Advanced Search
Volume 38 Issue 3
Mar.  2012
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (3): 309-313,318.
Zhang Jianhua, Xie Kan. Secondary flow thrust vector control study for fluidic throat nozzle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 309-313,318. (in Chinese)
Citation: Zhang Jianhua, Xie Kan. Secondary flow thrust vector control study for fluidic throat nozzle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (3): 309-313,318. (in Chinese)
shu

Secondary flow thrust vector control study for fluidic throat nozzle

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 May 2011
  • Publish Date: 30 Mar 2012
    Abstract
  • The secondary flow vector control concept for the fluidic throat nozzle of solid rocket motor was studied. Through numerical simulation, the work condition of concurrent thrust modulation and vector control was analyzed, in which there exist secondary flow at the throat and expansion part meanwhile. The throat modulation and thrust vector control performance of nine typical secondary flow concepts were compared, and the influence on the secondary flow vector control was discussed for the existence of secondary flow at the throat. The results of concept comparison can provide references for practical design.

     

    • FullText(HTML)
  • loading
    • References(9)
  • [1]
    李娟,李江,王毅林,等.喉栓式变推力发动机性能研究[J].固体火箭技术,2007,30(6):505-509
    Li Juan,Li Jiang,Wang Yilin,et al.Study on performance of pintle controlled thrust solid rocket motor[J].Tech of Solid Rocket Motors,2007,30(6):505-509(in Chinese)
    [2]
    谢侃,刘宇,王一白.固体火箭发动机气动喉部的两相流数值模拟[J].推进技术,2010,31(1):56-60
    Xie Kan,Liu Yu,Wang Yibai.Simulation for the two-phase flow aerodynamic throat of solid rocket motors[J].Journal of Propulsion Power,2010,31(1):56-60(in Chinese)
    [3]
    McArdle J G.Internal characteristics and performance of an aerodynamically controlled,variable discharge convergent Nozzle[R].NACA TN4312,1958
    [4]
    McAulay J E.Cold-air investigation of three variable-throat-area convergent-divergent Nozzles[R]. NASA TMX-42,1958
    [5]
    Catt J A,Miller D N,Giuliano V J.A static investigation of fixed-geometry nozzle using fluidic injection for throat-area control[R].AIAA 95-2604
    [6]
    谢侃,王一白,刘宇.固体火箭发动机气动喉部非定常过程[J].推进技术,2011,32(1):103-108
    Xie Kan,Wang Yibai,Liu Yu.Unsteady process of aerodynamic throat for solid rocket motor[J].Journal of Propulsion Power,2011,32(1):103-108(in Chinese)
    [7]
    谢侃.随控流体喉部的数值和实验研究[D].北京:北京航空航天大学宇航学院,2010
    Xie Kan.Numerical and experimental study for the fluidic nozzle throat[D].Beijing:School of Astronautics,Beijing University of Aeronautics and Astronautics,2010(in Chinese)
    [8]
    王峥,胡永强.固体火箭发动机[M].北京:宇航出版社,1993
    Wang Zheng,Hu Yongqiang.Solid rocket motors[M].Beijing:Astronautics Press,1993(in Chinese)
    [9]
    Waithe K A,Deere K A.Experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring[R].AIAA 2003-3802,2003
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2439) PDF downloads(707) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return