Volume 26 Issue 10
Oct.  2011
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2011  >  26(10): 2267-2273
SONG Shuang-wen, LEI Yu-bing, YAO Shang-hong, MA Hui, HU Hao-sheng. Experimental study on compressible flow in trapped vortex cavity[J]. Journal of Aerospace Power, 2011, 26(10): 2267-2273.
Citation: SONG Shuang-wen, LEI Yu-bing, YAO Shang-hong, MA Hui, HU Hao-sheng. Experimental study on compressible flow in trapped vortex cavity[J]. Journal of Aerospace Power, 2011, 26(10): 2267-2273.
shu

Experimental study on compressible flow in trapped vortex cavity

  • 1.

    China Aviation Powerplant Research Institute, Aviation Industry Corporation of China, Zhuzhou Hunan 41200

  • 2.

    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • Received Date: 2010-11-23
  • Rev Recd Date: 2011-02-12
  • Publish Date: 2011-10-28
    Abstract
  • The effect of geometry and aerodynamic factors on the flow in trapped vortex cavity was evaluated.The effect of geometry was analyzed by altering the ratio of height to length(H/L) of the cavity,injection position and main-flow inlet angle;the impact of aerodynamics was analyzed by varying main-flow and second inject flow inlet velocity.Total pressure loss was measured by total pressure probe,and the velocity field was measured by particle image velocimetry (PIV).The results reveal that:(1) When the position of the injection holes is in the bottom or the middle position,large scale vortexes can be formed in the trapped vortex cavity.A couple of opposite swirling vortexes are formed in the middle position;and only a single vortex can be formed in the bottom. (2) For the middle injection configuration, increasing the main-flow mach number and inlet angle can enhance the vortex intensity in the upside of the cavity. (3) The total pressure loss increases apparently with the growing main-flow inlet Mach number.

     

    • FullText(HTML)
  • loading
    • References(12)
  • [1]
    Roquemore W M,Shouse D,Burrus D L,et al.Vortex combustor concept for gas turbine engines .AIAA 2001-0483,2001.
    [2]
    Straub D L,Casleton K H,Lewis R E,et al.Assessment of rich-burn,quick-mix,lean-burn trapped vortex combustor for stationary gas turbines[J].ASME Journal of Engineering for Gas Turbines and Power,2005,127(1):36-41.
    [3]
    Burrus D L,Johnson A W,Roquemor W M,et al.Performance assessment of a prototype trapped vortex combustor concept for gas turbine application .ASME 2001-GT-0087,2001.
    [4]
    Hendricks R C,Shouse D T,Roquemore W M.Experimental and computational study of trapped vortex combustor sector rig with tri-pass diffuser .NASA TM-2004-212507,2004.
    [5]
    Hendricks R C,Buehrle R,Liu N S,et al.Numerical simulation of the RTA combustion rig .NASA TM-2005-21389,2005.
    [6]
    Meyer T R,Brown M S,Fonov S,et al.Optical diagnostics and numerical characterization of a trapped-vortex combustor .AIAA 2002-3863,2002.
    [7]
    Zelina J,Ehret J,Hancock R D,et al.Ultra-compact combustion technology using high swirl for enhanced burning rate .AIAA 2002-3725,2002.
    [8]
    Thornburg H,Zelina B S,Greenwood R.Numerical study of an inter-turbine burner (ITB) concept with curved radial vane .AIAA 2007-649,2007.
    [9]
    樊未军,易琪,严明,等.驻涡燃烧室凹腔双涡结构研究[J].中国电机工程学报,2006,26(9):66-70. FAN Weijun,YI Qi,YAN Ming,et al.A study of double vortex structure in the trapped vortex combustor[J].Proceedings of the CSEE,2006,26(9):66-70.(in Chinese)
    [10]
    邢菲,樊未军,张荣春,等.蒸发管供油的单驻涡燃烧室贫油点火试验[J].推进技术,2009,30(5):523-527. XING Fei,FAN Weijun,ZHANG Rongchun,et al.Ignition performance of a single trapped vortex combustor with evaporation tube as fuel supply[J].Journal of Propulsion Technology,2009,30(5):523-527.(in Chinese)
    [11]
    孔祥雷,樊未军,邢菲,等.单涡/贫油驻涡燃烧室的出口温度分布试验[J].航空动力学报,2010,25(4):784-799. KONG Xianglei,FAN Weijun,XING Fei,et al.Experimental study on outlet temperature distribution in ingle vortex/lean oil trapped vortex combustor[J].Journal of Aerospace Power,2010,25(4):784-799.(in Chinese)
    [12]
    张弛.切向驻涡燃烧室基础研究 .北京:北京航空航天大学,2007. ZHANG Chi.Basal research on tangent trapped vortex combustor .Beijing:Beijing University of Aeronautics and Astronautics,2007.(in Chinese)
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF(1673.0KB)
    XML

    Article Metrics

    Article views (2017) PDF downloads(14) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return