| Citation: | WENG Xiao-chai, GUO Rong-wei. Study of novel flow control concept for fix-geometry two-dimensional mix-compression supersonic inlet[J]. Journal of Aerospace Power, 2012, 27(11): 2492-2498.
|
| [1] |
谢旅荣,郭荣伟.双下侧定几何二元混压式超声速进气道的风洞试验[J].航空学报,2009,30(6):1000-1006. XIE Lürong,GUO Rongwei.Experimental investigati on of fixed-geometry two-dimensional mixed-compression supersonic inlet with twin-inlet 90o configuration at venter[J].Acta Aeronautica et Astronautica Sinica,2009,30(6):1000-1005.(in Chinese)
|
| [2] |
谭慧俊,陈智,李光胜.基于激波形状控制的定几何高超声速可调进气道概念及初步验证[J].中国科学:E辑 技术科学,2007,37(11):1469-1479. TAN Huijun,CHEN Zhi,LI Guangsheng.The concept and preliminary experiment of the adjustable inlet with fix-geometry hypersonic based on cont rolling shock[J].Science in China:Press E Technological Sciences,2007,37(11):1469-1479.(in Chinese)
|
| [3] |
Leissler L A,Nettles J C.Investigation to Mach number 2.0 of shock-position control system for a variable-geometry inlet in combination with AJ34 turbojet engine [R].NACA RME54127,1954.
|
| [4] |
Watanabe Y,Miyagi H,Sekido T.Conceptual design study on combine-cycle engine for hypersonic transport.ISABE 93-7018,1993.
|
| [5] |
Takayuki K,Nobuhiro T,Tetsuya S,et al.Development study on axisymmetric air inlet for ATREX engine [R].AIAA-2001-1895,2001.
|
| [6] |
Yusuke M.Multi-row disk arrangement concept for spike of axisymmetric air inlet [R].AIAA-2004-3407,2004.
|
| [7] |
Kobayashi H,Tanatsugu N,Sato T.Experimental study of multi-row disk inlets for hypersonic air breathing propulsion [R].AIAA-2004-861,2004.
|
| [8] |
Falempin F.Lea flight test programe:a mandatory step in the European R&T effort for hypersonic air breathing propulsion [R].ISABE 2005-1089,2005.
|
| [9] |
Fraishtadt V L,Kuranov A L,Sheikin E G.Use of MHD systems in hypersonic aircraft[J].Technical Physics,1998,43(11):1309-1313.
|
| [10] |
Sheikin E G,Kuranov A L.MHD control in hypersonic aircraft [R].AIAA-2005-1335,2005.
|
| [11] |
Sheikin E G,Kuranov A L.MHD controlled inlet for scramjet with various configurations of magnetic field [R].AIAA-2004-1195,2004.
|
| [12] |
Shneider M N,Macheret S O,Miles R B.Nonequilibrium magnetohydrodynamic control of scramjet inlet [R].AIAA-2002-2251,2002.
|
| [13] |
Richard G H,Jeff S N,Russell L D.Computational investigation of a method to compress air fluidically in supersonic inlets[J].Spacecraft Rockets,2001,38(1):51-59.
|
| [14] |
谢旅荣.双下侧定几何二元混压超声速进气道气动设计及实验研究 [D].南京:南京航空航天大学,2007. XIE Lürong.Design and investigation of fixed-geometry two-dimensional mixed-compression supersonic inlet with twin-inlet 90° configuration at venter of the missile [D].Nanjing:Nanjing University of Aeronautics and Astronautics,2006.(in Chinese)
|
| [15] |
谢旅荣,郭荣伟.双下侧定几何二元混压式进气道的流场特征和气动性能分析[J].空气动力学学报,2011,3(29):257-263. XIE Lürong,GUO Rongwei.Flow pattern and performance of fix-geometry two-dimensional mixed-compression supersonic inlets with 90o configuration at venter of the missile[J].Acta Aerodynamic Sinica,2011,29(3):257-263.(in Chinese)
|
DownLoad: