Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K
MINUCCI, M. A. S., NAGAMATSU, H. T.
Journal of Propulsion and Power ; 9 , 1 ; 139-145
1993-01-01
7 pages
Article (Journal)
Electronic Resource
English
INLET UNSTART OF AN ETHYLENE-FUELED MODEL SCRAMJET WITH A MACH 4.5 FREESTREAM FLOW
British Library Conference Proceedings | 2012
|Effect of Freestream Noise on Roughness-Induced Boundary-Layer Transition for a Scramjet Inlet
British Library Conference Proceedings | 2000
|