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

一种波瓣混合器超级燃烧室的掺混特性

程晓军 范育新 蔡迪 王家骅

程晓军, 范育新, 蔡迪, 王家骅. 一种波瓣混合器超级燃烧室的掺混特性[J]. 航空动力学报, 2014, (7): 1606-1614. doi: 10.13224/j.cnki.jasp.2014.07.013
引用本文: 程晓军, 范育新, 蔡迪, 王家骅. 一种波瓣混合器超级燃烧室的掺混特性[J]. 航空动力学报, 2014, (7): 1606-1614. doi: 10.13224/j.cnki.jasp.2014.07.013
CHENG Xiao-jun, FAN Yu-xin, CAI Di, WANG Jia-hua. Mixing characteristics of hyperburner with a lobed mixer[J]. Journal of Aerospace Power, 2014, (7): 1606-1614. doi: 10.13224/j.cnki.jasp.2014.07.013
Citation: CHENG Xiao-jun, FAN Yu-xin, CAI Di, WANG Jia-hua. Mixing characteristics of hyperburner with a lobed mixer[J]. Journal of Aerospace Power, 2014, (7): 1606-1614. doi: 10.13224/j.cnki.jasp.2014.07.013

一种波瓣混合器超级燃烧室的掺混特性

doi: 10.13224/j.cnki.jasp.2014.07.013
基金项目: 

江苏省普通高校研究生科研创新计划(CXZZ12_0167)

详细信息
    作者简介:

    程晓军(1986-),男,陕西宝鸡人,博士生,主要从事脉冲爆震发动机低阻起爆技术研究及涡扇冲压组合发动机燃烧室燃烧组织方面研究。

  • 中图分类号: V236

Mixing characteristics of hyperburner with a lobed mixer

  • 摘要: 为了使涡轮基组合循环发动机超级燃烧室的涡扇涵道和冲压涵道两股气流具有高效低阻的掺混特性,设计了一种结构简单的方形波瓣混合器.用数值模拟方法对该方形波瓣混合器与常规混合器进行了比较分析,结果表明方形波瓣混合器具有与菊花型波瓣混合器相似的流向涡高效低阻掺混特性.进行混合器结构参数变化对掺混特性的影响研究发现扩张角对方形波瓣混合器的热混合效率的影响起主要作用,而出口高度的影响不大;当方形波瓣混合器的波长比为1.0时,方形波瓣混合器具有高效低阻的掺混特性.

     

  • [1] 刘大响,金捷.21世纪世界航空动力技术发展趋势与展望[J].中国工程科学,2004,6(9):1-8. LIU Daxiang,JIN Jie.The development trends and prospect of world aeroprolulsion technology in the 21st century[J].Engineering Science,2004,6(9):1-8.(in Chinese)
    [2] Lee J,Winslow R,Buehrle R L.The GE-NASA RTA hyperburner design and development[R].NASA/TM 2005-213803,2005.
    [3] Saunders J D,Stueber T J,Thomas S R,et al.Testing of the NASA hypersonics project's combined cycle engine large scale inlet mode transition experiment (CCELIMX)[R].NASA/TM-2012-217217,2012.
    [4] Bridges J,Wernet M P.Cross-stream PIV measurements of jets with internal lobed mixers[R].AIAA-2004-2896,2004.
    [5] McCormick D C,Bennett J C,Jr.Vortical and turbulent structure of a lobed mixer free shear layer[J].AIAA Journal,1999,37(9):1852-1859.
    [6] Cooper N J,Merati P.Numerical simulation of the vortical structures in a lobed jet mixing flow[R].AIAA-2005-635,2005.
    [7] LIU Youhong.Experimental and numerical investigation of circularly lobed nozzle with/without central plug[J].International Journal of Heat and Mass Transfer,2002,45(12):2577-2585.
    [8] 岳巍,雷志军,苏尚美,等.波瓣混合器涡系结构及射流掺混机理的数值研究[J].航空动力学报,2013,28(2):338-346. YUE Wei,LEI Zhijun,SU Shangmei,et al.Numerical investigation on vortex structure and jet mixing mechanism in lobed mixer[J].Journal of Aerospace Power,2013,28(2):338-346.(in Chinese)
    [9] 李立国,张靖周.航空用引射混合器[M].北京:国防工业出版社,2007.
    [10] Mao R,Yu S C M,Chua L P.On the vorticity characteristics of lobe-forced mixer at different configurations[J].Experiments in Fluids,2009,46(6):1049-1066.
    [11] Abolfadl A,Metwally M A,El-Messiry A M,et al.Experimental investigation of lobed mixer performance[J].Journal of Propulsion and Power,2001,17(5):1109-1116.
    [12] SHAN Yong,ZHANG Jingzhou.Numerical investigation of flow mixture enhancement and infrared radiation shield by lobed forced mixer[J].Applied Thermal Engineering,2009,29(17/18):3687-3695.
    [13] Wellner J,Rober T,Tranb P.On the development and application of a hybrid approach to the simulation of broadband noise in a lobed mixer[R].AIAA-2011-2799,2011.
    [14] LI Ping,LI Wenlong,HE Guoqiang.Research on turbulent mixing of the bypass and core flows for air-turbo-rocket[J]. Journal of Solid Rocket Technology,2012,35(1):47-52.
    [15] Majamaki A J,Smith O I,Karagozian A R.Passive mixing control via lobed injectors in high-speed flow[J].AIAA Journal,2003,41(4):623-632.
    [16] XIE Yi,LIU Youhong.Numerical investigation of lobe spacing ratio on performance of forced mixer nozzle[J].Heat Transfer Asian Research,2011,40(7):593-607.
    [17] Salman H,Page G J,McGuirk J J.Prediction of lobed mixer vortical structures with a k-ε turbulence model[J].AIAA Journal,2003,41(5):878-887.
  • 加载中
计量
  • 文章访问数:  1423
  • HTML浏览量:  6
  • PDF量:  803
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-04-17
  • 刊出日期:  2014-07-28

目录

    /

    返回文章
    返回