The Worthey Connection

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

U.S. Universities

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

National Research Council, Institute for Aerospace Research

Belgium

Von Karman Institute for Fluid Dynamics

France

Onera

Germany

DNW German-Dutch Wind Tunnels

India

Indian Institute of Science

National Aerospace Laboratories

Indian Institute of Technology Kanpur

 

Russia

Central Aerohydrodynamic Institute TsAGI

Institute of Theoretical and Applied Mechanics

Sweden

FOI - Swedish Defence Research Agency

 

United Kingdom

Flow Science - Goldstein Research Laboratory

Imperial College

DERA

University of Glasgow

 

National Aeronautics & Space Administration

NASA Ames Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

80 X 120 ft

80 x 120

0 to 100 kts

0 - 1.2

40 X 80 ft

40 x 80 x 80

0 to 300 kts

0 - 3

12 ft Pressure Tunnel

11.3 x 11.3 x 28

0.05 - 0.55

0.1 - 12

Return

NASA Langley Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

14 X 22 Foot Subsonic Tunnel

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

Low-Turbulence Pressure Tunnel (LTPT)

7.5 x 3 x 7.5

0.05 - 0.5

0.4 - 15.

20-foot Vertical Spin Tunnel

20 dia, 25 H

0 to 85 ft/sec

0.0 to 0.15

Return

NASA Glenn Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

9 X 15 ft

9 x 15

0 - 0.2

0 - 1.4

Icing Research Tunnel
(IRT)

6 x 9

0 - 0.5

3.3

Return

U.S. Department of Defense

US Air Force Research Laboratories

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

SARL

10 x 7

0.20 - 0.50

 

Vertical Wind Tunnel

12 x 15

0 - 150 ft/sec

0 - 0.91

Return

Naval Surface Warfare Center, Carderock Division

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Subsonic

8 x 10

20 - 275 ft/sec

1.75

Return

US Army Aeromechanics Laboratory

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Army Aeromechanics
Laboratory

(NASA Ames)

7 x 10

0 - 0.33

0 - 2.1

Return

U.S. Industry

The Boeing Company

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

20 X 20

20 x 20

0 - 215 knots
0 - 100 knots (open-jet)

0 - 2.3

BRAIT

5 x 8
4 x 6 (w/inserts)

0 - 150 knots (5x8)
0 - 250 knots (4x6)

 

9 x 9 Subsonic Propulsion Tunnel

9 x 9

0 - 200 knots

 

Return

Lockheed Martin

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

LSWT # 1 & 2

30 x 26 (#1)
16 x 23 (#2)

14 -146 ft/sec (#1)
29 - 293 ft/sec (#2)

0 - 1
0 - 2

8 X 12

8 x 12

0 - 293 ft/sec

0 - 1.7

IWT

4 x 2.5

88 - 308 ft/sec

0 - 2

Return

Allied Aerospace Industries - Micro Craft

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

LSWT

8 x 12

0 - 0.37

0 - 2.5

Return

Northrop Grumman

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Research

2.5 x 3.5

Max Q = 60 psf

1.7

7 X 10

7 x 10

Mach = 0 to 0.36

1.8

Return

United Technologies

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Large Subsonic WT

8' Octogonal x 16' long
10 x 15 x 31
18' Octogonal x 40' long

Mach = 0 to 0.90
Mach = 0 to 0.45
Mach = 0 to 0.26

4.5
2.6
1.6

Acoustic Research Tunnel

5' Diameter
50" Diameter x 8' long

Up to Mach = 0.65
Up to Mach = 0.35

4.6
4.6

Pilot Wind Tunnel

4 x 6 x 8

Mach = 0.12

0.90

Return

 

