| Citation: | WANG De-peng, TIAN Fang-chao, ZHANG Qi-fan, TAN Hui-jun, BU Huan-xian, LI Guang-sheng. Effect of entry shape on starting characteristics of inward turning inlets[J]. Journal of Aerospace Power, 2015, 30(6): 1400-1406. doi: 10.13224/j.cnki.jasp.2015.06.015 |
| [1] |
Heiser W H,Pratt D T.Hypersonic airbreathing propulsion[M]. Washington DC:AIAA Education Series,1994.
|
| [2] |
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.
|
| [3] |
Bulman M J,Siebenhaar A.The rebirth of round hypersonic propulsion[R].AIAA-2006-5035,2006.
|
| [4] |
Barkmeyer D,Starkey R M L.Inverse waverider design for inward turning inlets[R].AIAA-2005-3915, 2005.
|
| [5] |
Smart M K,Trexler C A.Mach 4 performance of hypersonic inlet with rectangular-to-elliptical shape transition[J]. Journal of Propulsion and Power,2004,20(2):288-293.
|
| [6] |
Ungewitter R J,Ott J D,Dash S M.Advanced modeling methods for hypersonic scramjet evaluation[R].AIAA-2006-4578,2006.
|
| [7] |
Matthews A J,Jones T V.Design and test of a modular waverider hypersonic intake[R].AIAA-2005-2279,2005.
|
| [8] |
Tam C J,Baurle R A.Inviscid CFD analysis of streamline traced hypersonic inlets at off-design conditions[R].AIAA-2001-0675,2001.
|
| [9] |
Smart M K,White J A.Computational investigation of the performance and back-pressure limits of a hypersonic inlet[R].AIAA-2002-0508,2002.
|
| [10] |
Van Wie D M,Kwok F T,Walsh R F.Starting characteristics of supersonic inlets[R].AIAA 96-2914,1996.
|
| [11] |
McClinton C R,Hunt J L.Airbreathing hypersonic technology vision vehicles and development dreams[R].AIAA 99-4987,1999.
|
| [12] |
Tan H J,Guo R W.Experimental study of the unstable-unstarted condition of a hypersonic inlet at Mach 6[J].Journal of Propulsion and Power,2007,23(4):783-788.
|
| [13] |
Malo F J,Gaitonde D V.Numerical investigation of an innovative inward turning inlet[R].AIAA-2005-4871,2005.
|
| [14] |
Malo F J,Gaitonde D V.Analysis of an innovative inward turning inlet using an air-JP8 combustion mixture at Mach 7[R].AIAA-2006-3041,2006.
|
| [15] |
Billig F S,Tam C J,Baurle R A,et al.Design and analysis of streamline traced hypersonic inlets[R].AIAA 99-4974,1999.
|
| [16] |
Smart M K.Design of three-dimensional hypersonic inlets with rectangular to elliptical shape transition[J].Journal of Propulsion and Power,1999,15(3):408-416.
|
| [17] |
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)
|
| [18] |
Jacobsen L S,Tam C J,Robert B F.Starting and operation of a streamline-traced busemann inlet at Mach 4[R].AIAA-2006-4508,2006.
|