| Citation: | WEN Yu-fen, YAN Jia-min, CHEN Hao, MA You-lin. Investigation on the performance of a supersonic inlet with diversing flow control on the exit[J]. Journal of Aerospace Power, 2016, 31(9): 2132-2139. doi: 10.13224/j.cnki.jasp.2016.09.011
|
| [1] |
谢旅荣,郭荣伟.一种受总体限制的弹用S弯进气道的设计和试验验证[J].航空动力学报,2006,24(1):95-101. XIE Lürong,GUO Rongwei.Design and experimental study of an S-shaped inlet restricted by missile[J].Journal of Aerospace Power,2006,24(1):95-101.(in Chinese)
|
| [2] |
钟易成,陈晓,王伟.不同进气道状态对矩形大S弯扩压器流动特性的影响[J].推进技术,1996,17(6):43-48. ZHONG Yicheng,CHEN Xiao,WANG Wei.The influence of incoming flow conditions on flow characteristics in a large S-bend rectangular diffuser[J].Journal of Propulsion Technology,1996,17(6):43-48.(in Chinese)
|
| [3] |
翁小侪,郭荣伟.一种腹下S弯进气道低速大攻角下气动特性实验[J].航空动力学报,2008,23(9):1573-1578. WENG Xiaochai,GUO Rongwei.Investigation of pneumatic characteristics for a ventral S-shape inlet at high incidence and low speed[J].Journal of Aerospace Power,2008,23(9):1573-1578.(in Chinese)
|
| [4] |
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[J].空气动力学报,1996,14(2):141-147. GUO Rongwei,LIANG Dewang,CHEN Yizhong.Investigation on swirl control in a diffusing S-shaped inlet with a horizontal guiding fence[J].Acta Aerodynamica Sinica,1996,14(2):141-147.(in Chinese)
|
| [5] |
梁德旺,郭荣伟,宁向荣,等.S弯扩压器内旋流的自动抑制[J].南京航空航天大学学报,1996,28(6):750-754. LIANG Dewang,GUO Rongwei,NING Xiangrong,et al.Auto-reduction of swirl in a S-shaped diffuser[J].Journal of Nanjing University of Aeronautics and Astronautics,1996,28(6):750-754.(in Chinese)
|
| [6] |
翁培奋.S弯进气道旋流的转动叶片模拟技术[J].空气动力学报,1997,15(4):519-523. WENG Peifen.Swirlin flow simulator in a S-shaped diffuser by a rotating blade[J].Acta Aerodynamica Sinica,1997,15(4):519-523.(in Chinese)
|
| [7] |
Reichert B A,Wendt B J.Improving diffusing S-duct performance by secondary flow control[R].AIAA 94-0365,1994.
|
| [8] |
Anderson B H,Keller D J.A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers[R].NASA/TM-2001-211278,2002.
|
| [9] |
Anderson B H,Keller D J.Robust parameter design methodologies for optimal micro-scale secondary flow control in compact inlet diffusers[R].NASA/TM-2002-211477,2002.
|
| [10] |
Anderson B H,Keller D J.Optimal micro-scale secondary flow control for the management of high cycle fatigue and distortion compact inlet diffusers[R].NASA/TM-2002-211686,2002.
|
| [11] |
Anderson B H,Miller D N,Addeington G A,et al.Optimal micro-jet flow control for compact air vehicle inlets[R].NASA/TM-2004-212937,2004.
|
| [12] |
梁德旺,郭荣伟,赵明桂.格栅对进气道的气动性能和电磁散射特性的影响[J].航空学报,1998,19(5):567-569. LIANG Dewang,GUO Rongwei,ZHAO Minggui.Effect of honeycomb on aerodynamic performance and radar cross section of inlet[J].Acta Aeronautica et Astronautica Sinica,1998,19(5):567-569.(in Chinese)
|
| [13] |
Sullerey R K,Pradeep A M.Secondary flow control using vortex generator jets[J].Journal of Fluids Engineering,2004,126(4):650-657.
|
| [14] |
Pradeep A M,Sullerey R K.Secondary flow control in a circular S-duct diffuser using vortex generator jets[R].Portland,Oregon:2nd AIAA Flow Conference,2004.
|
| [15] |
翁培奋,郭荣伟.S弯进气道旋流缩涡实验研究[J].航空动力学报,1994,9(3):310-312. WENG Peifen,GUO Rongwei.Experimental investigation on swirl control in an S-shaped diffuser by vortex reduced device[J].Journal of Aerospace Power,1994,9(3):310-312.(in Chinese)
|
| [16] |
SUN Shu,GUO Rongwei.Serpentine inlet performance enhancement using vortex generator based flow control[J].Chinese Journal of Aeronautics,2006,19(1):10-17.
|
| [17] |
赵振山,董军,郭承鹏.基于数值涡流发生器双S型进气道被动流动控制装置参数优化[J].空气动力学报,2011,29(1):22-26. ZHAO Zhenshan,DONG Jun,GUO Chengpeng.Parameters optimization of passive flow control device for a dual S inlet by numerical vortex generator model[J].Acta Aerodynamica Sinica,2011,29(1):22-26.(in Chinese)
|
| [18] |
李斌斌,程克明,顾蕴松.斜出口合成射流激励器S进气道分离流动控制[J].实验流体力学,2012,26(2):34-37. LI Binbin,CHENG Keming,GU Yunsong.Separation flow control of beveled synthetic jet actuator in S-shaped inlet[J].Journal of Experiments in Fluid Mechanics,2012,26(2):34-37.(in Chinese)
|
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