Test description and preliminary pitot-pressure surveys for Langley Test Technique Demonstrator at Mach 6
28th Joint Propulsion Conference and Exhibit ; 1992 ; Nashville , TN , U.S.A.
1992-01-01
Conference paper
Electronic Resource
English
Hypersonic Aerodynamic Characteristics For Langley Test Technique Demonstrator
British Library Conference Proceedings | 1993
|Langley Mach 4 Scramjet Test Facility
NTIS | 1985
|Langley Mach 4 Scramjet Test Facility
NTRS | 1985
|