期刊文献+

环形燃烧室火焰筒及旋流器流场计算 被引量:2

NUMERICAL SIMULATION OF TURBULENT FLOWS IN ANNUAL COMBUSTORS WITH SWIRLER
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摘要 本文采用偏微分方程法生成贴体网格,在任意曲线坐标系下数值研究两种先进燃烧室火焰筒及其旋流器三维紊流流场。由于旋流器的形状复杂,本文采用型线定点法确定网格的边界。在非交错网格系下采用SIMPLE算法和混合差分格式对离散方程进行求解。计算结果表明计算方法合理,这计算程序进一步扩展,可用来预估环形燃烧室反应流流场。 In this paper, the body-fitted grids of the combustor with the swirl cup are generated by an elliptical grid generation technique. Numerical simulations of three-dimensional inert turbulent flows in two annular combustors with the swirl cup are developed in arbitrary curvilinear coordinate systems. For the complicated shape of the swirler , a boundary grid generation procedure is developed by treating the swirler as a obstacle and by suitably meshing near it. Hybrid scheme and SIMPLE algorithm are used to solve the finite difference equations on a non-staggered grid system. The results of calculation show that the numerical procedure is reasonable and can be expended to predict the turbulent reacting flows in the annular combustor.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第z1期253-256,共4页 Journal of Engineering Thermophysics
关键词 火焰筒 旋流器 贴体网格 数值计算 冷态流场 combustor swirler body-fitted grid numerical simulation non-reacting flow
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参考文献3

  • 1[1]Adel M, Michael B.A New Air Blast Nozzle for Advanced Gas Turbine Gas Turbine Combustors. ASME 2000-GT-0117, 2000
  • 2[2]Kessler B N, Theisen P. Flow Field Mixing Characteristics of An Aero-Engine Combustor, Part Ⅱ: Numerical Simulations. AIAA, 2002-3708, 2002
  • 3赵坚行,伍艳玲,周琳.先进燃烧室涡流杯流场计算[J].工程热物理学报,2000,21(1):110-114. 被引量:13

二级参考文献2

  • 1伍艳玲.燃烧室双级旋流器计算:[硕士论文].南京:南京航空航天大学,1998..
  • 2伍艳玲,硕士学位论文,1998年

共引文献12

同被引文献11

  • 1Manampathy 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.
  • 2Lee D, Yeh L. Numerical Simulations of Gas Turbine Combustor Flows[J]. Journal of Propulsion and Power, 1993,37(4) : 322.
  • 3Magnussen B F. Effects of Turbulent Structure and Local Concentrations on Soot Formation and Combustion in C2H2 Diffusion Flames[R]. 17^th Symposium (Int.) on Combustion ,p. 1383,1978.
  • 4Khali E E. Modelling of Furnaces and Combustors[M]. Abacus Press. 1982.
  • 5Mongia H C,M. AI-Roub,et al,Swirl Cup Modeling Part Ⅰ[R]. AIAA Paper 2001-3576,2001.
  • 6Adel M ,Michael B. A new hybrid air blast nozzle for advanced gas turbine gas turbine combustors [R].ASME 2000-GT-0117, Munich, Germany: [s. n. ],2000.
  • 7Kessler B N ,Theisen P. Flow field mixing characteristics of an aero-engine combustor,part Ⅱ:numerical simulations [R ]. AIAA 2002-3708, Indiana, US: AIAA, 2002.
  • 8Hassa C, Voigt P. Flow field charactersitics of an aero-engine combustor-part Ⅰ:experimental results [R]. AIAA 2002-3709, Indiana, US: AIAA,2002.
  • 9Koh H, Kim D, Jung K,et al. The effects of swirler geometry on the performance of gas turbine combustor using planar imaging technique[R]. AIAA 2001-3757,Salt Lane City, US:AIAA,2001.
  • 10陈兴隆,周力行,张健.甲烷-空气同轴突扩湍流燃烧的新二阶矩模型的数值模拟[J].工程热物理学报,1999,20(6):759-763. 被引量:4

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