• DocumentCode
    1888139
  • Title

    Numerical Simulation on Flow Field of Laval-style Atomizer by Fluent

  • Author

    Si Chaorun ; Zhang Xianjie ; Wang Junbiao

  • Author_Institution
    Shannxi Eng. Res. Center for Digital Manuf. Technol., Northwestern Polytech. Univ., Xi´an, China
  • fYear
    2013
  • fDate
    16-17 Jan. 2013
  • Firstpage
    747
  • Lastpage
    750
  • Abstract
    Gas atomization can be used in producing high-quality metal powder and the atomizer has great influence on the production quality. In this paper, the annular orifice atomizer is optimized by adopting Laval nozzle as the shape of gas jet orifice and a three-dimensional model of supersonic annular orifice atomizer is adopted to investigate the flow field characteristic at different atomization gas pressure (P0), including gas velocity, static pressure and aspiration pressure at the delivery tube tip. The numerical results indicate that the maximum gas velocity in the atomization zone increases with increasing P0. The aspiration pressure is also found to increase as P0 increases. Comparing with annular slit atomizer, there is no airflow shock wave in the flow field, which can weak the atomization effect.
  • Keywords
    dissociation; flow simulation; nozzles; numerical analysis; pipe flow; sprays; supersonic flow; two-phase flow; Laval nozzle; Laval-style atomizer; aspiration pressure; delivery tube tip; flow field; gas atomization; gas jet orifice; gas velocity; high-quality metal powder; numerical simulation; static pressure; supersonic annular orifice atomizer; three-dimensional model; Atomic measurements; Electron tubes; Equations; Fluid flow; Mathematical model; Metals; Orifices; Laval nozzle; gas atomization; numerical simulation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Measuring Technology and Mechatronics Automation (ICMTMA), 2013 Fifth International Conference on
  • Conference_Location
    Hong Kong
  • Print_ISBN
    978-1-4673-5652-7
  • Type

    conf

  • DOI
    10.1109/ICMTMA.2013.186
  • Filename
    6493838