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折流燃烧室两相喷雾燃烧流场数值模拟

颜应文 宋双文 胡好生 王倚阳 雷雨冰 赵坚行 林志勇

颜应文, 宋双文, 胡好生, 王倚阳, 雷雨冰, 赵坚行, 林志勇. 折流燃烧室两相喷雾燃烧流场数值模拟[J]. 航空动力学报, 2011, 26(5): 1003-1010.
引用本文: 颜应文, 宋双文, 胡好生, 王倚阳, 雷雨冰, 赵坚行, 林志勇. 折流燃烧室两相喷雾燃烧流场数值模拟[J]. 航空动力学报, 2011, 26(5): 1003-1010.
YAN Ying-wen, SONG Shuang-wen, HU Hao-sheng, WANG Yi-yang, LEI Yu-bing, ZHAO Jian-xing, LIN Zhi-yong. Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor[J]. Journal of Aerospace Power, 2011, 26(5): 1003-1010.
Citation: YAN Ying-wen, SONG Shuang-wen, HU Hao-sheng, WANG Yi-yang, LEI Yu-bing, ZHAO Jian-xing, LIN Zhi-yong. Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor[J]. Journal of Aerospace Power, 2011, 26(5): 1003-1010.

折流燃烧室两相喷雾燃烧流场数值模拟

基金项目: 中国博士后科学基金(20090461115); 江苏省博士后科研资助计划(0901033C)

Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor

  • 摘要: 在任意曲线坐标系下对折流燃烧室两相喷雾燃烧流场进行数值模拟,采用偏微分方程法生成三维贴体网格,采用k-ε双方程模型模拟湍流黏性,分别采用EBU(eddy break-up)-Arrhenius燃烧模型、EDC(eddy dissipation concept)燃烧模型以及二阶矩(second-order-moment,简称SOM)燃烧模型模拟化学反应速率,在非交错网格下,采用欧拉-拉格朗日方法模拟气液两相喷雾燃烧过程,气液之间相互耦合采用PSIC(particle-source-in-cell)算法求解.数值分析不同湍流燃烧模型对折流燃烧室两相喷雾燃烧流场的影响,计算结果与试验数据比较,表明采用不同湍流燃烧模型所得的两相喷雾燃烧流场有所不同,其中SOM燃烧模型和EBU燃烧模型都能较好地数值模拟折流燃烧室两相喷雾燃烧过程.

     

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出版历程
  • 收稿日期:  2010-04-22
  • 修回日期:  2010-07-05
  • 刊出日期:  2011-05-28

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