| Citation: | YOU Jin, XIA Zhi-xun, FANG Chuan-bo, HU Jian-xin, LIU Bing. Influence of single square pulse injection on restart characteristics for mixed-compression inlet[J]. Journal of Aerospace Power, 2011, 26(10): 2181-2187.
|
| [1] |
Satoru T,Brett J C,Akira F,et al.Inlet unstart influence on aerodynamics characteristics of next generation supersonic transport(SST) .AIAA-98-5546,1998.
|
| [2] |
Tahir R B,Sannu M,Timofeev E V.Unsteady starting of high mach number air inlets-a CFD study .AIAA 2003-5191,2003.
|
| [3] |
Wagner J L,Valdivia A,Yuceil K B,et al.An experimental investigation of supersonic inlet unstart .AIAA 2007-4352,2007.
|
| [4] |
Maru Y,Tanatsugu N,Sato T,et al.Multi-row disk arrangement concept for spike of axisymmetric air inlet .AIAA 2004-3407,2004.
|
| [5] |
Najafiyazdi A,Tahir R,Timofeev E V.Analytical and numerical study of flow starting in supersonic inlets by mass spillage .AIAA 2007-5072,2007.
|
| [6] |
潘瑾,张堃元.移动唇口变收缩比侧压式进气道反压特性和自起动性能[J].航空动力学报,2009,24(1):104-109. PAN Jin,ZHANG Kunyuan.Study on back pressure abd self-starting characteristics for sidewall-compression inlet with variable internal contraction ratio by moving cowl[J].Journal of Aerospace Power,2009,24(1):104-109.(in Chinese)
|
| [7] |
Schulte D,Henckels A,Wepler U.Reduction of shock induced boundary layer separation in hypersonic inlets using bleed [J].Aerospace Science and Technology,1998,2(4):231-139.
|
| [8] |
Haberle J,Gulhan A.Investigation of the performance of a scramjet inlet at Mach 6 with boundary layer bleed .AIAA 2006-8139,2006.
|
| [9] |
张华军,梁德旺.某组合发动机进气道抽吸作用分析[J].南京航空航天大学学报,2006,38(5):577-582. ZHANG Huajun,LIANG Dewang.Analysis of suction roles for supersonic inlet on combined engine[J].Journal of Nanjing University of Aeronautics and Astronautics,2006,38(5):577-582.(in Chinese)
|
| [10] |
李宇飞,何国强,刘佩进.一种辅助高超音速进气道起动方法研究[J].固体火箭技术,2007,30(5):392-395. LI Yufei,HE Guoqiang,LIU Peijin.Investigation on one aid hypersonic inlet starting method[J].Journal of Solid Rocket Technology,2007,30(5):392-395.(in Chinese)
|
| [11] |
Van W D,Kwok F T,Walsh R F.Starting characteristics of supersonic inlets .AIAA 96-2914,1996.
|
| [12] |
方传波,夏智勋,胡建新,等.基于主动射流控制的二元混压式进气道起动特性研究[J].固体火箭技术,2010,33(3):280-284. FANG Chuanbo,XIA Zhixun,HU Jianxin,et al.Study on starting characteristics of a two-dimensional supersonic inlet based on active injection control[J].Journal of Solid Rocket Technology,2010,33(3):280-284.(in Chinese)
|
| [13] |
Simon T,Philippe D,Sebastien D.Experimental study of supersonic inlet buzz[J].AIAA Journal,2006,44(10): 2354-2365.
|
| [14] |
Ferri A,Nucci L M,Louis M.The origin of aerodynamic instability of supersonic inlets at subcritical conditions .Langley Field,VA,U.S.:NACA RM-L50K30,1951.
|
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