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US Army Aeromechanics Laboratory
Return
|
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
20 x 20 |
0 - 215 knots |
0 - 2.3 | |
5 x 8 |
0 - 150 knots (5x8) |
| |
9 x 9 |
0 - 200 knots |
|
Return
Lockheed Martin
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
30 x 26 (#1) |
14 -146 ft/sec (#1) |
0 - 1 | |
8 X 12 |
8 x 12 |
0 - 293 ft/sec |
0 - 1.7 |
IWT |
4 x 2.5 |
88 - 308 ft/sec |
0 - 2 |
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Allied Aerospace Industries - Micro Craft
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
8 x 12 |
0 - 0.37 |
0 - 2.5 |
Return
Northrop Grumman
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
2.5 x 3.5 |
Max Q = 60 psf |
1.7 | |
7 x 10 |
Mach = 0 to 0.36 |
1.8 |
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United Technologies
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
8' Octogonal x 16' long |
Mach = 0 to 0.90 |
4.5 | |
Acoustic Research Tunnel |
5' Diameter |
Up to Mach = 0.65 |
4.6 |
4 x 6 x 8 |
Mach = 0.12 |
0.90 |
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University Facilities
Georgia Institute of Technology
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
7 x 9 |
0 - 0.22 |
0 - 1.6 | |
3.5 x 3.5 |
73 ft/sec |
0.5 |
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Massachusetts Institute of Technology
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
7.5 x 10 |
Up to 0.36 |
Up to 2.25 |
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University of Maryland
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
7.75 x 11.04 |
0.0 - 0.3 |
N/A |
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Old Dominion University
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
30 x 60 |
38 - 132 ft/sec |
1 |
Return
Texas A&M University
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
7 x 10 |
0 - 0.25 |
0 - 1.9 |
Return
Virginia Polytechnic Institute
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
6 x 6 |
0 - 275 ft/sec |
1.5 |
Return
University of Washington
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
8 x 12 |
0 - 302 ft/sec |
0 - 1.8 |
Return
Wichita State University
Wind Tunnel |
Test Section (ft) |
|
Reynolds No. |
7 x 10 |
0 - 264 ft/sec |
0 - 1.5 |
Return
International Installations
Belgium
Von Karman Institute for Fluid Dynamics
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
rectangular test section with 0.1 m x 0.3 m cross section and 1.6 m length |
0 - 65 m/s |
| |
10 cm x 8 cm |
0 - 90 m/s |
| |
3 m diameter |
2 to 60 m/s |
| |
octagonal test section of 0.28 m width and 1.3 m length |
0 - 45 m/s |
| |
0.16 m x 0.16 m cross section |
0 - 20 m/s |
| |
0.36 m x 0.27 m |
0 - 15 m/s |
|
Return
Canada
National Research Council, Institute for Aerospace Research
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
9.1m x 9.1m x 22.9m |
0 to 55 m/s |
| |
1.9m x 2.7m x 5.2m |
140 m/s |
| |
5m dia open jet |
28 m/s |
| |
57cm x 57cm x 183cm |
5 to 100 m/s |
| |
0.9m x 0.9m x 2.3m |
0.3 to 40 m/s |
|
Return
France
Onera
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
4.5 x 3.5 x 11 |
0.05 - 0.36 |
