APPROXIMATION OF OPTIMUM THRUST NOZZLE CONTOUR

被引:0
|
作者
RAO, GVR
机构
来源
ARS JOURNAL | 1960年 / 30卷 / 06期
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:561 / 561
页数:1
相关论文
共 50 条
  • [21] Effect of tabs on the thrust of a convergent nozzle
    Huang, Y., 2001, Beijing University of Aeronautics and Astronautics (BUAA) (27):
  • [22] OPTIMUM DESIGN OF THRUST BEARINGS
    POLLMANN, E
    MASCHINENBAUTECHNIK, 1974, 23 (02): : 79 - 81
  • [23] 3-DIMENSIONAL THRUST NOZZLE DESIGN FOR MAXIMUM AXIAL THRUST
    SNYDER, LE
    THOMPSON, HD
    AIAA JOURNAL, 1971, 9 (10) : 1891 - &
  • [24] Evaluation of fluidic thrust vectoring nozzle via thrust pitching angle and thrust pitching moment
    L. Li
    M. Hirota
    K. Ouchi
    T. Saito
    Shock Waves, 2017, 27 : 53 - 61
  • [25] Evaluation of fluidic thrust vectoring nozzle via thrust pitching angle and thrust pitching moment
    Li, L.
    Hirota, M.
    Ouchi, K.
    Saito, T.
    SHOCK WAVES, 2017, 27 (01) : 53 - 61
  • [26] Exploration and study of fluid thrust vector nozzle
    Xue, Fei
    Wang, Huaqiang
    Wang, Yuchao
    3RD INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND INDUSTRIAL APPLICATIONS, 2019, 1300
  • [27] Effects of vector nozzle deflection on engine thrust
    Ding, Kai-Feng
    Wang, Xiao-Feng
    Fan, Si-Qi
    2000, JPT, Beijing, China (21):
  • [28] An Efficient Approach for Nozzle Rocket Thrust Estimation
    Sribonfha, Pansaporn
    Sirisup, Sirod
    Chusilp, Pawat
    Kulsirikasem, Weerachart
    15TH IEEE INTERNATIONAL CONFERENCE ON COMPUTATIONAL SCIENCE AND ENGINEERING (CSE 2012) / 10TH IEEE/IFIP INTERNATIONAL CONFERENCE ON EMBEDDED AND UBIQUITOUS COMPUTING (EUC 2012), 2012, : 17 - 21
  • [29] Nozzle Optimization of Dual Thrust Rocket Motors
    Alazeezi, Mohammed
    Elek, Predrag
    NEW TECHNOLOGIES, DEVELOPMENT AND APPLICATION II, 2020, 76 : 468 - 477
  • [30] THRUST IMPROVEMENT WITH ABLATIVE INSERT NOZZLE EXTENSION
    CLAYTON, RM
    BACK, LH
    JOURNAL OF PROPULSION AND POWER, 1986, 2 (01) : 91 - 93