University Facilities

Georgia Institute of Technology

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

7 X 9 ft

7 x 9

0 - 0.22

0 - 1.6

Low Turbulence

3.5 x 3.5

73 ft/sec

0.5

Return

Massachusetts Institute of Technology

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Wright Brothers

7.5 x 10
Elliptical

Up to 0.36
@ 0.25 bar

Up to 2.25
@ 1.5 bar

Return

University of Maryland

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Glenn L. Martin

7.75 x 11.04

0.0 - 0.3

N/A

Return

Old Dominion University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Langley Full Scale Tunnel

30 x 60

38 - 132 ft/sec

1

Return

Texas A&M University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

7 X 10 ft

7 x 10

0 - 0.25

0 - 1.9

Return

Virginia Polytechnic Institute

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Stability Wind Tunnel

6 x 6

0 - 275 ft/sec

1.5

Return

University of Washington

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Kirsten Wind Tunnel

8 x 12

0 - 302 ft/sec

0 - 1.8

Return

Wichita State University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Beech Wind Tunnel

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)

Speed Range
(Mach No.)

Reynolds No.

Cold wind tunnel CWT-1

rectangular test section with 0.1 m x 0.3 m cross section and 1.6 m length

0 - 65 m/s

 

Cryogenic wind tunnel T'3

10 cm x 8 cm

0 - 90 m/s

 

L-1A

3 m diameter

2 to 60 m/s

 

L-2A

octagonal test section of 0.28 m width and 1.3 m length

0 - 45 m/s

 

L-7

0.16 m x 0.16 m cross section

0 - 20 m/s

 

L-7+

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)

Speed Range
(Mach No.)

Reynolds No.

9m x 9m Low Speed Wind Tunnel

9.1m x 9.1m x 22.9m

0 to 55 m/s

 

2.3m x 3m Wind Tunnel

1.9m x 2.7m x 5.2m

140 m/s

 

5m Vertical Wind Tunnel

5m dia open jet
3m x 3m square open jet
2m x 3m open jet or solid wall

28 m/s

 

Altitude Icing Tunnel

57cm x 57cm x 183cm

5 to 100 m/s

 

0.9 m pilot wind tunnel

0.9m x 0.9m x 2.3m

0.3 to 40 m/s

 

Return

France

Onera

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.

F1

4.5 x 3.5 x 11

0.05 - 0.36

8x106

F2

1.8 x 1.4 x 5

0 - 105 m/sec

1.1x106

Return

 

Germany / Netherlands

DNW - German-Dutch Wind Tunnels

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106)

LST
Low Speed Tunnel

3 x 2.5

0 - 0.23

1.4

NWB

3.25 x 2.8

0 - 0.26
(0 - 0.22 open)

1.8

LLF
Large Low Speed Facility

6 x 6
8 x 6
9.5 x 9.5

0 - 152 m/s
0 - 116 m/s
0 - 62 m/s

6
5.3
3.9

Cryogenic wind tunnel Cologne (KKK)

2.4 m x 2.4 m

up to 0.38

9.5

HDG
High Pressure Wind Tunnel

0.6 x 0.6 closed
0.6 x 0.4 closed
0.6 x 0.4 open

2 - 35 m/s

12

Return

India

Indian Institute of Science

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

Open Circuit LSWT

9 x 14 ft

upto 55 m/s

3

National Aerospace Laboratories

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

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)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

National Wind Tunnel Facility

3 x 2.25 m

upto 80 m/s

6

Return
Russia

Central Aerohydrodynamic Institute TsAGI

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per m x 106)

T 101

24 x 14 x 24  elliptical

5 - 55 m/sec

up to 3.3

T 102

4 x 2.33  elliptical

5 - 55 m/sec

up to 3.3

T 103

2.33 x 4  elliptical

5 - 110 m/sec

up to 7

T 104

7   round

15 - 125 m/sec

up to 8

T 30

1.2  round

10 - 65 m/sec

up to 4

Return

Institute of Theoretical and Applied Mechanics

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per m x 106)

T-324 (CC)

1 x 1

0.03 - 0.3

3

Return

 

Sweden

FOI - Swedish Defence Research Agency

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

LT1

3.6 dia

0 - 80 m/s

 