8x106 | |
1.8 x 1.4 x 5 |
0 - 105 m/sec |
1.1x106 |
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Germany / Netherlands
DNW - German-Dutch Wind Tunnels
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
3 x 2.5 |
0 - 0.23 |
1.4 | |
3.25 x 2.8 |
0 - 0.26 |
1.8 | |
6 x 6 |
0 - 152 m/s |
6 | |
2.4 m x 2.4 m |
|||
0.6 x 0.6 closed |
Return
India
Indian Institute of Science
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
Open Circuit LSWT |
9 x 14 ft |
upto 55 m/s |
3 |
National Aerospace Laboratories
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
Low speed wind tunnel |
1.5 x 1.5 m |
upto 60 m/s |
3 |
Indian Institute of Technology Kanpur
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
3 x 2.25 m |
upto 80 m/s |
6 |
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Russia
Central Aerohydrodynamic Institute TsAGI
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
24 x 14 x 24 elliptical |
5 - 55 m/sec |
up to 3.3 | |
4 x 2.33 elliptical |
5 - 55 m/sec |
up to 3.3 | |
2.33 x 4 elliptical |
5 - 110 m/sec |
up to 7 | |
7 round |
15 - 125 m/sec |
up to 8 | |
1.2 round |
10 - 65 m/sec |
up to 4 |
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Institute of Theoretical and Applied Mechanics
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
1 x 1 |
0.03 - 0.3 |
3 |
Sweden
FOI - Swedish Defence Research Agency
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
3.6 dia |
0 - 80 m/s |
|
Return
United Kingdom - Great Britain
Flow Science - Goldstein Research Laboratory
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
0.5 m x 0.5 m square cross section by 3.0 m long |
42 m/s |
| |
1.35 m x 0.95 m cross section with corner fillets by 2.0 m long |
50m/s |
| |
2.75 m x 2.23 m octagonal cross section by 5.5 m long |
70 m/s |
| |
4.57 m x 1.52 m rectangular cross section by 9.14 m long |
20 m/s |
|
Imperial College
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
3 x 1.5 |
up to 35 m/sec |
| |
1.37 x 1.22 |
|
| |
0.9 x 0.9 |
|
| |
2 x 0.6 |
|
|
Return
DERA
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
5m dia |
|
| |
13ft x 9ft |
|
| |
|
up to 45 m/s |
| |
4ft x 3ft |
up to 30 m/s |
|
Return
University of Glasgow
Wind Tunnel |
Test Section (m) |
|
Reynolds No. |
2.65 x 2.04 |
0 to 76 m/s |
| |
2.13 x 1.61 |
0 to 60 m/s |
| |
1.15 x 0.95 |
0 to 30 m/s |
| |
0.9 x 0.9 |
0 to 5 m/s |
|
Return
Wind Tunnel Test Section (ft) Reynolds No. 80 x 120 0 to 100 kts 0 - 1.2 40 x 80 x 80 0 - 3 11.3 x 11.3 x 28 Wind Tunnel Test Section (ft) Reynolds No. 14.5 x 21.75 x 50 0 to 0.3 0 to 2.1 12 foot Low Speed Tunnel 12 ft x 15 ft 0 to 77 ft/sec 0 to 0.5 7.5 x 3 x 7.5 0.05 - 0.5 0.4 - 15. 20 dia, 25 H 0 to 85 ft/sec 0.0 to 0.15 Wind Tunnel Test Section (ft) Reynolds No. 9 x 15 0 - 0.2 0 - 1.4 6 x 9 0 - 0.5 3.3 Wind Tunnel Facility Test Section Reynolds No. 10 x 7 0.20 - 0.50 12 x 15 0 - 150 ft/sec 0 - 0.91 Wind Tunnel Facility Test Section Reynolds No. 8 x 10 20 - 275 ft/sec 1.75 Wind Tunnel Facility Test Section Reynolds No. Army Aeromechanics 7 x 10 0 - 0.33 0 - 2.1 Wind Tunnel Test Section (ft) Reynolds No. 20 x 20 0 - 215 knots 0 - 2.3 5 x 8 0 - 150 knots (5x8) 