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斜出口合成射流激励器S进气道分离流动控制 被引量:10

Separation flow control of beveled synthetic jet actuator in S-shaped inlet
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摘要 设计加工了单膜双腔式斜出口合成射流激励器,应用PSI DTC Initium压力扫描系统对斜出口合成射流激励器在S进气道主动流动控制中的应用进行了研究。结果表明:斜出口合成射流激励器能够抑制S进气道分离流动,提高出口总压恢复系数σ和降低畸变指数DC90,只需通过改变激励器的工作电压和频率,就可实现对S进气道内部流场的控制。在共振频率下,当来流速度V=80m/s,采用斜出口合成射流控制可使出口截面平均总压恢复系数增加0.37%,此时所耗合成射流能量仅为主流的0.24%。 Design and process a type of beveled synthetic jet actuator with single membrane and dual chambers,and its application in the S-shaped inlet active flow control has been studied by using PSI DTC initium pressure scanning system.The results show that beveled synthetic jet actuator can suppress flow separation in S-shaped inlet,improve the total pressure recovery coefficient σ and reduce the pressure distortion DC90.Only by changing the actuator operating voltage and frequency,the flow control can be achieved within the S inlet.At the resonance frequency of synthetic jet actuator and the stream velocity V=80m/s,using beveled synthetic jet actuator can increase the total pressure recovery coefficient by 0.37%,when the energy consumption of synthetic jet is only 0.24% of the main stream.
出处 《实验流体力学》 EI CAS CSCD 北大核心 2012年第2期34-37,共4页 Journal of Experiments in Fluid Mechanics
关键词 斜出口合成射流激励器 S进气道 边界层分离 流场测量 流动控制 beveled synthetic jet actuator S-shaped inlet boundary layer separation flow field measurement flow control
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参考文献16

  • 1FULGHUM D A.Stealth engine advances revealed in JSF designs[J].Aviation Week&Space Technology,2001(19):90-93.
  • 2GRIDLEY M C,WALKER S H.Inlet and nozzle tech-nology for 21st century fighter aircraft[J].ASME96-GT-244,1996.
  • 3HAMED A,NUMBERS K.Inlet distortion considera-tions for high cycle fatigue in gas turbine engine[R].AIAA 1997-3364.
  • 4陈文,杨应凯.关于未来战斗机/发动机一体化技术的探讨[J].国际航空,2002(8):63-65. 被引量:1
  • 5HUNTER L G,HAWKINS J E.F-16variable geome-try inlet design and performance[R].AIAA1981-1394.
  • 6ALLAN B G,OWENS L R,LIN J C.Optimal designof passive flow control for a boundary layer ingestingoffset inlet using design of experiments[R].AIAA2006-1049.
  • 7TOURNIER S E,PADUANO J D,PAGAN D.Flowcontrol in a transonic inlet[R].AIAA 2006-3883.
  • 8郭荣伟,梁德旺,陈贻忠.进口导流叶片对S弯进气道出口旋流的抑制研究[J].空气动力学学报,1996,14(2):141-147. 被引量:8
  • 9李大伟,马东立.背负式S形进气道流场控制技术[J].北京航空航天大学学报,2008,34(12):1456-1459. 被引量:12
  • 10PRADEEP A M,SULLEREY R K.Secondary flow con-trol in a circular s-duct diffuser using vortex generatorjets[R].AIAA 2004-2615.

二级参考文献21

  • 1李大伟,张云飞,马东立.背负式S形进气道设计及数值分析[J].推进技术,2006,27(1):61-65. 被引量:11
  • 2郭荣伟,梁德旺,陈贻忠.进口导流叶片对S弯进气道出口旋流的抑制研究[J].空气动力学学报,1996,14(2):141-147. 被引量:8
  • 3Owens L R, Allan B G, Gorton S A. Boundary-layer-ingesting inlet flow control[ R]. AIAA-2006-839, 2006
  • 4Anderson B H, Keller D. A robust design methodology for opti- mal micro-scale secondary flow control in compact inlet diffusers [R]. AIAA-2002-0541,2002
  • 5Allan B G, Yao C S, Lin J C. Numerical simulations of vortex generator vanes and jets on a fiat plate[R]. AIAA-2002-3160, 2006
  • 6Reichert B A, Wendt B J. Improving diffusing S-duct performance by secondary flow control[ R ]. AIAA-94-0365,1994
  • 7Anderson B H, Gibb J. Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [ R ]. AIAA-92-3177,1992
  • 8郭荣伟,The Aeronautical Quarterly,1993年,5卷
  • 9翁培奋,AIAA J,1992年,30卷,7期
  • 10林麒,航空学报,1989年,10卷,1期

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