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数值分析二级涡流器环形燃烧室的燃烧性能
引用本文:李井华,赵坚行.数值分析二级涡流器环形燃烧室的燃烧性能[J].航空动力学报,2007,22(8):1233-1240.
作者姓名:李井华  赵坚行
作者单位:南京航空航天大学高新技术研究院, 南京 210016
摘    要:采用多维经验分析法在任意曲线坐标系下对包括二级突扩扩压器、双级轴向涡流器及火焰筒在内的单头部环形燃烧室的燃烧性能进行计算.并对RNGk-ε紊流模型加以改进, 使其更适用于数值模拟非交错贴体坐标系下的三维两相化学反应流.采用EBU-Arrhenius紊流燃烧模型、六通量热辐射模型以及颗粒群轨道模型对油雾燃烧进行模拟.同时, 数值分析了不同涡流器几何尺寸对燃烧室整体流场和燃烧性能的影响, 数值计算结果与实验数据相当一致, 表明计算方法合理, 计算程序可靠, 可用来估算环形燃烧室的燃烧性能. 

关 键 词:航空、航天推进系统    环形燃烧室    RNGk-ε紊流模型    火焰筒    涡流器    燃烧性能
文章编号:1000-8055(2007)08-1233-08
收稿时间:2006/7/31 0:00:00
修稿时间:2006年7月31日

Numerical analysis of combustion performance in an annular combustor with two-stage swirler
LI Jing-hua and ZHAO Jian-xing.Numerical analysis of combustion performance in an annular combustor with two-stage swirler[J].Journal of Aerospace Power,2007,22(8):1233-1240.
Authors:LI Jing-hua and ZHAO Jian-xing
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:In an arbitrary curvilinear coordinate system, a multidimensional empirical analysis methodology was developed to calculate the combustion performance of an annular combustor, which consists of the dump diffuser, two-stage flame tube and cooling passages.The RNG k-ε turbulent model was also modified, for enabling correct calculations of three-dimensional and two-phase turbulent reactive flows under a non-staggered grid system.Spray combustion was simulated through EBU-Arrhenius turbulent combustion model, six-flux radiation model and particle trajectory model.And numerical analysis was conducted for the effects of the geometry of swirlers on entire combustor flow fields and combustion performances.Predictions and measurements were in satisfactory agreement, and it was shown that numerical procedures are fairly reasonable and reliable for estimating the combustion performances of annular combustors. 
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