9 x 9 0 - 200 knots Wind Tunnel Test Section (ft) Reynolds No. 30 x 26 (#1) 14 -146 ft/sec (#1) 0 - 1 8 X 12 8 x 12 0 - 293 ft/sec 0 - 1.7 IWT 4 x 2.5 88 - 308 ft/sec 0 - 2 Wind Tunnel Test Section (ft) Reynolds No. 8 x 12 0 - 0.37 0 - 2.5 Wind Tunnel Test Section (ft) Reynolds No. 2.5 x 3.5 Max Q = 60 psf 1.7 7 x 10 Mach = 0 to 0.36 1.8 Wind Tunnel Test Section (ft) Reynolds No. 8' Octogonal x 16' long Mach = 0 to 0.90 4.5 Acoustic Research Tunnel 5' Diameter Up to Mach = 0.65 4.6 4 x 6 x 8 Mach = 0.12 0.90 Wind Tunnel Test Section (ft) Reynolds No. 7 x 9 0 - 0.22 0 - 1.6 3.5 x 3.5 73 ft/sec 0.5 Wind Tunnel Test Section (ft) Reynolds No. 7.5 x 10 Up to 0.36 Up to 2.25 Wind Tunnel Test Section (ft) Reynolds No. 7.75 x 11.04 0.0 - 0.3 N/A Wind Tunnel Test Section (ft) Reynolds No. 30 x 60 38 - 132 ft/sec 1 Wind Tunnel Test Section (ft) Reynolds No. 7 x 10 0 - 0.25 0 - 1.9 Wind Tunnel Test Section (ft) Reynolds No. 6 x 6 0 - 275 ft/sec 1.5 Wind Tunnel Test Section (ft) Reynolds No. 8 x 12 0 - 302 ft/sec 0 - 1.8 Wind Tunnel Test Section (ft) Reynolds No. 7 x 10 0 - 264 ft/sec 0 - 1.5 Wind Tunnel Test Section (m) Reynolds No. rectangular test section with 0.1 m x 0.3 m cross section and 1.6 m length 0 - 65 m/s 10 cm x 8 cm 0 - 90 m/s 3 m diameter 2 to 60 m/s octagonal test section of 0.28 m width and 1.3 m length 0 - 45 m/s 0.16 m x 0.16 m cross section 0 - 20 m/s 0.36 m x 0.27 m 0 - 15 m/s Wind Tunnel Test Section (m) Reynolds No. 9.1m x 9.1m x 22.9m 0 to 55 m/s 1.9m x 2.7m x 5.2m 140 m/s 5m dia open jet 28 m/s 57cm x 57cm x 183cm 5 to 100 m/s 0.9m x 0.9m x 2.3m 0.3 to 40 m/s Wind Tunnel Test Section (m) Reynolds No. 4.5 x 3.5 x 11 0.05 - 0.36 8x106 1.8 x 1.4 x 5 0 - 105 m/sec 1.1x106 Wind Tunnel Test Section (m) Reynolds No. 3 x 2.5 0 - 0.23 1.4 3.25 x 2.8 0 - 0.26 1.8 6 x 6 0 - 152 m/s 6 2.4 m x 2.4 m 0.6 x 0.6 closed Wind Tunnel Test Section (m) Reynolds No. Open Circuit LSWT 9 x 14 ft upto 55 m/s 3 Wind Tunnel Test Section (m) Reynolds No. Low speed wind tunnel 1.5 x 1.5 m upto 60 m/s 3 Wind Tunnel Test Section (m) Reynolds No. 3 x 2.25 m upto 80 m/s 6 Wind Tunnel Test Section (m) Reynolds No. 24 x 14 x 24 elliptical 5 - 55 m/sec up to 3.3 4 x 2.33 elliptical 5 - 55 m/sec up to 3.3 2.33 x 4 elliptical 5 - 110 m/sec up to 7 7 round 15 - 125 m/sec up to 8 1.2 round 10 - 65 m/sec up to 4 Wind Tunnel Test Section (m) Reynolds No. 1 x 1 0.03 - 0.3 3 Wind Tunnel Test Section (m) Reynolds No. 3.6 dia 0 - 80 m/s Wind Tunnel Test Section (m) Reynolds No. 0.5 m x 0.5 m square cross section by 3.0 m long 42 m/s 1.35 m x 0.95 m cross section with corner fillets by 2.0 m long 50m/s 2.75 m x 2.23 m octagonal cross section by 5.5 m long 70 m/s 4.57 m x 1.52 m rectangular cross section by 9.14 m long 20 m/s Wind Tunnel Test Section (m) Reynolds No. 3 x 1.5 up to 35 m/sec 1.37 x 1.22 0.9 x 0.9 2 x 0.6 Wind Tunnel Test Section (m) Reynolds No. 5m dia 13ft x 9ft up to 45 m/s 4ft x 3ft up to 30 m/s Wind Tunnel Test Section (m) Reynolds No. 2.65 x 2.04 0 to 76 m/s 2.13 x 1.61 0 to 60 m/s 1.15 x 0.95 0 to 30 m/s 0.9 x 0.9 0 to 5 m/s
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)
Return
(Mach No.)
