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US Army Aeromechanics Laboratory
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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20 x 20 |
0 - 215 knots |
0 - 2.3 | |
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5 x 8 |
0 - 150 knots (5x8) |
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9 x 9 |
0 - 200 knots |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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30 x 26 (#1) |
14 -146 ft/sec (#1) |
0 - 1 | |
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8 X 12 |
8 x 12 |
0 - 293 ft/sec |
0 - 1.7 |
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IWT |
4 x 2.5 |
88 - 308 ft/sec |
0 - 2 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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8 x 12 |
0 - 0.37 |
0 - 2.5 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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2.5 x 3.5 |
Max Q = 60 psf |
1.7 | |
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7 x 10 |
Mach = 0 to 0.36 |
1.8 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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8' Octogonal x 16' long |
Mach = 0 to 0.90 |
4.5 | |
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Acoustic Research Tunnel |
5' Diameter |
Up to Mach = 0.65 |
4.6 |
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4 x 6 x 8 |
Mach = 0.12 |
0.90 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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7 x 9 |
0 - 0.22 |
0 - 1.6 | |
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3.5 x 3.5 |
73 ft/sec |
0.5 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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7.5 x 10 |
Up to 0.36 |
Up to 2.25 |
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Wind Tunnel |
Test Section (ft) |
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Reynolds No. |
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7.75 x 11.04 |
0.0 - 0.3 |
N/A |
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Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
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30 x 60 |
38 - 132 ft/sec |
1 |
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Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
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7 x 10 |
0 - 0.25 |
0 - 1.9 |
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Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
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6 x 6 |
0 - 275 ft/sec |
1.5 |
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Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
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8 x 12 |
0 - 302 ft/sec |
0 - 1.8 |
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Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
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7 x 10 |
0 - 264 ft/sec |
0 - 1.5 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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rectangular test section with 0.1 m x 0.3 m cross section and 1.6 m length |
0 - 65 m/s |
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10 cm x 8 cm |
0 - 90 m/s |
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3 m diameter |
2 to 60 m/s |
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octagonal test section of 0.28 m width and 1.3 m length |
0 - 45 m/s |
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0.16 m x 0.16 m cross section |
0 - 20 m/s |
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0.36 m x 0.27 m |
0 - 15 m/s |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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9.1m x 9.1m x 22.9m |
0 to 55 m/s |
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1.9m x 2.7m x 5.2m |
140 m/s |
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5m dia open jet |
28 m/s |
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57cm x 57cm x 183cm |
5 to 100 m/s |
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0.9m x 0.9m x 2.3m |
0.3 to 40 m/s |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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4.5 x 3.5 x 11 |
0.05 - 0.36 |
8x106 | |
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1.8 x 1.4 x 5 |
0 - 105 m/sec |
1.1x106 |
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Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
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3 x 2.5 |
0 - 0.23 |
1.4 | |
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3.25 x 2.8 |
0 - 0.26 |
1.8 | |
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6 x 6 |
0 - 152 m/s |
6 | |
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2.4 m x 2.4 m |
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0.6 x 0.6 closed |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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Open Circuit LSWT |
9 x 14 ft |
upto 55 m/s |
3 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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Low speed wind tunnel |
1.5 x 1.5 m |
upto 60 m/s |
3 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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3 x 2.25 m |
upto 80 m/s |
6 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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24 x 14 x 24 elliptical |
5 - 55 m/sec |
up to 3.3 | |
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4 x 2.33 elliptical |
5 - 55 m/sec |
up to 3.3 | |
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2.33 x 4 elliptical |
5 - 110 m/sec |
up to 7 | |
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7 round |
15 - 125 m/sec |
up to 8 | |
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1.2 round |
10 - 65 m/sec |
up to 4 |
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Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
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1 x 1 |
0.03 - 0.3 |
3 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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3.6 dia |
0 - 80 m/s |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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0.5 m x 0.5 m square cross section by 3.0 m long |
42 m/s |
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1.35 m x 0.95 m cross section with corner fillets by 2.0 m long |
50m/s |
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2.75 m x 2.23 m octagonal cross section by 5.5 m long |
70 m/s |
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4.57 m x 1.52 m rectangular cross section by 9.14 m long |
20 m/s |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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3 x 1.5 |
up to 35 m/sec |
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1.37 x 1.22 |
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0.9 x 0.9 |
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2 x 0.6 |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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5m dia |
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13ft x 9ft |
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up to 45 m/s |
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4ft x 3ft |
up to 30 m/s |
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Wind Tunnel |
Test Section (m) |
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Reynolds No. |
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2.65 x 2.04 |
0 to 76 m/s |
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2.13 x 1.61 |
0 to 60 m/s |
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1.15 x 0.95 |
0 to 30 m/s |
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0.9 x 0.9 |
0 to 5 m/s |
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Wind Tunnel Test Section (ft) Reynolds No. 80 x 120 0 to 100 kts 0 - 1.2 40 x 80 x 80 0 - 3
Subsonic Wind Tunnels
National Aeronautics & Space Administration
NASA Ames Research Center
NASA Langley Research Center
NASA Glenn Research Center
United States Department of Defense
US Air Force Research Laboratories
US Army Aeromechanics Laboratory
Naval Surface Warfare Center, Carderock Division
U. S. Aerospace Industry
The Boeing Company
Lockheed Martin Corporation
Allied Aerospace Industries - MicroCraft
Northrop Grumman Corporation
United Technologies
Georgia Institute of Technology
Massachusetts Institute of Technology
University of Maryland
Old Dominion University
Texas A&M University
University of Washington
Virginia Polytechnic Institute
Wichita State University
International Installations
Canada
Belgium
France
Germany
India
Russia
Sweden
United Kingdom
National Aeronautics & Space Administration
(Mach No.)
(per ft x 106)