Super/Hypersonic Variable Intake System
Inha Jet Propulsion Laboratory(IJPL)
Department of Aerospace Engineering, Inha Univ.
Scramjet Mode : Mach 4~7
Mode Transition : Mach 4
Turbo-ramjet Mode : Mach 0~4
Experiment Results : Mach 2
Experiment Results : Mach 7
