留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

偏心对双级旋流器出口流场影响数值模拟

蒋尧 胡建 胡好生

蒋尧, 胡建, 胡好生. 偏心对双级旋流器出口流场影响数值模拟[J]. 航空动力学报, 2015, 30(12): 2919-2924. doi: 10.13224/j.cnki.jasp.2015.12.015
引用本文: 蒋尧, 胡建, 胡好生. 偏心对双级旋流器出口流场影响数值模拟[J]. 航空动力学报, 2015, 30(12): 2919-2924. doi: 10.13224/j.cnki.jasp.2015.12.015
JIANG Yao, HU Jian, HU Hao-sheng. Numerical simulation on the effect of misalignment on outlet flow field of double-swirler[J]. Journal of Aerospace Power, 2015, 30(12): 2919-2924. doi: 10.13224/j.cnki.jasp.2015.12.015
Citation: JIANG Yao, HU Jian, HU Hao-sheng. Numerical simulation on the effect of misalignment on outlet flow field of double-swirler[J]. Journal of Aerospace Power, 2015, 30(12): 2919-2924. doi: 10.13224/j.cnki.jasp.2015.12.015

偏心对双级旋流器出口流场影响数值模拟

doi: 10.13224/j.cnki.jasp.2015.12.015
详细信息
    作者简介:

    蒋尧(1988-),男,江苏镇江人,工程师,硕士,主要从事燃烧室气动设计工作.

  • 中图分类号: V231.3

Numerical simulation on the effect of misalignment on outlet flow field of double-swirler

  • 摘要: 采用Fluent软件,数值模拟了一级旋流器和二级旋流器偏心情况下,双级旋流器出口流场变化,湍流模型采用标准k-ε模型,计算了3种不同偏心量(0,0.5,1.7mm)下的双级旋流器出口流场,并将计算结果与试验结果进行了对比.研究表明:偏心对双级旋流器出口流场影响较大,0.5mm偏心下双级旋流器出口的回流区发生畸变,径向速度峰值区域位于X/D=0.5~1.0范围内;轴向速度和径向速度的计算结果与试验结果吻合良好.

     

  • [1] McDonell V G,Arellao L,Lee S W,et al.Effect of hardware alignment of fuel distribution and combustion performance for a production engine fuel injection assembly[R].Irvine,California:26th Symposium on Combustion,1996.
    [2] Nikjooy M,Mongia H C,Samuelsen G S,et al.A numerical and experimental study of confined swirling jets[R].AIAA 89-2898,1989.
    [3] Ateshkadi A,Mcdonell V,Samuelsen G S.Effect of hardware geometry on gas and drop behavior in a radial mixer spray[R].AIAA 98-0247,1998.
    [4] Hsiao G,Mongia H C.Swirl cup modeling:Part Ⅲ grid independent solution with different turbulence models[R].AIAA-2003-1349,2003.
    [5] Hsiao G,Mongia H C,Vij A.Swirl cup modeling:Part Ⅱ inlet boundary conditions[J].AIAA-2003-1350,2003.
    [6] Grinstein F F,Young T R,LI Guoqiang,et al.Computational and experimental analysis of the flow dynamics in a multi-swirler combustor[R].AIAA-2002-1006,2002.
    [7] Mongia H C,AI-Roub M,Danis A,et al.Swirl cup modeling:Part Ⅰ[R].AIAA-2001-3576,2001.
    [8] FU Yongqiang,CAI Jun,Jeng S M,et al.Confinement effects on the swirling flow of a counter-rotating swirl cup[J].ASME Paper GT2005-68622,2005.
    [9] CAI Jun,FU Yongqiang,Flohre N.Experimental study on coherent structures of a counter-rotating multi-swirler cup[J].AIAA-2007-5674,2007.
    [10] Reddy A P,Sujith R I,Chakravarthy S R.Swirler flow field characteristic in a sudden expansion combustor geometry[J].Journal of Propulsion and Power,2006,22(4):800-808.
    [11] Syred N,Beer J M.Combustion in swirling flows:a review[J].Combustion and Flame,1974,23(2):143-201.
    [12] Adrian S,Hollis D,Carrote J.PIV measurements of combustor turbulence fields[J].ASME Paper GT2007-28050,2007.
    [13] Ramos J I,Somert H T.Swirling flow in a research combustor[J].AIAA Journal,1985,23(2):241-248.
    [14] Rizk N K,Mongia H C.Three-dimensional analysis of gas turbine combustors[J].Journal of Propulsion and Power,1991,7(3):445-451.
    [15] Rosfjord T J,Russell S.Nozzle design and manufacturing influences on fuel spray circumferential uniformity[J].Journal of Propulsion and Power,1989,5(2):144-150.
    [16] Rosfjord T J,Eckerle W A.Aerating fuel nozzle design influence on airflow features[J].Journal of Propulsion and Power,1991,7(6):849-856.
    [17] Cohen J M,Rosfjord T J.Influences on the sprays formed by high-shear fuel nozzle/swirler assemblies[R].Journal of Propulsion and Power,1993,9(1):16-27.
    [18] 蒋尧.双级旋流器偏心对旋流器出口流场影响研究[D].湖南 株洲:中国航空动力机械研究所,2013. JIANG Yao.Research on the outlet flow field of double-swirler'smisalignment[D].Zhuzhou Hunan:China Aviation Powerplant Research Institute,2013.(in Chinese)
  • 加载中
计量
  • 文章访问数:  976
  • HTML浏览量:  52
  • PDF量:  454
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-04-28
  • 刊出日期:  2015-12-28

目录

    /

    返回文章
    返回