equation |
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