| 串装双燃速药柱发动机的内流场计算 |
| |
| 引用本文： | 赵坚,张振鹏.串装双燃速药柱发动机的内流场计算[J].推进技术,2001,22(4):315-318. |
| |
| 作者姓名： | 赵坚 张振鹏 |
| |
| 作者单位： | 北京航空航天大学宇航学院 |
| |
| 摘 要： | 对一维的加质燃烧室流场、轴对称的二维喷管内流场和高燃速药柱燃烧完成后的燃烧室二维内流场以及三维药柱几何做了一体化计算。应用轴对称的N－S方程、TVD有限体积法的显式MacCormack格式，对燃烧室后段和长尾喷管跨声速流场进行求解，得到了双燃速内弹道性能和轴对称二维流场中燃气参数的分布。结果具有较高的精度，并为进一步的燃烧室和喷管热结构分析提供数值依据。
|
| 关 键 词： | 内弹道计算 内流场计算 串装双燃速药柱发动机 一维加质燃烧室流场 二维喷管内流场 药柱几何计算 燃烧室后段 长尾喷管跨声速流场 |
| 文章编号： | 1001-4055(2001)04-0315-04 |
| 修稿时间： | 2000年10月19 |
Numerical simulation on internal flow field for engine with series dual burning rate grain |
| |
| Zhao Jian and ZhangZhengPeng.Numerical simulation on internal flow field for engine with series dual burning rate grain[J].Journal of Propulsion Technology,2001,22(4):315-318. |
| |
| Authors: | Zhao Jian and ZhangZhengPeng |
| |
| Institution: | School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China |
| |
| Abstract: | An integral computation for unsteady compressible 1 D fluid flows with mass addition and moving boundary in combustion chamber, axi symmetric 2 D fluid flows in combustion chamber nozzle and 3 D grain geometric shape. Explicit TVD finite volume Mac Cormack scheme for time dependent N S equations was used. The results indicate the internal ballistics in series dual burning rate grain motor and the distribution of axi symmetric 2 D flow parameters in the chamber nozzle. |
| |
| Keywords: | Computational fluid dynamics Solid propellant rocket engine Interior ballistic calculation Integrated design |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《推进技术》浏览原始摘要信息 |
| 点击此处可从《推进技术》下载免费的PDF全文 |
