Experimental study on the spray characteristics of a pintle injector element

被引:20
|
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
  • [31] Experimental Study on Spray Characteristics of Voice Coil Motor Injector
    Wu H.
    Zhang Z.
    Zhang F.
    Gao H.
    Neiranji Xuebao/Transactions of CSICE (Chinese Society for Internal Combustion Engines), 2022, 40 (02): : 162 - 170
  • [32] Flow visualization of cryogenic spray from a movable pintle injector
    Keonwoong Lee
    Dongsoo Shin
    Min Son
    Heejang Moon
    Jaye Koo
    Journal of Visualization, 2019, 22 : 773 - 781
  • [33] Spray characteristics of a pintle injector based on annular orifice area (vol 167, 201, 2020)
    Lee, Suji
    Kim, Daehwan
    Koo, Jaye
    Yoon, Youngbin
    ACTA ASTRONAUTICA, 2020, 173 : 473 - 474
  • [34] Flow visualization of cryogenic spray from a movable pintle injector
    Lee, Keonwoong
    Shin, Dongsoo
    Son, Min
    Moon, Heejang
    Koo, Jaye
    JOURNAL OF VISUALIZATION, 2019, 22 (04) : 773 - 781
  • [35] Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine
    Son, Min
    Yu, Kijeong
    Radhakrishnan, Kanmaniraja
    Shin, Bongchul
    Koo, Jaye
    JOURNAL OF THERMAL SCIENCE, 2016, 25 (01) : 90 - 96
  • [36] Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine
    Min Son
    Kijeong Yu
    Kanmaniraja Radhakrishnan
    Bongchul Shin
    Jaye Koo
    JournalofThermalScience, 2016, 25 (01) : 90 - 96
  • [37] Verification on spray simulation of a pintle injector for liquid rocket engine
    Min Son
    Kijeong Yu
    Kanmaniraja Radhakrishnan
    Bongchul Shin
    Jaye Koo
    Journal of Thermal Science, 2016, 25 : 90 - 96
  • [38] Spray characteristics of a multi-slit type throttleable pintle injector with different slit heights
    Heo, Subeom
    Jeong, Juhwan
    Yoon, Youngbin
    ACTA ASTRONAUTICA, 2024, 215 : 475 - 492
  • [39] Effect of Local Momentum Ratio on Spray Windward Distribution of a Gas-Liquid Pintle Injector Element
    Jin, Xuan
    Yang, Yang
    Cao, Xiaomei
    Wu, Jinshui
    AEROSPACE, 2022, 9 (09)
  • [40] Experimental Investigation on a Throttleable Pintle-Centrifugal Injector
    Li, Tianwen
    Yu, Nanjia
    Zhao, Zeng
    Zhao, Yaming
    APPLIED SCIENCES-BASEL, 2025, 15 (05):