航空学报 > 1996, Vol. 17 Issue (1): 83-85

二元矢量喷管内流特性的数值模拟

杨弘炜, 李椿萱   

  1. 北京航空航天大学流体力学研究所, 北京, 100083
  • 收稿日期:1993-12-13 修回日期:1994-09-22 出版日期:1996-02-25 发布日期:1996-02-25

NUMERICAL SIMULATIONS OF INTERNAL FLOW CHARACTERISTICS IN TWO-DIMENSIONAL NOZZLES WITH THRUST VECTORING

Yang Hongwei, Li Chunxuan   

  1. Fluid Mechanics Institute, Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1993-12-13 Revised:1994-09-22 Online:1996-02-25 Published:1996-02-25

摘要: 应用多重网格MacCormack显示格式对不同矢量角下二元喷管的流动进行了模拟分析。计算时,在细网络上采用了雷诺平均N-S方程和K-ε湍流模型方程;在粗网格上则采用Euler方程。数值计算给出了较清晰的流谱。壁面压力分布的计算值也与实验结果吻合。通过计算结果分析了喷管几何参数对流场的影响。所得结果显示出多重网格算法高效可靠,可用于开展参数研究

关键词: 喷管设计, 二维流, 喷管推力系数, 多网格法.纳维-斯托克斯方程

Abstract: Numerical simulations of internal flows with thrust vectoring in two-dimensional convergent-divergent nozzles utilizing multigrid technique in conjunction with MacCormack's explicit scheme are presented in this paper. The computations employ the Reynolds averaged Navier-Stokes equations for the fine grids with K-ε turbulence model,and on the coarse grids, on the other hand, Euler equations are solved. Numerical results provide good resolution to the flow fields, and the computed pressure distributions are found in good agreement with the experimental data. The influences of geometric parameters upon the flow quality and thrust coefficient are also analyzed. The results demonstrate that the multigrid technique adopted here is reliable and suitable for parametric study.

Key words: nozzle design, two dimensional flow, nozzle thrust coefficients, multigrid method, Navier-Stokes equations

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