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Facility Type:  Aerodynamics

Glossary for Test Techniques Acronyms

Facility Name Mach Number Reynolds Number Dimensions
h x w (x l)
Test Techniques
0.3M Transonic Cryogenic Tunnel 0.2 to 0.9 1 to 100 x 106/ft 13 in x 13 in x 69 in 2-D testing, focusing Schlieren
14 X 22 Foot Subsonic Tunnel 0 to 0.3 0 to 2.1 x 106/ft 14.5 ft x 21.75 ft x 50 ft Acoustic measurements, LVS, oil flow, free flight, forced oscillation, rotorcraft, propulsion, semi-span, smoke flow, DGV
Low Turbulence Pressure Tunnel 0.05 to 0.5 0.4 to 15 x 106/ft 7.5 ft x 3 ft x 7.5 ft Acoustics using focused microphone array, PSP, LITA
National Transonic Facility 0.1 to 1.2 4 to 146 x 106/ft 8.2 ft x 8.2 ft x 25 ft PSP/TSP, VMD, Full Span, Semi-Span
Unitary Plan Wind Tunnel 1.5 to 2.9
2.3 to 4.6
0.5 To 6 x 106
0.5 To 11 x 106/ft
4 ft x 4 ft x 7 ft
4 ft x 4 ft x 7 ft
PSP/TSP, LVS, VMD, UV oil flow, sonic boom, stage separation, dynamic stability
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NASA Official Responsible For Content: Pete Jacobs
Page Curator: Lori Rowland
Date Last Updated: 10/25/06