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喷管内横流流场的数值模拟
引用本文:徐旭,张振鹏.喷管内横流流场的数值模拟[J].固体火箭技术,1997,20(4):12-17.
作者姓名:徐旭  张振鹏
作者单位:北京航空航天大学宇航学院!北京,100083
摘    要:采用显式的原始MacCormack时间分裂格式和改进的TVD MacCormack格式分别求解了二维轴对称喷管内横流流场的N-S方,得到了与理论分析结果相近似的流场结果图谱,并对以上两方法得到的结果进行了比较,结果表明:TVD的方法具有更高的精度。文中还介绍了一种基于TTM方法的改进的网格生成方法,用于生成贴壁性和正交性都比较好的网格,实现了完全由边界网点分布来确定内部网格点的分布。

关 键 词:火箭发动机  喷管  横流  数值模拟  TVD

Numerical Simulation of Cross-Flow in Rocket Motor Nozzle
Xu Xu, ZhangZhenpeng.Numerical Simulation of Cross-Flow in Rocket Motor Nozzle[J].Journal of Solid Rocket Technology,1997,20(4):12-17.
Authors:Xu Xu  ZhangZhenpeng
Abstract:A time-split MacCormack scheme and a TVD MacCormack scheme are used to solve the twodimensional axisymetric N-S equations of Cross-flow in rocket motor nozzle. Both the methods give fine results and the TVD scheme is proved to be of more higher accuracy. A kind of grid generation method based on the TTM method is also introduced to generate body-fitted calculating mesh, the distribution of inner grids can be totally controled by the distribution of grids on boundaries.
Keywords:Rocket moter nozzle  Cross flow  Numerical simulation
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