涡流器燃烧室头部两相反应流数值模拟
Numerical investigation of two-phase reacting flows in annular combustor domes with swirl cup
-
摘要: 在任意曲线坐标系中数值模拟带涡流器燃烧室头部的三维两相反应流场,其中,采用偏微分方程法生成块结构网格;气相在Euler坐标系下采用修正的k-ε双方程模型处理紊流特性,用修正的EDM-Ar-rhenius紊流燃烧模型模拟化学反应速率,用六通量模型考虑热辐射的影响;液相处理采用在Lagrange坐标系下颗粒群轨道模型。在非交错网格系下采用SIMPLE算法及混分差分格式求解离散方程,采用单元内颗粒源法(PSIC)算法进行两相之间的耦合,计算所得的旋流数与试验数据相当接近。结果表明涡流器几何形状对燃烧室流场影响较大,涡流器的优化设计可以提高燃烧性能。Abstract: In arbitrary curvilinear coordinate system,numerical simulations of three-dimensional and two-phase reacting flows in annular combustor domes with the swirl cup are performed.The block-structured grids are generated by solving a system of elliptic partial differential equations.The gas phase equations are solved in an Eulerian frame of reference.Modified k-ε model is employed to describe the turbulent characteristics.Modified Eddy Dissipation Model-Arrhenius turbulent combustion model is used to determine the reaction rate.To consider the influence of heat radiation,the six flux model is applied to the predictions of radiant heat transfer in the combustor.The liquid phase is treated in a Lagrangian frame of reference with the particle trajectory model.Hybrid scheme and SIMPLE algorithm are used to solve the finite-difference equations in non-staggered grid system.The couple of the gas phase and the liquid phase is adopted by the Particle Source in cell Method(PSIC).The calculating swirl number is in agreement with experimental data.Predictions show that the influence of different geometries of the swirl cup on combustor flow characteristics is considerable.So the combustion performance may be improved by the optimum design of the swirl cup.
-
Key words:
- aerospace propulsion system /
- numerical simulation /
- two-phase reacting flow /
- swirl cup /
- combustor
-
[1] Mongia H C,M.AI-Roub,et al,Swirl Cup Modeling Part I[R].AIAA Paper 2001-3576,2001. [2] Manampathy G G,Mongia H C.Swirl Cup Modeling-Part Ⅲ:Spray Combustion in CFM-56 Single Cup Flame Tube[R].AIAA Paper 2003-0319,2003. [3] 赵坚行,燃烧的数值模拟[M],北京:科学出版社,2002. [4] Lee D,Yeh L.Numerical Simulations of Gas Turbine Combustor Flows[J].Journal of Propulsion and Power,1993,37(4):322. [5] Magnussen B F.Effects of Turbulent Structure and Local Concentrations on Soot Formation and Combustion in C2 H2Diffusion Flames[R].17th Symposium(Int.) on Combustion,p.1383,1978 [6] Khali E E.Modelling of Furnaces and Combustors[M].Abacus Press.1982. [7] 蔡文祥,胡好生,赵坚行.环形燃烧室火焰筒及旋流器流场计算[J].工程热物理学报,2005,26:253-256.Cai Wenxiang,Hu Haosheng,Zhao Jianxing.Numerical Simulation of Turbulent Flows in Annul Combustors with Swirler[J].Journal of Engineering Thermophysics,2005,26:253-256.
点击查看大图
计量
- 文章访问数: 1588
- HTML浏览量: 2
- PDF量: 462
- 被引次数: 0