Effects of vector nozzle deflection on engine thrust

被引：0
|
作者：
Ding, Kaifeng [1 ]
Wang, Xiaofeng [1 ]
Fan, Siqi [1 ]
机构：
[1] Chinese Flight Test Establishment, Xi'an, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2000年 / 21卷 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
6
引用
收藏
页码：23 / 25
相关论文
共 50 条
  • [21] Multi-nozzle thrust matching control of STOVL engine
    Pang, Shuwei
    Fu, Xueting
    Li, Qiuhong
    Zhou, Wenxiang
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2024,
  • [22] Flow and thrust characteristics of an expansion-deflection dual-bell nozzle
    Wang, Yong
    Lin, Yuzhen
    Eri, Qitai
    Kong, Bo
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 123
  • [23] COMPUTER EXPERIMENTS ON ION BEAM DEFLECTION FOR THRUST VECTOR CONTROL
    HAMZA, V
    JOURNAL OF SPACECRAFT AND ROCKETS, 1966, 3 (08) : 1304 - &
  • [24] Experimental Investigation of Nozzle Effects on Thrust and Inlet Pressure of an Air-breathing Pulse Detonation Engine
    CHEN Wenjuan
    Chinese Journal of Aeronautics , 2012, (03) : 381 - 387
  • [25] Experimental Investigation of Nozzle Effects on Thrust and Inlet Pressure of an Air-breathing Pulse Detonation Engine
    Chen Wenjuan
    Fan Wei
    Zhang Qun
    Peng Changxin
    Yuan Cheng
    Yan Chuanjun
    CHINESE JOURNAL OF AERONAUTICS, 2012, 25 (03) : 381 - 387
  • [26] Experimental Investigation of Nozzle Effects on Thrust and Inlet Pressure of an Air-breathing Pulse Detonation Engine
    CHEN Wenjuan FAN Wei ZHANG Qun PENG Changxin YUAN Cheng YAN Chuanjun School of Power and Energy Northwestern Polytechnical University Xian China
    Chinese Journal of Aeronautics, 2012, 25 (03) : 381 - 387
  • [27] FORMATION OF VORTEX STRUCTURES IN THE PRENOZZLE SPACE OF AN ENGINE WITH A VECTORABLE THRUST NOZZLE
    Volkov, K. N.
    Emel'yanov, V. N.
    Denisikhin, S. V.
    JOURNAL OF ENGINEERING PHYSICS AND THERMOPHYSICS, 2016, 89 (03) : 660 - 670
  • [28] Characteristics of flow and thrust variations in a jet engine with a variable area nozzle
    Park, Junho
    Sohn, Chae Hoon
    JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2015, 29 (11) : 5001 - 5010
  • [29] Numerical simulation of nozzle internal flowfield and thrust for attitude control engine
    Natl Univ of Defence Technology, Changsha, China
    Tuijin Jishu, 6 (50-53):
  • [30] Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle
    V. A. Levin
    N. E. Afonina
    V. G. Gromov
    G. D. Smekhov
    A. N. Khmelevskii
    V. V. Markov
    Combustion, Explosion, and Shock Waves, 2012, 48 : 406 - 417
12345