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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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