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Numerical Investigation on Effectiveness of Flow Separation Control in Two-dimensional High-load Compressor Cascade by Synthetic Jet 被引量:3

Numerical Investigation on Effectiveness of Flow Separation Control in Two-dimensional High-load Compressor Cascade by Synthetic Jet
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摘要 The effectiveness of flow separation control in two-dimensional high load cascade by synthetic jet is investigated through numerical simulation of the effect of excitation frequency and amplitude together with the adaptability of synthetic jet to off-design conditions. Test results indicate that synthetic jet can be used to effectively control the large-scale two-dimensional flow separation in compressor cascade. Preferable results can be obtained when excitation frequency is close to or times of the characteristic frequency of original flow field. Excitation amplitude has a more important effect on the effectiveness of flow separation control, and the increase in excitation amplitude can bring about a dramatic decrease in the loss of total pressure. Synthetic jet has also a very good adaptability to off-design conditions. It can therefore be concluded that the incidence sensitivity of compressor cascade can be effectively reduced by synthetic jet. The effectiveness of flow separation control in two-dimensional high load cascade by synthetic jet is investigated through numerical simulation of the effect of excitation frequency and amplitude together with the adaptability of synthetic jet to off-design conditions. Test results indicate that synthetic jet can be used to effectively control the large-scale two-dimensional flow separation in compressor cascade. Preferable results can be obtained when ex- citation frequency is close to or times of the characteristic frequency of original flow field. Excitation amplitude has a more important effect on the effectiveness of flow separation control, and the increase in excitation ampli- tude can bring about a dramatic decrease in the loss of total pressure. Synthetic jet has also a very good adaptabil- ity to off-design conditions. It can therefore be concluded that the incidence sensitivity of compressor cascade can be effectively reduced by synthetic jet.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第5期441-446,共6页 热科学学报(英文版)
关键词 合成射流 压气机叶栅 分离控制 叶栅流动 数值模拟 高负荷 二维 激发频率 synthetic jet, excitation frequency, excitation amplitude, off-design conditions, numerical simulation
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  • 1侯安平,姜正礼,凌代军,周盛.亚音压气机平面叶栅内流动的声激励试验研究[J].北京航空航天大学学报,2005,31(1):56-59. 被引量:6
  • 2罗振兵,夏智勋.合成射流技术及其在流动控制中应用的进展[J].力学进展,2005,35(2):221-234. 被引量:105
  • 3Kral L D.Numerical Simulation of Synthetic Jet Actuators.AIAA 97-1824
  • 4Guo D.Vectoring Control of a Primary Jet with Synthetic Jets.AIAA 2001-0738
  • 5Chen F J.Development of Synthetic Jet Actuators for Active Flow Control at NASA Langley.AIAA2000-2405
  • 6Smith B L.The Formation and Evolution of Synthetic Jets.Phys.Fluids,1998,10(9):2281-2298
  • 7Jose L.Gilarranze.PIV Measurement and Modeling of Synthetic Jet Actuators for Flow Control.FEDSM98-5087
  • 8Seifert A,Bachar T.Oscillatory blowing:a tool to delay boundary-layer separation[J].AIAA J,1993,31 (11):2052-2060.
  • 9Israel D M,Fasel H F.Investigate of separation control in compressible boundary layers using periodic disturbances[R].AIAA-99-3657,1999.
  • 10Wu J Z,Lu X Y,Denny A G,et al.Post-stall flow control on an airfoil by local unsteady forcing[J].J Fluid Mech,1998,371:21-58.

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