| Citation: | CHANG Jun-tao, YU Da-ren, BAO Wen. Characteristic analysis of unstart/restart of hypersonic inlets caused by variations of attack angle of freestream[J]. Journal of Aerospace Power, 2008, 23(5): 816-821.
|
| [1] |
Mayer D,Paynter G C.Prediction of supersonic inlet unstart caused by freestream disturbances[J].AIAA Journal,1995,33(2):266-275.
|
| [2] |
Mayer D,Paynter G C.Boundary conditions for unsteady supersonic inlet analyses[J].AIAA Journal,1994,32(6):1200-1206.
|
| [3] |
Neaves M D,McRae D S,Edwards J R.High-speed inlet unstart calculations using an implicit solution adaptive mesh algorithm[R].AIAA Paper 2001-0825,2001.
|
| [4] |
Zha G C,Knight D,Smith D.Numerical investigations of high speed civil transport inlet unstart transient at angle of attack[J].Journal of Aircraft,1998,35(6):851-856.
|
| [5] |
Zha G C,Knight D,Smith D.Numerical simulation of high speed civil transport inlet operability with angle of attack[J].AIAA Journal,1998,36(7):1223-1229.
|
| [6] |
Schmitz D M,Bissinger N C.Design and testing of fixedgeometry hypersonic intakes[R].AIAA Paper 1998-1529,1998.
|
| [7] |
Van Wie D M,Kwok F T.Starting characteristics of supersonic inlets[R].AIAA Paper 1996-2914,1996.
|
| [8] |
鲍文,常军涛,郭新刚,等.超燃冲压发动机进气道不起动、仿真研究[J].航空动力学报,2005,20(5):731-735.BAO Wen,CHANG Juntao,GUO Xingang,et al.Unstart simulation of scramjet inlets[J].Jouranl of Aerospace Power,2005,20(5):731-735.
|
| [9] |
鲍文,郭新刚,常军涛,等.基于粗糙集的高超声速进气道不起动判断方法研究[J].宇航学报,2006,27:136-140.BAO Wen,GUO Xingang,CHANG Juntao,et al.Research on judgment criterion of hypersonic inlet unstart based on rough set[J].Journal of Astronautics,2006,27:136-140.
|
| [10] |
YU Daren,CHANG Juntao,BAO Wen,et al.Optimal classifications criterions of hypersonic inlet start/unstart[J].Journal of Propulsion and Power,2007,23(2):310-316.
|
| [11] |
袁化成,梁德旺.高超声速侧压式模型进气道不起动特性分析[J].南京航空航天大学学报,2004,36(6):683-687.YUAN Huacheng,LIANG Dewang.Characteristic analysis of unstart performance for hypersonic side-wall inlet model[J].Journal of Nanjing University of Aeronautics & Astronautics,2004,36(6):683-687.
|
| [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.
|
| [13] |
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.
|
| [14] |
Carlos G R.Computational fluid dynamics analysis of the central institute of aviation motors/NASA scramjet[J].Journal of Propulsion and Power,2003,19(4):547-555.
|
DownLoad: