| Citation: | XIE LÜ-rong, GUO Rong-wei. Investigation of the restart performance of a mixed-compression two-dimensional supersonic inlet with fixed-geometry[J]. Journal of Aerospace Power, 2008, 23(2): 389-395.
|
| [1] |
Seddon J,G ol dsmit h E L.Int ake aerodynam ics[M].London:Blackw ell Science,1999.
|
| [2] |
Van D M,K wok F T,W al sh R F.S tart ing charact erist ics of s upersonic inlet s[R].A IA A 96 2914,1996.
|
| [3] |
Takas ak e S,Brett J C,Fujimot o A,et al.Inlet un st art in fluence on aerodyn ami c charact erist ics of nex t gen erati on s uper sonic t ran sport(SST)[R].A IA A 98-5546,1998.
|
| [4] |
Norm an D W,Warren E A.Ex perim ent al invest igat ional of a larges cale,two dim ens ional,mixed com pres sion inlet s yst em perform ance at super sonic condit ion,M=1.55 to 32[R].N ASA TND 6392,1971.
|
| [5] |
Glenn A M,Robert W C.A n experim ent al invest igat ion of the rest art area rat io of a Mach 30 axisymm et ric mixed com pres sion inlet[R].N A SA TMX 1547,1968.
|
| [6] |
Gary L C,G eorge H N,M ichael J C.An automatic rest artcontrol system for an axi symmet ric mixed com pression inlet[R].N A S A T N D 5590,1969.
|
| [7] |
Bobby W S,Robert W C.Eff ect of bleed syst em back pressure and porous area on the per for mance of an axi symmetric mixed compression inl et at Mach 2 5[R].N A S A TMX 1710,1968.
|
| [8] |
Michael K F,Warren G H,Eli R.Cont rol of shock w ave boundary layer interact ions by bleed in s upersonic mixedcom pression inlet s[R].N A S A CR 2595.1975.
|
| [9] |
Sato T,K aji S.St udy on st eady and unst eady uns tart phenomenadue to com pound chokin g and/or flu ct uation s in com bust or of scramj et engines[R].A IA A 92 5102,1992.
|
| [10] |
H aw kins W R,M arquart E J.Tw o dimen sional generi c in let uns tart det ect ion at M ach 25-50[R].A IA A 95 6019,1995.
|
| [11] |
J osep h F W,Edw ard T M,Paul L B.Experiment al inves tigati on of t h e performance of a Mach 2 7 t w o di mens ional bi fur cat ed du ct inl et with 30 percent in ternal cont ract ion [R].N A SA TM 106728,1996.
|
| [12] |
H errmann C D,K oschel K W.Experimen tal in vest igat ion of the in ternal compr ess ion of a h ypers on ic int ake[R].A IA A 2002 4130,2002.
|
| [13] |
K an t row it z A,Donaldson C.Prel iminary in vest igati on of super sonic diff ers[R].N A C A W RL 713,1945.
|
| [14] |
Rudolf H.Sup ersoni c inlet dif fus ers an d int roduct ion to int ernal aerodynam ics[R].M inneapoli s:M inneapoli cs H oneyw ell R egult or Company,1953.
|
| [15] |
谢旅荣,郭荣伟.定几何混压式轴对称超声速进气道气动特性数值仿真和实验验证[J].航空学报,2007,28(1):78-83.X IE L rong,GUO R on gw ei.N umerical simul at ion and experiment al validat ion of the flow in a m ixed compr ess ionaxisym metric super sonic inlet with f ixed geom et ry[J].Act a A eronau ticaet A stronaut ica S inica,2007,28(1):78-83.
|
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