Return

United Kingdom - Great Britain

Flow Science - Goldstein Research Laboratory

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

0.5m x 0.5m Low Turbulence Tunnel

0.5 m x 0.5 m square cross section by 3.0 m long

42 m/s

 

1.35m x 0.95m Blow Down Tunnel

1.35 m x 0.95 m cross section with corner fillets by 2.0 m long

50m/s

 

Avro' 2.7m x 2.2m (9' x 7') Low Speed Closed Return Tunnel

2.75 m x 2.23 m octagonal cross section by 5.5 m long

70 m/s

 

4.5m x 1.5m (15' x 5') Environmental Wind Tunnel

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)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

10 x 5 Honda Wind Tunnel

3 x 1.5

up to 35 m/sec

 

Donald Campbell General Purpose Low Speed Wind Tunnel

1.37 x 1.22

 

 

Low Speed Wind-Tunnel

0.9 x 0.9

 

 

Flow Visualisation Tunnel

2 x 0.6

 

 

Return

 

DERA

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

5m Pressurized Low Speed

5m dia

 

 

13ft x 9ft Atmospheric Low Speed

13ft  x 9ft

 

 

boundary Layer Tunnel

 

up to 45 m/s

 

4ft x 3ft Low Speed Tunnel

4ft x 3ft

up to 30 m/s

 

Return

University of Glasgow

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

Argyll Wind Tunnel

2.65 x 2.04

0 to 76 m/s

 

Handly-Page Wind Tunnel

2.13 x 1.61

0 to 60 m/s

 

The 1.15 x 0.95 Low Speed Wind Tunnel

1.15 x 0.95

0 to 30 m/s

 

Flow Visualisation Wind Tunnel

0.9 x 0.9

0 to 5 m/s

 

Return

 


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

U.S. Universities

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

National Research Council, Institute for Aerospace Research

Belgium

Von Karman Institute for Fluid Dynamics

France

Onera

Germany

DNW German-Dutch Wind Tunnels

India

Indian Institute of Science

National Aerospace Laboratories

Indian Institute of Technology Kanpur

 

Russia

Central Aerohydrodynamic Institute TsAGI

Institute of Theoretical and Applied Mechanics

Sweden

FOI - Swedish Defence Research Agency

 

United Kingdom

Flow Science - Goldstein Research Laboratory

Imperial College

DERA

University of Glasgow

 

National Aeronautics & Space Administration

NASA Ames Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

80 X 120 ft

80 x 120

0 to 100 kts

0 - 1.2

40 X 80 ft

40 x 80 x 80

0 to 300 kts

0 - 3

12 ft Pressure Tunnel

11.3 x 11.3 x 28

0.05 - 0.55

0.1 - 12

Return

NASA Langley Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

14 X 22 Foot Subsonic Tunnel

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

Low-Turbulence Pressure Tunnel (LTPT)

7.5 x 3 x 7.5

0.05 - 0.5

0.4 - 15.

20-foot Vertical Spin Tunnel

20 dia, 25 H

0 to 85 ft/sec

0.0 to 0.15

Return

NASA Glenn Research Center

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

9 X 15 ft

9 x 15

0 - 0.2

0 - 1.4

Icing Research Tunnel
(IRT)

6 x 9

0 - 0.5

3.3

Return

U.S. Department of Defense

US Air Force Research Laboratories

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

SARL

10 x 7

0.20 - 0.50

 

Vertical Wind Tunnel

12 x 15

0 - 150 ft/sec

0 - 0.91

Return

Naval Surface Warfare Center, Carderock Division

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Subsonic

8 x 10

20 - 275 ft/sec

1.75

Return

US Army Aeromechanics Laboratory

Wind Tunnel Facility

Test Section
(ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Army Aeromechanics
Laboratory

(NASA Ames)

