期刊文献+

跨声压气机动叶弯、掠对静叶静压脉动的影响 被引量:1

Effect of bowed and swept rotors on stator pressure fluctuation in a transonic compressor
原文传递
导出
摘要 对一单级跨声压气机采用了三种弯、掠动叶后设计工况下的非定常流场分别进行了数值模拟,分析了动叶弯、掠对下游静叶表面静压非定常脉动的影响.研究结果表明:三种弯、掠动叶都减轻了静叶前缘顶部和根部的静压脉动,使静叶前缘所受到的静压扰动沿径向分布更为均匀,尤其是弯掠动叶的作用最为明显;除去叶片前缘区域,三种弯、掠动叶对下游静叶的顶部压力面和吸力面的扰动都有所减弱,仍然以弯掠动叶的作用最为显著,而在静叶的中部和根部前缘区域之外的表面,动叶的弯、掠对压力扰动的影响不明显. The unsteady 3-D flow fields in a transonic compressor at design point were simulated numerically to study the effect of the bowed and swept rotors on stator surface static pressure fluctuation.The results show that,all three types of bowed or swept rotors,especially the bowed-swept rotor,could weaken the static pressure fluctuation on the top and bottom of stator leading edge compared with the baseline.As a result,the stator surface pressure fluctuation near leading edge area becomes more uniform in radial direction.Expect for the stator leading edge area,the amplitude of pressure fluctuation decreases on the top of pressure and suction surface downstream the bowed and swept rotors,but the effect at mid-span and hub is insignificant.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2010年第10期2312-2318,共7页 Journal of Aerospace Power
基金 国家自然科学基金(50646021)
关键词 跨声压气机 非定常 静压脉动 transonic compressor unsteady bow sweep static pressure fluctuation
  • 相关文献

参考文献14

二级参考文献54

共引文献63

同被引文献13

  • 1Paul W Giel,NASA/GE Highly-loaded Turbine Research Program[C].AIAA Turbine Engine Testing Working Group Meeting,Cleveland,Ohio,May 8-9,2008.
  • 2R Florea,L Bertuccioli,T G Tillman.Flow-Control-Enabled Aggressive Turbine Transition Ducts and Engine System Analysis[R].AIAA 2006-3512,2006.
  • 3Stephane Baralon.Aggressive Intermediate Duct Aerodynamics for competitive and Environmentally Friendly Jet Engines[J].Aerodays 2006,Vienna,2006.
  • 4C Arroyo Osso,F Wallin and T G Johansson.Experimental and Numerical Investigation of an Aggressive Intermediate Turbine Duct:Part 1-Flowfield at Design Inlet Conditions[R].AIAA-2008-7055,2008.
  • 5C Arroyo Osso,F Wallin and T G Johansson.Experimental and Numerical Investigation of an Aggressive Intermediate Turbine Duct:Part 2-Flowfield under Off-design Inlet Conditions[R],AIAA-2008-7056,2008.
  • 6K Leach and R Thulin.Energy Efficient Engine-Turbine Transition Duct Model Technology Report[R].NASA CR-167996,Aug.1982.
  • 7M GAnderson.Fluent CFD versus sovran and klomp diffuser data benchmark study[R].AIAA 2008-665,2008.
  • 8孙志刚,黄洪雁,谭春青,冯国泰,张冬阳.某型燃机涡轮过渡段流场优化设计[J].工程热物理学报,2008,29(6):940-942. 被引量:23
  • 9毛凯,吴虎,徐倩楠.大涵道比涡扇发动机涡轮过渡段的数值研究[J].科学技术与工程,2012,20(6):1308-1313. 被引量:4
  • 10史峻,吴虎,宋石平.某型燃气轮机涡轮过渡段流场的数值模拟[J].航空计算技术,2012,42(1):4-7. 被引量:4

引证文献1

二级引证文献1

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