| Citation: | YUAN Hua-cheng, GUO Rong-wei. High enthalpy wind tunnel tests of hypersonic inlets with rectangular section[J]. Journal of Aerospace Power, 2010, 25(12): 2748-2755. |
| [1] |
Heiser W H,Pratt D T,Daley D H,et al.Hypersonic airbreathing propulsion[M].Washington,DC:American Institute of Aeronautics and Astronautics,Inc.,1994.
|
| [2] |
Berry S A,Auslender A H,Dilley A D,et al.Hypersonic boundary-layer trip development for Hyper-X .AIAA 2000-4012,2000.
|
| [3] |
Berry S A,Nowak R J,Horvath T J.Boundary layer control for hypersonic airbreathing vehicles .AIAA 2004-2246,2004.
|
| [4] |
Emami S,Trexler C A,Auslender A H,et al.Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 .NASA TP 3502,1995.
|
| [5] |
Bissinger N C,Schmitz D M.Design and wind tunnel testing of intakes for hypersonic vehicles .AIAA 93-5042,1993.
|
| [6] |
Van Wie D M,Kwok F T,Walsh R F.Starting characteristics of supersonic inlets .AIAA 96-2914,1996.
|
| [7] |
Reubush D E,Nguyen L T,Rausch V L.Review of X-43A return to flight activities and current status .AIAA-2003-7085,2003.
|
| [8] |
Huebner L,Rock K,Witte D,et al.Hyper-X engine testing in the NASA Langley 8-foot high temperature tunnel .AIAA-2000-3605,2000.
|
| [9] |
袁化成,梁德旺.高超声速进气道再起动特性分析[J].推进技术,2006,27(5):390-393. YUAN Huacheng,LIANG Dewang.Analysis of characteristics of restart performance for a hypersonic inlet[J].Journal of Propulsion Technology,2006,27(5):390-393.(in Chinese)
|
| [10] |
梁德旺,袁化成,张晓嘉.影响高超声速进气道起动能力的因素分析[J].宇航学报,2006,27(4):714-719. LIANG Dewang,YUAN Huacheng,ZHANG Xiaojia.Research on the effects of start ability of hypersonic inlet[J].Journal of Astronautics,2006,27(4):714-719.(in Chinese)
|
| [11] |
黄伟,罗世彬,王振国.隔离段对二维混压式进气道出口参数的影响[J].火箭推进,2007,33(4):8-11. HUANG Wei,LUO Shibin,WANG Zhenguo.Effects of the isolator on the exit parameters of two-dimensional inlet[J].Journal of Rocket Propulsion,2007,33(4):8-11.(in Chinese)
|
| [12] |
王成鹏,张红英,孙姝,等.高超飞行器进气道/内流道流动特性试验[J].航空动力学报,2007,22(10):1704-1709. WANG Chengpeng,ZHANG Hongying,SUN Shu,et al.Experimental study of flow characteristics of inlet/internal flowpath for a hypersonic flight vehicle[J].Journal of Aerospace Power,2007,22(10):1704-1709.(in Chinese)
|
| [13] |
袁化成,郭荣伟.矩形截面高超声速进气道气动设计及实验验证[J].南京航空航天大学学报,2009,41(4):423-428. YUAN Huacheng,GUO Rongwei.Design and experimental verification of hypersonic inlet with rectangular section[J].Journal of Nanjing University of Aeronautics and Astronautics,2009,41(4):423-428.(in Chinese)
|
| [14] |
谢旅荣,郭荣伟.一种高超声速二元混压式进气道的研究[J].航空学报,2009,30(12):2288-2294. XIE Lürong,GUO Rongwei.Investigation of a two-dimensional mixed-compression hypersonic inlet[J].Acta Aeronautica et Astronautica Sinica,2009,30(12):2288-2294.(in Chinese)
|