Numerical simulation of the aerodynamic characteristics of blunt-head missile under large attack angles

被引:0
|
作者
University of Shanghai for Science and Technology, Shanghai 200093, China [1 ]
不详 [2 ]
机构
来源
Kongqi Donglixue Xuebao | 2008年 / 3卷 / 412-418期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [1] AERODYNAMIC CHARACTERISTICS OF A CANARD-CONTROLLED MISSILE AT HIGH ANGLES OF ATTACK
    SMITH, EH
    HEBBAR, SK
    PLATZER, MF
    JOURNAL OF SPACECRAFT AND ROCKETS, 1994, 31 (05) : 766 - 772
  • [2] Numerical simulation on cavitation of submarine launched missile's surface at large angles of attack
    Beijing Institute of Astronautical System Engineering, Beijng 100076, China
    Yuhang Xuebao, 2008, 6 (1701-1705+1772):
  • [3] Numerical simulation of static aerodynamic characteristics of CT-1 model at high angles of attack
    China Aerodynamics Research and Development Center, Mianyang 621000, China
    Hangkong Xuebao, 2008, 4 (859-865):
  • [4] NUMERICAL SIMULATION ON THE AERODYNAMIC FORCE OF THE ICED CONDUCTOR FOR DIFFERENT ANGLES OF ATTACK
    Liu, Y.
    Tang, A. P.
    Liu, K. T.
    Tu, J. W.
    ENGINEERING REVIEW, 2015, 35 (02) : 157 - 169
  • [6] Characteristics of self-excited forces in flutter of typical blunt body under large attack angles
    Liu, Mu-Guang
    Chen, Zheng-Qing
    Liu, M.-G., 2013, Chinese Vibration Engineering Society (32): : 22 - 25
  • [7] NUMERICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF TWO DIFFERENT COMPONENT BODIES AT VARIOUS ANGLES OF ATTACK
    Skibina, N. P.
    Gimaeva, N. R.
    Savkina, N., V
    Maslov, E. A.
    VESTNIK TOMSKOGO GOSUDARSTVENNOGO UNIVERSITETA-MATEMATIKA I MEKHANIKA-TOMSK STATE UNIVERSITY JOURNAL OF MATHEMATICS AND MECHANICS, 2020, (64): : 136 - 145
  • [8] Modeling of unsteady aerodynamic characteristics at high angles of attack
    Hao, Dong
    Zhang, Lin
    Yu, Jing
    Mao, Daiyong
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (06) : 2291 - 2301
  • [9] EXPERIMENTAL MISSILE PITCH-DAMPING AND ROLL-DAMPING CHARACTERISTICS AT LARGE ANGLES OF ATTACK
    USELTON, BL
    JENKE, LM
    JOURNAL OF SPACECRAFT AND ROCKETS, 1977, 14 (04) : 241 - 247
  • [10] Numerical simulation of aerodynamic characteristics of trapezoidal wing configuration at different flap angles
    Wang, Yuntao
    Li, Song
    Meng, Dehong
    Hong, Junwu
    Yang, Xiaochuan
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2015, 36 (06): : 1823 - 1829