Sidejet aerodynamic interaction effects of the missile

被引：5
|
作者：
Kikumoto, K
Sentoh, E
Tanaka, H
Takahashi, T
机构：
[1] Japan Defense Agcy, Tokyo 1908533, Japan
[2] IHI Aerosp Co Ltd, Gunma 3703298, Japan
[3] Kawasaki Heavy Ind Co Ltd, Gifu 5048710, Japan
来源：
AIAA JOURNAL | 2001年 / 39卷 / 04期
关键词：
D O I：
10.2514/2.1383
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The side thruster is a highly responsive means for attitude control of missiles. The sidejet force is influenced by the interaction of the sidejet with the external airflow. The sidejet aerodynamic interaction effects were analyzed from following two viewpoints: 1) the pressure field in the vicinity of the sidejet and 2) the Force acting on the missile. Technical data of sidejet aerodynamic interaction effects were obtained by means of Right tests of missiles that were equipped with four impulse side thrusters that were small-size, rapidly burning solid-propellant rocket motors. The data agree with computational fluid dynamics analyses and wind-tunnel tests.
引用
收藏
页码：611 / 617
页数：7
相关论文
共 50 条
  • [41] Numerical Simulation of Aerodynamic Interaction Effects in Coaxial Compound Helicopters
    Wang, Maosheng
    Wang, Yanyang
    Cao, Yihua
    Zhang, Qiang
    FDMP-FLUID DYNAMICS & MATERIALS PROCESSING, 2023, 19 (05): : 1301 - 1315
  • [42] EFFECTS OF GAS-SURFACE INTERACTION MODELS ON AERODYNAMIC CHARACTERISTICS
    KUZUU, K
    KUBOTA, H
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1991, 34 (105) : 109 - 120
  • [43] Interaction of missile propulsion and aerodynamics
    Buchanan, C.R., 1600, Royal Aeronautical Soc, London, United Kingdom (104):
  • [44] Methods for distributing semiempirical, nonlinear, aerodynamic loads on missile components
    Moore, FG
    McInville, RM
    Housh, C
    JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (06) : 744 - 752
  • [45] Interaction of missile propulsion and aerodynamics
    Buchanan, CR
    Gemmill, AJT
    Martin, PG
    AERONAUTICAL JOURNAL, 2000, 104 (1036): : 271 - 277
  • [46] COMPARISON OF MISSILE FLIGHT-TEST DRAG WITH AERODYNAMIC PREDICTIONS
    EASTMAN, DW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1993, 30 (06) : 682 - 688
  • [47] AERODYNAMIC FORCES ON NONCIRCULAR CROSS-SECTION MISSILE FOREBODIES
    EST, BE
    NELSON, HF
    JOURNAL OF AIRCRAFT, 1992, 29 (04): : 612 - 618
  • [48] Aerodynamic performances of cruise missile flying above local terrain
    Ahmad, A.
    Saad, M. R.
    Idris, A. Che
    Rahman, M. R. A.
    Sujipto, S.
    AEROTECH VI - INNOVATION IN AEROSPACE ENGINEERING AND TECHNOLOGY, 2016, 152
  • [49] Aerodynamic Modeling of a Missile Combining Transfer Learning and Dendritic Net
    Ni, Zijian
    Chen, Shiwei
    Zhu, Zejun
    Wang, Wei
    JOURNAL OF AIRCRAFT, 2024, 61 (05): : 1535 - 1549
  • [50] EVALUATION OF MISSILE AERODYNAMIC CHARACTERISTICS USING RAPID PREDICTION TECHNIQUES
    SUN, J
    CUMMINGS, RM
    JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (06) : 513 - 520
12345