3Emami,Trexler A,Auslender H,Weidner P.Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4[R].NASA-TP-3502
4Wind-Tunnel Blockage and Actuation Systems Test of a Two-Dimensional Scramjet Inlet Unstart Model at Mach 6[R].NASA-TM-109152
5Van Wie D M,Kwok F T,and Walsh R F.Starting Characteristics of Supersonic Inlets[R].AIAA-96-2914,1996
6Sannu MAolder,Evgeny V.Timofeevy and Roabi B.Tahir,Flow starting in high compression hypersonic air inlets by mass spillage[J].AIAA 2004-4130
7Tahir R B and molder S.Unsteady starting of high Mach number air inlets-A CFD study[J].AIAA 2003-5191
8Ge-Cheng Zha,Doyle.Knight and Donald Smith.Numerical investigation of HSCT inlet unstart transient at angle of attack[J].AIAA-98-3583
9Kantrowitz A and Donaldson C.Preliminary Investigation of Supersonic Differs[R],NACA WRL-713,1945
10Curran E T and Murthy S N B.Scramjet Propulsion[M].Published by the AIAA Volumen 189:462-465
