Influence of air swirl orientation on the spray characteristics of a micro-channel-based rotary (MCR) atomizer

被引:4
作者
Kumar, Anjith [1 ]
Sahu, Srikrishna [1 ]
Sundararajan, T. [1 ]
机构
[1] Indian Inst Technol Madras, Dept Mech Engn, Thermodynam & Combust Engn Lab, Chennai 600036, India
关键词
Rotary atomizer; Air swirl; Spiraling jet break-up; Phase Doppler particle analyzer; Sauter mean diameter (SMD); Weber number; Droplet dispersion; LIQUID JET; CROSS-FLOW; ATOMIZATION; COMBUSTION; BREAKUP; PERFORMANCE; SIZE;
D O I
10.1016/j.ast.2023.108449
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this work, we investigate the atomization and spray characteristics of a novel rotary atomizer with micro-channel grooves, using optical diagnostics. Micro-jets emanate from the grooves provided in the rotating injector. The spiraling liquid jets interact with the surrounding high-speed swirling air flow, resulting in the creation of a well-dispersed fine spray. Attention is focused on the effects of air swirler orientation with respect to that of injector rotation. Accordingly, the co-and counter-swirl cases are investigated. The primary jet breakup process is visualized using back-lit illumination technique, which also provides the measurement of jet breakup length. The jet break-up modes are identified for different air swirl strength and orientation and injector rotational speed. The size, number density and velocity components of the spray droplets are measured using PDPA technique at different axial and radial locations. Air velocity is also measured (in the absence of liquid injection) using the LDV technique. In addition, Laser Sheet Imaging (LSI) is employed to investigate the overall spray structure. Results show that the droplet size significantly reduces when air swirl strength or injector rotational speed is increased. Though not much difference is observed in the characteristic droplet size between the co-and counter swirl cases, the droplet size distribution is narrower and droplet dispersion is improved for the latter. The current findings demonstrate the potential of the rotary injector to dynamically control the spray characteristics as per requirement.& COPY; 2023 Elsevier Masson SAS. All rights reserved.
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页数:18
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共 51 条
  • [1] Influence of spinning cup and disk atomizer configurations on droplet size and velocity characteristics
    Ahmed, Mahmoud
    Youssef, M. S.
    [J]. CHEMICAL ENGINEERING SCIENCE, 2014, 107 : 149 - 157
  • [2] Characteristics of Mean Droplet Size Produced by Spinning Disk Atomizers
    Ahmed, Mahmoud
    Youssef, M. S.
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2012, 134 (07):
  • [3] Akinyemi O.S., 2018, EFFECT FUEL PROPERTI
  • [4] Experimental characterization of a pressure swirl spray by analyzing the half cone angle fluctuation
    Amoresano, A.
    Allouis, C.
    Di Santo, M.
    Iodice, P.
    Quaremba, G.
    Niola, V
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2018, 94 : 122 - 133
  • [5] PHASE DOPPLER SPRAY ANALYZER FOR SIMULTANEOUS MEASUREMENTS OF DROP SIZE AND VELOCITY DISTRIBUTIONS
    BACHALO, WD
    HOUSER, MJ
    [J]. OPTICAL ENGINEERING, 1984, 23 (05) : 583 - 590
  • [6] Bhandari D., 2018, ICLASS 2018 14 TRIEN
  • [7] Experimental investigation of spray characteristics of a liquid jet in a turbulent subsonic gaseous crossflow
    Broumand, Mohsen
    Ahmed, Mahmoud M. A.
    Birouk, Madjid
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (03) : 3237 - 3244
  • [8] Liquid film break-up in a model of a prefilming airblast nozzle
    Carvalho, IS
    Heitor, MV
    [J]. EXPERIMENTS IN FLUIDS, 1998, 24 (5-6) : 408 - 415
  • [9] Practical design of ultrasonic spray devices: experimental testing of several atomizer geometries
    Dobre, M
    Bolle, L
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2002, 26 (2-4) : 205 - 211
  • [10] Experimental study on spray characteristics of fan nozzle for integrated afterburner in lateral airflow
    Fei, Li
    Zhao, Bingbing
    He, Liming
    Cheng, Weida
    Yu, Jinlu
    Zeng, Hao
    Yuan, Jiahui
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 130