Supersonic and hypersonic quiet tunnel technology at NASA Langley
28th Joint Propulsion Conference and Exhibit ; 1992 ; Nashville , TN , U.S.A.
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
NASA Langley Mach 6 Quiet Wind-Tunnel Performance
| AIAA | 1997
Design of Mach 2.4 Quiet Nozzles for the NASA Langley Supersonic Low-Disturbance Pilot Tunnel
| British Library Conference Proceedings | 1994
The NASA-Langley 20-inch supersonic wind tunnel
| AIAA | 1986