期刊文献+

自由流湍流度对某低压涡轮级气动影响的数值研究 被引量:2

Numerically investigate the effects of freestream turbulence on dynamics of a low-pressure turbine stage
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摘要 基于Langtry-Menter转捩模型,定常求解雷诺平均的三维粘性N-S方程组,数值研究了不同雷诺数工况下,自由流湍流度(FST)变化对某低压涡轮级流场及性能的影响,揭示了FST对该低压涡轮级叶片吸力面表面流动及涡轮级效率雷诺数效应的影响规律;并基于一种损失分离方法,细分了FST对该低压涡轮级内部各损失分量,如叶型损失、端壁边界层损失,叶尖泄漏损失的影响. Based on SST turbulence model coupled with Langtry-Menter transition model, a three-dimensional, vicous, steady CFD analysis was performed for investigating the effects of freestream turbulence on the dynamics of a LP turbine stage at different Reynolds numbers. From the CFD prediction results, the rules of freestream turbulence effects on the flow mechanics on blade suction surface, and on Reynolds number effects on this LP turbine stage efficiency were obtained. Also, based on a kind of loss separation method, freesteam turbulence effects on the flow loss components, such as the profile loss, the endwall boundary loss, and the tip clearance loss inside this LP turbine stage were further distinguished.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第8期1490-1497,共8页 Journal of Aerospace Power
关键词 自由流湍流度 雷诺数效应 低压涡轮 损失分离 转捩模型 freestream turbulence Reynolds number effects low-pressure turbine loss separations transion model
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参考文献6

  • 1罗华玲,乔渭阳,许开富.基于转捩模型的涡轮流场及性能数值模拟[J].西北工业大学学报,2007,25(6):778-783. 被引量:4
  • 2Mayle R E. The role of laminar-turbulent transition in gas turbine engines[R]. ASME Paper No. GT-1991-261, 1991.
  • 3Matsunuma T, Abe H. Influence of turbulence intensity on annular turbine stator aerodynamics at low reynolds number[R]. ASME Paper No. GT-1999-151, 1999.
  • 4Stieger R D, Hodson H P. The unsteady development of a turbulent wake through a downstream low-pressure turbine blade passage [R]. ASME Paper No. GT-2004- 53061, 2004.
  • 5Langtry R B, Menter F R. A correlation-based transition model using local variables Part Ⅱ-Test cases and industry applications [R]. ASME Paper No. GT-2004-53454, 2004.
  • 6Menter F R, Langtry R B. A correlation-based transition model using local variables Part Ⅰ-Model formulation[R]. ASME Paper No. GT-2004-53452, 2004.

二级参考文献11

  • 1杨琳,刘火星,邹正平,李维.低雷诺数条件下低压涡轮气动设计[J].工程热物理学报,2005,26(2):228-230. 被引量:7
  • 2杨琳,冯涛,邹正平,李维.低雷诺数涡轮内部流场分析[J].北京航空航天大学学报,2005,31(11):1194-1197. 被引量:13
  • 3Castner R,Chiappetta S.An Engine Research Program Focused on Low Pressure Turbine Aerodynamic Performance.ASME Paper GT 2002-30004.
  • 4Langtry R B,Menter F R.A Correlation-Based Transition Model Using Local Variables:Part Ⅱ -Test Cases and Industry Applications.ASME Paper ASME-GT2004-53454.
  • 5Menter F R,Langtry R B.A Correlation-Based Transition Model Using Local Variables:Part Ⅰ -Model Formulation.ASME Paper ASME-GT2004-53452.
  • 6Smith D J L,Johnston I H.Investigations on an Experimental Single-Stage Turbine of Conservative Design.ARC Reports and Memoranda,1967,3541.
  • 7Johnston I H,Smart D.An Experiment in Turbine Blade Profile Design.ARC Current Papers,1967,941.
  • 8Whitney W J,Schum H J,Behning F P.Cold-Air Investigation of a Turbine for High-Temperature-Engine Application,Ⅳ-Two-Stage Turbine Performance.NASA TN D-3751,1972.
  • 9Huang J,Corke T C,Thomas F O.Plasma Actuators for Separation Control of Low Pressure Turbine Blades.AIAA2003-1027.
  • 10李特维诺夫·尤·阿.航空涡轮喷气发动机的特性和使用性能.北京:国防工业出版社,1968.

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