推进技术 ›› 1997, Vol. 18 ›› Issue (2): 44-49.

• • 上一篇    下一篇

真空小喷管羽流场的Monte Carlo直接模拟

蔡国飙,王慧玉,祖国君,张振鹏   

  1. 北京航空航天大学宇航学院!北京;100083;北京航空航天大学宇航学院!北京;100083;北京航空航天大学宇航学院!北京;100083;北京航空航天大学宇航学院!北京;100083
  • 发布日期:2021-08-15
  • 基金资助:
    国家自然科学基金

MONTE CARLO DIRECT SIMULATION OF SMALL NOZZLE PLUME IN VACUUM

  1. School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, 100083;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing, 100083
  • Published:2021-08-15

摘要: 利用直接模拟的MonteCarlo方法数值模拟了真空喷管羽流场,获得了符合规律的数值模拟结果。由于将随机取样频率法(R-S-F)用于轴对称问题中,解决了计算机内存和速度上的困难,同时也证明了R-S-F方法的可靠性。

关键词: 喷管气流;蒙特卡罗法;流动分布;数值模拟

Abstract: Vacuum plume problem is a important research problem puzzling astronautics designers, specially for communication satellites and space station. This paper adopted DSMC methods numerically to simulate vacuum plume of small nozzle, and gained corresponding results. This work is a good begining for further research on vacuum plume contemination, and referential to engineering design.

Key words: Nozzle plume;Monte Carlo method;Flow distribution;Numerical simulation