Numerical Study of the Impinging Jets Formed by an Injector with Different Nozzle Diameters

被引:0
|
作者
Kazmierski, Bartosz [1 ]
Kapusta, Lukasz Jan [1 ]
机构
[1] Warsaw University of Technology, Poland
关键词
Disintegration - Jets - Large eddy simulation - Nozzles - Reynolds number - Rockets;
D O I
暂无
中图分类号
学科分类号
摘要
The collision of two or more liquid jets may provide considerable atomisation and efficient mixing of injected substances at the same time. This phenomenon is used, among others, in rocket engines, where the fuel and oxidiser are introduced separately and almost immediately mixed through self-impingement. Depending on the injection and operating conditions, diverse configurations of impinging jets are used, such as doublets, triplets, etc. The appropriately designed injectors and operating conditions ensure the short length of the liquid structures that are developed as a result of the jets' collision, as well as lead to intensive atomisation. The following work presents a numerical analysis of some impinging jets with relatively high Reynolds numbers. Two different nozzle diameters were considered, which were designed for fuels with different calorific values and stoichiometric ratios. The work aims to investigate the influence of the nozzle diameters on the liquid jets' interaction in the same nozzle arrangement (the same impingement angle and distance). The simulations were performed for the same liquid to exclude the influence of the liquid's properties and conclude on the diameter's effect alone. The injection pressure was the same in all of the cases. The calculations were made using large eddy simulation (LES) and volume of fluid (VOF) approaches. The simulation results indicated that the larger diameters enhanced the formation of waves in the liquid sheet that brought about the sheet's disintegration and ligament formations. © The Author(s) 2022.
引用
收藏
页码:1107 / 1119
相关论文
共 50 条
  • [31] Effect of Nozzle Geometry and Distance on Cooling Performance of Impinging Jets
    Kobayashi, Hirokazu
    Kabeya, Kazuhisa
    Takashima, Yukio
    Takahashi, Hideyuki
    Takeda, Gentaro
    ISIJ INTERNATIONAL, 2018, 58 (08) : 1500 - 1509
  • [32] Effect of Nozzle Geometry and Distance on Cooling Performance of Impinging Jets
    Kobayashi, Hirokazu
    Kabeya, Kazuhisa
    Takashima, Yukio
    Takahashi, Hideyuki
    Takeda, Gentaro
    TETSU TO HAGANE-JOURNAL OF THE IRON AND STEEL INSTITUTE OF JAPAN, 2017, 103 (08): : 458 - 467
  • [33] NUMERICAL INVESTIGATION OF PLATE COOLING USING MULTIPLE IMPINGING JETS IN DIFFERENT ALIGNMENTS
    Yildizeli, Alperen
    Cadirci, Sertac
    ISI BILIMI VE TEKNIGI DERGISI-JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2023, 43 (01) : 1 - 9
  • [34] Experimental and numerical investigation of the thermal performance of impinging synthetic jets with different waveforms
    Singh, Pushpanjay K.
    Sahu, Santosh K.
    Upadhyay, Prabhat K.
    Singh, Shashwat
    EXPERIMENTAL HEAT TRANSFER, 2023, 36 (02) : 121 - 142
  • [35] Numerical investigation of heat transfer characteristics of impinging synthetic jets with different waveforms
    Zhang, Yanyao
    Li, Ping
    Xie, Yonghui
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2018, 125 : 1017 - 1027
  • [36] CAVITIES FORMED ON LIQUID SURFACES BY IMPINGING GASEOUS JETS
    CHESLAK, FR
    NICHOLLS, JA
    SICHEL, M
    JOURNAL OF FLUID MECHANICS, 1969, 36 : 55 - &
  • [37] Craters Formed in Granular Beds by Impinging Jets of Gas
    Metzger, Philip T.
    Latta, Robert C., III
    Schuler, Jason A.
    Immer, Christopher D.
    POWDERS AND GRAINS 2009, 2009, 1145 : 767 - +
  • [38] Characteristics of liquid sheets formed by two impinging jets
    Li, Ri
    Ashgriz, Nasser
    PHYSICS OF FLUIDS, 2006, 18 (08)
  • [39] Impinging Performance of High-Pressure Water Jets Emitting from Different Nozzle Orifice Shapes
    Huang, Fei
    Mi, Jianyu
    Li, Dan
    Wang, Rongrong
    GEOFLUIDS, 2020, 2020
  • [40] Numerical study of turbulent five-impinging-jets on a heated plate
    Liu, MS
    Lin, YT
    Chang, CM
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 1998, 15 (01) : 43 - 51