Numerical simulation on the plume flow structures for a missile

被引：0
|
作者：
Xu, Chun-Guang [1 ]
Liu, Jun [1 ]
机构：
[1] Inst. of Aerosp. and Mat. Eng., Natl. Univ. of Defence Technol., Changsha 410073, China
来源：
| 2003年 / Journal of Propulsion Technology卷 / 24期
关键词：
Combustion - Navier Stokes equations - Thermal plumes - Wakes;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A detailed numerical investigation of a kind of missile's plume fields was simulated using an existing three dimensional TLA N-S computational technique based on ENO difference scheme for Mach number Ma=0.8-1.6, altitude H=2 km-15 km, combustor total pressure pc=20 MPa and 40 MPa. The result shows altitude and combustor total pressure markedly influence plume fields width. A formula was obtained by analyzing flows structures and measurement. The result can be used as the foundation to evaluate the edge of plume flows.
引用
收藏
相关论文
共 50 条
  • [1] Numerical simulation of the infrared characteristic of missile exhaust plume
    Ruan, Li-Ming
    Qi, Hong
    Wang, Sheng-Gang
    Yang, Chang-Peng
    Infrared and Laser Engineering, 2008, 37 (06) : 959 - 962
  • [2] Modeling and simulation of missile plume flow field characteristics
    1600, Chinese Society of Astronautics (43):
  • [3] RCS simulation of plasma plume of missile
    Liu, Bo
    Shi, Jia-Ming
    Jin, Lin
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2007, 29 (01): : 41 - 44
  • [4] The RCS simulation of plasma plume of missile
    Liu, Bo
    Shi, Jiaming
    Jin, Lin
    Zhou, Wenyu
    PROCEEDINGS OF 2006 CIE INTERNATIONAL CONFERENCE ON RADAR, VOLS 1 AND 2, 2006, : 1768 - +
  • [5] Numerical analysis of detailed flow structures of a bubble plume
    Murai, Y
    Matsumoto, Y
    JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 1998, 41 (03) : 568 - 574
  • [6] Numerical simulation on particle distribution of the plume flow in vacuum
    Li, Zhong-Hua
    Li, Zhi-Hui
    Wu, Jun-Lin
    Peng, Ao-Ping
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2014, 37 (06): : 797 - 803
  • [7] Numerical simulation of flow field for thermal separation of multistage missile
    Li, Jiang
    Xiao, Yumin
    Sun, Dechuan
    Cai, Timin
    Shiyou Daxue Xuebao/Journal of the University of Petroleum China, 1998, 22 (05): : 62 - 65
  • [8] Numerical simulation of flow field for canard-controlled missile
    School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
    Xitong Fangzhen Xuebao, 2008, 14 (3656-3658):
  • [9] Numerical simulation of flow field for thermal separation of multistage missile
    Li, Jiang
    Xiao, Yumin
    Sun, Dechuan
    Cai, Timin
    Tuijin Jishu/Journal of Propulsion Technology, 1998, 19 (04): : 62 - 65
  • [10] Numerical simulation of missile separation
    Yang, Ming-Zhi
    Gui, Ye-Wei
    Liu, Gang
    Jiang, Xiong
    Xiao, Han-Shan
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2006, 24 (02): : 261 - 264
12345