期刊文献+

跨声速动叶弯和掠对非定常气动负荷的影响 被引量:5

EFFECT OF BOWED AND SWEPT ROTORS ON UNSTEADY AERODYNAMIC LOADING IN A TRANSONIC COMPRESSOR
原文传递
导出
摘要 对一单级跨声压气机设计工况下采用三种弯、掠动叶后的非定常流场分别进行了数值模拟,分析了动叶弯、掠对叶片气动负荷的非定常影响。研究结果表明:与原型动叶相比,三种弯、掠动叶由于改变了动叶气动负荷的分布苇心,其气动力矩的时均值都发生了明显的改变;动叶弯、掠使动叶和静叶气动负荷参数随时间的波动幅值明显降低,有益于动、静叶的强度保证;四种压气机模型动叶和静叶的气动负荷参数随时间的波动曲线的相位都发生了变化。 The unsteady 3-D flow fields in a transonic compressor at design point were simulated numerically to study the effects of the bowed and swept rotors on the aerodynamic loading of the blades. The results show that, compared with the baseline, the time-averaged aerodynamic moment of the bowed or swept rotors changes obviously. And the phases of the aerodynamic loading parameters fluctuation waves in time of both rotors and stators are shifted when bowed or swept rotors are applied. And the amplitude of the aerodynamic loading parameters fluctuation in time is evidently reduced with bowed or swept rotors, especially with bowed-swept rotor.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2010年第10期1663-1666,共4页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.50646021)
关键词 跨声压气机 非定常 气动负荷 transonic compressor bow sweep unsteady aerodynamic loading
  • 相关文献

参考文献7

二级参考文献21

  • 1宁卫,刘前智,姚吉先,周新海.跨音速压气机动静叶排相干的三维非定常流动数值分析[J].航空动力学报,1996,11(2):161-164. 被引量:10
  • 2邹正平.叶轮机三维复杂流动的若干问题[M].北京:北京航空航天大学,1999..
  • 3吴先鸿.用涡方法研究叶轮机内动静叶间的相互作用[M].北京:北京航空航天大学,1997..
  • 4毛明明,宋彦萍,王仲奇.跨声轴流压气机动叶的三维弯掠设计研究.见:2006航空宇航科学与技术全国博士生学术论坛论文集.北京:2006.490-499
  • 5Sanders A J, Fleeter S. Multi-Blade Row Interactions in a Transonic Axial Compressor, Part Ⅱ: Rotor Wake Forcing Function &: Stator Unsteady Aerodynamic Response. ASME Paper 2001, GT 2001-0269
  • 6Mailach R, Vogeler K. Aerodynamic Blade Row Interactions in an Axial Compressor, Part Ⅱ: Unsteady Profile Pressure Distribution and Blade Forces. ASME Paper 2003, GT2003-38766
  • 7Mailach R, Vogeler K. Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor, Part Ⅱ: Unsteady Aerodynamic Forces of Rotor and Stator Blade. ASME Paper 2004, GT2004 53099
  • 8Denton J D, Xu L. The Effects of Lean and Sweep on Transonic Fan Performance. ASME Paper 2002, GT2002- 30327.
  • 9Beini E, Biollo R. On the Aerodynamics of Swept and Leaned Transonic Compressor Rotors. ASME Paper 2006, GT2006-90547.
  • 10Braun M, Seume J R. Forward Sweep in a Four-Stage High-Speed Axial Compressor. ASME Paper 2006, GT2006=90218.

共引文献33

同被引文献39

  • 1尹喜庆,刘仲祥,穆勇.后掠叶片对轴流泵抗汽蚀性能的影响[J].应用科技,2005,32(5):52-54. 被引量:3
  • 2方昌德.飞机燃气涡轮发动机高周疲劳研究计划[J].国际航空,2005(8):63-65. 被引量:3
  • 3王仲奇,韩万今,徐文远,赵桂林.在低展弦比透平静叶栅中叶片的弯曲作用[J].工程热物理学报,1990,11(3):255-262. 被引量:35
  • 4王仲奇.一代新型轴流式透平机械叶片——叶片的弯扭联合气动成型理论及其实验结果[R].工程热物理能源利用学科气动热力学发展战略研讨会专题报告汇编,1989:55-65.
  • 5Han Wanjin, Wang Zhongqi.Relationships Between Static Pressure Distribution on Walls and Secondary Flow Losses in Rectangular Turbine Stator Cascades with Leaned and Curvilinear Blade at Different Incidences[C].Germany:INTERFLUID 1st International Congress on Fluid Handling Systems,1990.
  • 6Shi Jing.An Investigation of a Highly Loaded Transonic Turbine Stages with Compound Leaned Vans[J].Trans of ASME, Journal of Engineering for Gas Turbine and Power,1986,1(3):255-262.
  • 7Wisler D C, Bauer R C, Okiishi T H.Secondary Flow Turbulent Diffusion and Mixing in Axial-Flow Compressors[R].ASME 87-GT-16.
  • 8Breugelmans F A E.Influence of Incidence Angle on the secondary Flow in Compressor Cascade with Different Dihedral Distribution[R].ISABE 85-7078.
  • 9Bogod A B.Direct and Inverted Calculation of 2D Axisymmetric and 3D Flows in Axial Compressor Blade Rows[R].TsAGI, Russia, 1992.
  • 10Seo S J, Choi S M, Kim K Y.Design Optimization of a Low-Speed Fan Blade with Sweep and Lean[J].Journal of Power and Energy,2008,222(87).

引证文献5

二级引证文献28

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部