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环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比

韩吉昂 李晓东 钟兢军

韩吉昂, 李晓东, 钟兢军. 环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比[J]. 航空动力学报, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010
引用本文: 韩吉昂, 李晓东, 钟兢军. 环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比[J]. 航空动力学报, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010
HAN Ji-ang, LI Xiao-dong, ZHONG Jing-jun. Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor[J]. Journal of Aerospace Power, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010
Citation: HAN Ji-ang, LI Xiao-dong, ZHONG Jing-jun. Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor[J]. Journal of Aerospace Power, 2015, 30(2): 331-340. doi: 10.13224/j.cnki.jasp.2015.02.010

环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比

doi: 10.13224/j.cnki.jasp.2015.02.010
基金项目: 

国家高技术研究发展计划(2007AA05Z255)

中央高校基本科研业务费专项资金(3132015207)

详细信息
    作者简介:

    韩吉昂(1979-),男,河南襄城人,副教授,博士,主要从事发动机气动热力学研究.

  • 中图分类号: V235.1

Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor

  • 摘要: 采用三维雷诺平均Navier-Stokes(N-S)方程、renormalization group (RNG) k-ε湍流模型和标准壁面函数对驻涡腔有无喷射的环形中心钝体驻涡燃烧室的冷态流场进行了数值仿真,分析了驻涡腔有无喷射对环形中心钝体驻涡燃烧室涡系结构、驻涡腔流动参数和燃烧室总体性能的影响.结果表明:相比于无喷射时,驻涡腔添加喷射可以使驻涡腔内形成相对稳定的双驻涡结构;驻涡腔喷射的存在使得环形中心钝体驻涡燃烧室出口截面总压损失系数降低约9.2%,并能提高驻涡腔内的平均气流参数;驻涡腔喷射对环形中心钝体驻涡燃烧室出口截面流动参数沿流道高度方向的变化趋势影响不大.

     

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出版历程
  • 收稿日期:  2013-09-16
  • 刊出日期:  2015-02-28

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