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反向双旋涡流器受限火焰特性的流场分析

曾青华 孔文俊

曾青华, 孔文俊. 反向双旋涡流器受限火焰特性的流场分析[J]. 航空动力学报, 2016, 31(12): 2888-2894. doi: 10.13224/j.cnki.jasp.2016.12.009
引用本文: 曾青华, 孔文俊. 反向双旋涡流器受限火焰特性的流场分析[J]. 航空动力学报, 2016, 31(12): 2888-2894. doi: 10.13224/j.cnki.jasp.2016.12.009
ZENG Qing-hua, KONG Wen-jun. Flow field analysis for confined flames characteristics of counter dual-stage swirler[J]. Journal of Aerospace Power, 2016, 31(12): 2888-2894. doi: 10.13224/j.cnki.jasp.2016.12.009
Citation: ZENG Qing-hua, KONG Wen-jun. Flow field analysis for confined flames characteristics of counter dual-stage swirler[J]. Journal of Aerospace Power, 2016, 31(12): 2888-2894. doi: 10.13224/j.cnki.jasp.2016.12.009

反向双旋涡流器受限火焰特性的流场分析

doi: 10.13224/j.cnki.jasp.2016.12.009
基金项目: 

国家自然科学基金(51406196)

详细信息
    作者简介:

    曾青华(1982-),男,湖南常宁人,助理研究员,博士,主要从事燃烧理论与燃烧室研究.

  • 中图分类号: V231.2;TK263.4

Flow field analysis for confined flames characteristics of counter dual-stage swirler

  • 摘要: 分析了反向双旋涡流器受限燃烧火焰特性所对应的流场结构特征.研究发现:反向双旋涡流器流场结构随着受限比变化而发生变化.在受限比小于3.8时,流场上中心回流泡随着受限比增大而变长,与单级旋流涡流器流场上中心回流泡的生长规律相同;但受限比的继续增大,反向双旋涡流器流场上中心回流泡的生长则表现出不同于单级旋流涡流器的规律.单级旋流涡流器流场上中心回流泡会继续生长变长,而反向双旋涡流器流场上中心回流泡会在中间某位置出现分裂,呈现出前后两个不同的回流泡.该研究结果深化了对受限程度影响流动和燃烧的物理机制的认识,同时为反向双旋涡流器的优化设计提供指导.

     

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出版历程
  • 收稿日期:  2015-11-02
  • 刊出日期:  2016-12-28

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