| 分区和有限容积法计算长尾喷管中的湍流流动 |
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| 引用本文： | 淡林鹏,张振鹏,赵永忠,贾永刚.分区和有限容积法计算长尾喷管中的湍流流动[J].推进技术,2003,24(1):33-35. |
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| 作者姓名： | 淡林鹏 张振鹏 赵永忠 贾永刚 |
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| 作者单位： | 1. 北京航空航天大学,宇航学院,北京,100083
2. 内蒙古动力机械研究所,内蒙古,呼和浩特,010010 |
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| 摘 要： | 为了给长尾喷管热防护结构设计提供热边界条件，从轴对称二维雷诺平均N－S方程出发，采用分区算法和有限容积法计算了长尾喷管中的湍流流动，分析了流场的结构特性，提出了长尾喷管中燃气温度，压强和马赫数分布的某些规律以及燃气温度沿壁面的分布，计算和分析结果提出了长尾喷管热防护结构设计应注意的事项。
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| 关 键 词： | 长尾喷管 喷管气流 湍流模型 数值计算 有限体积法 防热结构 |
| 文章编号： | 1001-4055(2003)01-0033-03 |
| 修稿时间： | 2002年5月8日 |
Turbulent flow calculation for a tail-pipe nozzle using multiblock algorithm and finite volume method |
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| DAN Lin peng,ZHANG Zhen peng,ZHAO Yong zhong and JIA Yong gang.Turbulent flow calculation for a tail-pipe nozzle using multiblock algorithm and finite volume method[J].Journal of Propulsion Technology,2003,24(1):33-35. |
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| Authors: | DAN Lin peng ZHANG Zhen peng ZHAO Yong zhong and JIA Yong gang |
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| Institution: | DAN Lin peng 1,ZHANG Zhen peng 1,ZHAO Yong zhong 2,JIA Yong gang 2 |
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| Abstract: | Based on axisymmetric two dimensional N S equation, finite volume method and multiblock algorithm were used to study turbulent flow for a tail pipe nozzle,providing thermal environment for the design of anti thermal construct. The flow field was investigated and some properties of the distribution of temperature, pressure and Mach number of gas in nozzle and temperature of gas along the wall were obtained. From the calculation and analysis,some suggestions were put forward for the design of anti thermal construct. |
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| Keywords: | Tailpipe nozzle Nozzle flow Turbulence model Numerical calculation Finite volume method Heat protection construction |
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