| Citation: | TENG Jian, YUAN Hua-cheng. Research on aerodynamic characteristics of 2-D hypersonic inlet[J]. Journal of Aerospace Power, 2013, 28(4): 775-782. |
| [1] |
Seddon J, GoldSmith E L.Intake aerodynamics[M].2nd ed.Oxford:Blackwell Science Ltd.,1999.
|
| [2] |
Blockley R,Shyy W.Encyclopedia of aerospace engineering:Volume 2 propulsion and power[M].New York:John Wiley & Sons,Ltd.,2011.
|
| [3] |
Davis M.The standard handbook for aeronautical and astronautical engineers[M].London: McGraw-Hill Standard Handbooks,2003.
|
| [4] |
Falempin F,Scherrer D,Laruelle G,et al.French hypersonic propulsion program PREPHA:results,lessons and perspectives [R].AIAA-98-1565,1998.
|
| [5] |
Falempin F,Serre L.LEA flight test program-status in 2004 [R].AIAA-2004-3344,2004.
|
| [6] |
Kojima T,Tanatsugu N,Sato T,et al.Development study on axisymmetric air inlet for ATREX engine [R].AIAA-2001-1895,2001.
|
| [7] |
袁化成,滕健,郭荣伟.内收缩比可控的二元高超声速变几何进气道研究[J].航空动力学报,2012,27(11):2468-2474. YUAN Huacheng,TENG Jian,GUO Rongwei.Research on variable geometry technology of 2-D hypersonic inlet with contract ratio controlled[J].Journal of Aerospace Power,2012,27(11):2468-2474.(in Chinese)
|
| [8] |
袁化成,郭荣伟.矩形截面高超声速进气道高焓风洞实验[J].航空动力学报,2010,25(12):2748-2755. YUAN Huacheng, GUO Rongwei.High enthalpy wind tunnel tests of hypersonic inlets with rectangular section[J].Journal of Aerospace Power,2010,25(12):2748-2755.(in Chinese)
|
| [9] |
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)
|
| [10] |
Herrmann C D,Koschel W W.Experimental investigation of the internal compression of a hypersonic intake [R].AIAA-2002-4130,2002.
|
| [11] |
Mrozinski D P,Hayes J R.Numerical and experimental analysis of a hypersonic variable geometry inlet [R].AIAA-99-0899,1999.
|
| [12] |
Okai K,Taguchi H,Kojima T.Futamura numerical analysis of variable intake and nozzle for hypersonic engine [R].AIAA-2003-7069,2003.
|
| [13] |
Van Wie D M,Kwok F T,Walsh R F.Starting characteristics of supersonic inlets [R].AIAA-96-2914,1996.
|
| [14] |
Ferlauto M,Larocca F,Zannetti L.Integrated design and analysis of intakes and nozzles in air-breathing engines[J].Journal of Propulsion and Power,2002,18(1):28-34.
|
| [15] |
Smart M K.How much compression should a scramjet inlet do[J].AIAA Journal,2012,50(3):610-619.
|