Experimental study on the spray characteristics of a pintle injector element

被引:12
|
作者
Zhou, Rui [1 ]
Shen, Chibing [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Sci & Technol Scramjet Lab, Changsha 410073, Peoples R China
基金
中国国家自然科学基金;
关键词
Pintle injector element; Liquid-liquid impingement; Spray characteristics; COMBUSTION CHARACTERISTICS; FLUIDIC BAFFLE; PERFORMANCE; IGNITION; WAVE;
D O I
10.1016/j.actaastro.2022.02.019
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A liquid-liquid pintle injector element was used as the test object to analyze its spray characteristics from four aspects: spray morphology, spray dynamic characteristics, spray velocity distribution, and the relation between spray cone angle and momentum ratio. Experimental results indicated that the range of the spray area can be adjusted using the total momentum ratio. When the total momentum ratio changes in the scale of 0.04-0.2, the spray cone angle remains between 45 degrees and 70 degrees, where the semi-open fan-shaped spray area exhibits the most significant dynamic characteristics, the most uniform dynamic energy distribution, the largest high-speed velocity range, and the best atomization. The smaller the block factor, the more sensitive is the spray cone angle to changes in the total momentum ratio. In particular, an expression including the local momentum ratio as an independent variable can be used to accurately predict the spray cone angle in a liquid-liquid pintle injector.
引用
收藏
页码:255 / 262
页数:8
相关论文
共 50 条
  • [1] Experimental study on the spray characteristics of a gas–liquid pintle injector element
    Xuan Jin
    Chibing Shen
    Sen Lin
    Rui Zhou
    [J]. Journal of Visualization, 2022, 25 : 467 - 481
  • [2] Experimental study on the spray characteristics of a gas-liquid pintle injector element
    Jin, Xuan
    Shen, Chibing
    Lin, Sen
    Zhou, Rui
    [J]. JOURNAL OF VISUALIZATION, 2022, 25 (03) : 467 - 481
  • [3] Experimental research on the spray characteristics of pintle injector
    Chen, Huiyuan
    Li, Qinglian
    Cheng, Peng
    [J]. ACTA ASTRONAUTICA, 2019, 162 : 424 - 435
  • [4] Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape
    Nam, Jeongsoo
    Lee, Keonwoong
    Park, Sunjung
    Huh, Hwanil
    Koo, Jaye
    [J]. JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 47 (09) : 658 - 664
  • [5] Flow characteristics of a pintle injector element
    Cheng, Peng
    Li, Qinglian
    Chen, Huiyuan
    [J]. ACTA ASTRONAUTICA, 2019, 154 : 61 - 66
  • [6] Analysis on spray angle model for pintle injector element
    Wang, Kai
    Lei, Fanpei
    Zhang, Botao
    Yang, Anlong
    Zhou, Lixin
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (10):
  • [7] Experimental Research on Effects of Shape of Radial Orifice on Spray Characteristics of Pintle Injector
    Chen, Hui-Yuan
    Li, Qing-Lian
    Cheng, Peng
    Zhang, Bin
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (03):
  • [8] Experimental and numerical investigations on the spray characteristics of liquid-gas pintle injector
    Zhou, Wenyuan
    Xu, Xu
    Yang, Qingchun
    Zhao, Ronghui
    Jin, Yushu
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 121
  • [9] Experimental and numerical investigations on the spray characteristics of liquid-gas pintle injector
    Zhou, Wenyuan
    Xu, Xu
    Yang, Qingchun
    Zhao, Ronghui
    Jin, Yushu
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 121
  • [10] Experimental Research on Spray Field Structure of Liquid-Gas Pintle Injector Element
    Zhang, Bin
    Cheng, Peng
    Chen, Hui-Yuan
    Li, Qing-Lian
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (06):