| Citation: | NAN Xiang-jun, ZHANG Meng-zheng. Self-start characteristics test of 2-D hypersonic inlet[J]. Journal of Aerospace Power, 2016, 31(10): 2479-2484. doi: 10.13224/j.cnki.jasp.2016.10.022
|
| [1] |
Kantrowitz A,Coleman P D.Preliminary investigation of supersonic diffusers[R].NACA ACR No.L5D20,1945.
|
| [2] |
孙波,张堃元.Busemann进气道起动问题初步研究[J].推进技术,2006,27(2):128-131. SUN Bo,ZHANG Kunyuan.Preliminary investigation on Busemann inlet starting characteristics[J].Journal of Propulsion Technology,2006,27(2):128-131.(in Chinese)
|
| [3] |
Matthews A J,Jones T V.Design and test of a modular waverider hypersonic intake[R].AIAA-2005-3379,2005.
|
| [4] |
Matthews A J,Jones T V,Cain T M.Design and test of a hypersonic isentropic-spike intake with aligned cowl[J].Journal of Propulsion and Power,2005,21(5):838-843.
|
| [5] |
Barber T J,Hiett D,Fastenberg S.CFD modeling of the hypersonic inlet starting problem[R].AIAA-2006-123,2006.
|
| [6] |
Jacobsen L S,Tam C J,Behdadnia R.Starting and operation of a streamline-traced Busemann inlet at Mach 4[R].AIAA-2006-4508,2006.
|
| [7] |
Van Wie D M,Kwork F T,Walsh R F.Starting characteristics of supersonic inlets[R].AIAA 96-2914,1996.
|
| [8] |
Smart M K.Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition[J].Journal of Propulsion and Power,2001,17(2):276-283.
|
| [9] |
Mölder S,Timofeev E V,Tahir R B.Flow starting in high compression hypersonic air inlets by mass spillage[R].AIAA-2004-4130,2004.
|
| [10] |
潘瑾,张堃元.可变内收缩比侧压式进气道自起动性能[J].推进技术,2007,28(3):278-281. PAN Jin,ZHANG Kunyuan.Self-starting characteristics for side wall compression inlet with variable internal contraction ratio[J].Journal of Propulsion Technology,2007,28(3):278-281.(in Chinese)
|
| [11] |
王翼.高超声速进气道启动问题研究[D].长沙:国防科学技术大学,2008. WANG Yi.Investigation on the starting characteristics of hypersonic inlet[D].Changsha:National University of Defense Technology,2008.(in Chinese)
|
| [12] |
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)
|
| [13] |
金志光,张堃元.宽马赫数范围高超声速进气道伸缩唇口式变几何方案[J].宇航学报,2010,31(5):1503-1510. JIN Zhiguang,ZHANG Kunyuan.A variable geometry scramjet inlet with a translating cowl operating in a large Mach number range[J].Journal of Astronautics,2010,31(5):1503-1510.(in Chinese)
|
| [14] |
赵一龙,范晓樯,王翼,等.抽吸对高超侧压进气道自起动性能的影响[J].航空动力学报,2013,28(5):1101-1106. ZHAO Yilong,FAN Xiaoqiang,WANG Yi,et al.Effects of bleeding on self-starting characteristics of side-compression hypersonic inlet[J].Journal of Aerospace Power,2013,28(5):1101-1106.(in Chinese)
|
| [15] |
王建勇,谢旅荣,赵昊,等.一种改善高超声速进气道自起动能力的流场控制研究[J].航空学报,2015,36(5):1401-1410. WANG Jianyong,XIE Lürong,ZHAO Hao,et al.A flow-control conception of improving self-start performance of hypersonic inlet[J].Acta Aeronautica et Astronautica Sinica,2015,36(5):1401-1410.(in Chinese)
|
| [16] |
Hank J M,Murphy J S,Mutzman R C.The X-51A scramjet engine flight demonstration program[R].AIAA-2008-2540,2008.
|
| [17] |
Smart M K,Trexler C A.Mach 4 performance of a fixed-geometry hypersonic inlet with rectangular-to-elliptical shape transition[J].Journal of Propulsion and Power,2004,20(2):288-293.
|
| [18] |
Fujimoto A,Niwa N.Experimental and numerical investigation of Mach 2.5 supersonic mixed compression inlet[R].AlAA 93-0289,1993.
|
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