Volume 37 Issue 3
Mar.  2022
Turn off MathJax
Article Contents
KONG Xiangzhuang, HE Wu, GUO Zhihui. Spray characteristics of liquid jet in nonuniform crossflow[J]. Journal of Aerospace Power, 2022, 37(3): 534-544. doi: 10.13224/j.cnki.jasp.20210151
Citation: KONG Xiangzhuang, HE Wu, GUO Zhihui. Spray characteristics of liquid jet in nonuniform crossflow[J]. Journal of Aerospace Power, 2022, 37(3): 534-544. doi: 10.13224/j.cnki.jasp.20210151

Spray characteristics of liquid jet in nonuniform crossflow

doi: 10.13224/j.cnki.jasp.20210151
  • Received Date: 2021-04-06
  • Publish Date: 2022-03-28
  • Spray characteristics of liquid jet in nonuniform velocity distribution crossflow were experimentally studied.The nonuniform velocity distribution was produced by perforated plates,the images of spray were captured with a light sheet and a single lens reflex camera,and a phase Doppler particle analyzer (PDPA) was used to measure droplets diameter and velocity.The experimental results indicated that,in the nonuniform crossflow,the bending state and breakup regime of each jet section were different,resulting in the difference of penetration and spray characteristics.Compared with uniform corssflow,the jets penetrated further into the crossflow when the column breakup height increased,and the concentration distribution was more uniform when the velocity distribution was in positive gradient,in addition,the jet presented a flat thrown profile.When the velocity gradient was negative,the spray field moved inward and presented a stratified structure,the jet wake region elongated,and the profile of jet was in collapse state.Correlations of a liquid jet for nonuniform crossflow are presented.Nonuniform crossflow can improve atomization and uniformity,and Sauter mean diameter (SMD) reaches a minimum value when the velocity distribution is negative gradient.

     

  • loading
  • [1]
    LOVETT J,BROGAN T,PHILIPPONA D,et al.Development needs for advanced afterburner designs[R].AIAA 2004-4192,2004.
    [2]
    EBRAHIMI H.Overview of gas turbine augmentor design,operation,and combustion oscillation[R].AIAA 2006-4916,2006.
    [3]
    FOUST M,THOMSEN D,STICKLES R,et al.Development of the GE aviation low emissions TAPS combustor for next generation aircraft engines[R].AIAA 2012-0936,2012.
    [4]
    WU P K,KIRKENDALL K A,FULLER R P,et al.Breakup processes of liquid jets in subsonic crossflows[J].Journal of Propulsion and Power,1997,13(1):64-73.
    [5]
    BIROUK M,AZZOPATDI B J,STABLER T.Primary break-up of a viscous liquid jet in a cross airflow[J].Particle and Particle Systems Characterization,2003,20(4):283-289.
    [6]
    BROUMAND M,BIROUK M.Liquid jet in a subsonic gaseous crossflow:recent progress and remaining challenges[J].Progress in Energy and Combustion Science,2016,57:1-29
    [7]
    林宇震,李林,张弛,等.液体射流喷入横向气流混合特性研究进展[J].航空学报,2014,35(1):46-57.
    [8]
    ELSHAMY O,TAMBE S,CAI J,et al.Structure of liquid jets in subsonic crossflow at elevated ambient pressures[R].AIAA-2006-1224,2006.
    [9]
    LAKHAMRAJU B.Liquid jet breakup studies in subsonic airstream at elevated temperatures[D].Lincinnati,Ohio,US:University of Cincinnati,2005.
    [10]
    STENZLER J N,LEE J G,SANTAVICCA D A,et al.Penetration of liquid jets in a crossflow[R].AIAA-2013-1327,2003.
    [11]
    TAMBE S B,ELSHAMY O JENG S M.Liquid jets injected transversely into a shear layer[R].Reno,Nevada,US:45th AIAA Aerospaces Science Meeting and Exhibit,2013.
    [12]
    TAMBE S B,ELSHAMY O,JENG S M.Spray properties of liquid jets injected transversely into a shear layer[R].Cincinnati,US:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,2013.
    [13]
    BECKER J,HASSA C.Liquid fuel placement and mixing of generic aeroengine premix module at different operating conditions[J].Journal of Engineering for Gas Turbines and Power,2003,125(4):901-908.
    [14]
    LIN C K,KENNEDY J P,JACKSON T A.A review of penetration heights of transverse liquid jets in high-speed flows[R].Lavergne,France:15th Annul Conference on Liquid Atomization and Spray System,1999.
    [15]
    WANG Q,MONDRAGON U M,BROWN C T,et al.Characterization of trajectory,break point,and break point dynamics of a plain liquid jet in a crossflow[J].Atomization and Sprays,2011,21(3):203-219.
    [16]
    ESLAMIAN M,AMIGHI A,ASHGRIZ N.Atomization of liquid jet in high-pressure and high temperature subsonic crossflow[J].AIAA Journal,2014,52(7):1374-1385.
    [17]
    RANGER A A,NICHOLLS A J.Aerodynamic shattering of liquid drops[J].AIAA Journal,1969,7(2):285-290.
    [18]
    WU P K,FULLER R P,KIRKENDALL K A,et al.Spray structures of liquid jets atomized in subsonic crossflows[J].Journal of Propulsion and Power,1998,14(2):173-182.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (470) PDF downloads(78) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return