Pressure Fluctuation Measurements in the NASA Langley 20-Inch Mach 6 Wind Tunnel
42nd AIAA Fluid Dynamics Conference and Exhibit
2012-01-01
Conference paper
Electronic Resource
English
PRESSURE FLUCTUATION MEASUREMENTS IN THE NASA LANGLEY 20-INCH MACH 6 WIND TUNNEL
British Library Conference Proceedings | 2012
|The NASA-Langley 20-inch supersonic wind tunnel
AIAA | 1986
|NASA Langley Mach 6 Quiet Wind-Tunnel Performance
AIAA | 1997
|NASA Langley Mach 6 Qulet Wind-Tunnel Performance
Online Contents | 1997
|