(per ft x 106)
Return
(Mach No.)
(per ft x 106)
Return
US Air Force Research Laboratories
(ft)
(Mach No.)
(per ft x 106)
Return
Naval
(ft)
(Mach No.)
(per ft x 106)
Return
US Army Aeromechanics Laboratory
(ft)
(Mach No.)
(per ft x 106)
Laboratory
(NASA
Return
The Boeing Company
(Mach No.)
(per ft x 106)
0 - 100 knots (open-jet)
4 x 6 (w/inserts)
0 - 250 knots (4x6)
Return
Lockheed Martin
(Mach No.)
(per ft x 106)
16 x 23 (#2)
29 - 293 ft/sec (#2)
0 - 2
Return
Allied Aerospace Industries - Micro Craft
(Mach No.)
(per ft x 106)
Return
Northrop Grumman
(Mach No.)
(per ft x 106)
Return
United Technologies
(Mach No.)
(per ft x 106)
10 x 15 x 31
18' Octogonal x 40' long
Mach = 0 to 0.45
Mach = 0 to 0.26
2.6
1.6
50" Diameter x 8' long
Up to Mach = 0.35
4.6
Return
University Facilities
Georgia Institute of Technology
(Mach No.)
(per ft x 106)
Return
Massachusetts Institute of Technology
(Mach No.)
(per ft x 106)
Elliptical
@ 0.25 bar
@ 1.5 barReturn
(Mach No.)
(per ft x 106)
Return
(Mach No.)
(per ft x 106)
Return
(Mach No.)
(per ft x 106)
Return
Virginia Polytechnic Institute
(Mach No.)
(per ft x 106)
Return
(Mach No.)
(per ft x 106)
Return
(Mach No.)
(per ft x 106)
Return
International Installations
Von Karman Institute for Fluid Dynamics
(Mach No.)
Return
National Research Council, Institute for Aerospace Research
(Mach No.)
3m x 3m square open jet
2m x 3m open jet or solid wall
Return
Onera
(Mach No.)
Return
DNW - German-Dutch Wind Tunnels
(Mach No.)
(x106)
(0 - 0.22 open)
8 x 6
9.5 x 9.5
0 - 116 m/s
0 - 62 m/s
5.3
3.9
0.6 x 0.4 closed
0.6 x 0.4 open
Return
Indian Institute of Science
(Mach No.)
(x106/m)
National Aerospace Laboratories
(Mach No.)
(x106/m)
Indian Institute of Technology
(Mach No.)
(x106/m)
Return
Central Aerohydrodynamic Institute TsAGI
(Mach No.)
(per m x 106)
Return
Institute of Theoretical and Applied Mechanics
(Mach No.)
(per m x 106)
FOI - Swedish Defence Research Agency
(Mach No.)
(per meter)
Return
Flow Science - Goldstein Research Laboratory
(Mach No.)
(per meter)
(Mach No.)
(per meter)
Return
DERA
(Mach No.)
(per meter)
Return
(Mach No.)
(per meter)
Return