7 x 10

0 - 0.33

0 - 2.1

Return

U.S. Industry

The Boeing Company

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

20 X 20

20 x 20

0 - 215 knots
0 - 100 knots (open-jet)

0 - 2.3

BRAIT

5 x 8
4 x 6 (w/inserts)

0 - 150 knots (5x8)
0 - 250 knots (4x6)

 

9 x 9 Subsonic Propulsion Tunnel

9 x 9

0 - 200 knots

 

Return

Lockheed Martin

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

LSWT # 1 & 2

30 x 26 (#1)
16 x 23 (#2)

14 -146 ft/sec (#1)
29 - 293 ft/sec (#2)

0 - 1
0 - 2

8 X 12

8 x 12

0 - 293 ft/sec

0 - 1.7

IWT

4 x 2.5

88 - 308 ft/sec

0 - 2

Return

Allied Aerospace Industries - Micro Craft

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

LSWT

8 x 12

0 - 0.37

0 - 2.5

Return

Northrop Grumman

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Research

2.5 x 3.5

Max Q = 60 psf

1.7

7 X 10

7 x 10

Mach = 0 to 0.36

1.8

Return

United Technologies

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Large Subsonic WT

8' Octogonal x 16' long
10 x 15 x 31
18' Octogonal x 40' long

Mach = 0 to 0.90
Mach = 0 to 0.45
Mach = 0 to 0.26

4.5
2.6
1.6

Acoustic Research Tunnel

5' Diameter
50" Diameter x 8' long

Up to Mach = 0.65
Up to Mach = 0.35

4.6
4.6

Pilot Wind Tunnel

4 x 6 x 8

Mach = 0.12

0.90

Return

 

University Facilities

Georgia Institute of Technology

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

7 X 9 ft

7 x 9

0 - 0.22

0 - 1.6

Low Turbulence

3.5 x 3.5

73 ft/sec

0.5

Return

Massachusetts Institute of Technology

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Wright Brothers

7.5 x 10
Elliptical

Up to 0.36
@ 0.25 bar

Up to 2.25
@ 1.5 bar

Return

University of Maryland

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Glenn L. Martin

7.75 x 11.04

0.0 - 0.3

N/A

Return

Old Dominion University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Langley Full Scale Tunnel

30 x 60

38 - 132 ft/sec

1

Return

Texas A&M University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

7 X 10 ft

7 x 10

0 - 0.25

0 - 1.9

Return

Virginia Polytechnic Institute

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Stability Wind Tunnel

6 x 6

0 - 275 ft/sec

1.5

Return

University of Washington

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Kirsten Wind Tunnel

8 x 12

0 - 302 ft/sec

0 - 1.8

Return

Wichita State University

Wind Tunnel

Test Section (ft)

Speed Range
(Mach No.)

Reynolds No.
(per ft x 106)

Beech Wind Tunnel

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)

Speed Range
(Mach No.)

Reynolds No.

Cold wind tunnel CWT-1

rectangular test section with 0.1 m x 0.3 m cross section and 1.6 m length

0 - 65 m/s

 

Cryogenic wind tunnel T'3

10 cm x 8 cm

0 - 90 m/s

 

L-1A

3 m diameter

2 to 60 m/s

 

L-2A

octagonal test section of 0.28 m width and 1.3 m length

0 - 45 m/s

 

L-7

0.16 m x 0.16 m cross section

0 - 20 m/s

 

L-7+

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)

Speed Range
(Mach No.)

Reynolds No.

9m x 9m Low Speed Wind Tunnel

9.1m x 9.1m x 22.9m

0 to 55 m/s

 

2.3m x 3m Wind Tunnel

1.9m x 2.7m x 5.2m

140 m/s

 

5m Vertical Wind Tunnel

5m dia open jet
3m x 3m square open jet
2m x 3m open jet or solid wall

28 m/s

 

Altitude Icing Tunnel

57cm x 57cm x 183cm

5 to 100 m/s

 

0.9 m pilot wind tunnel

0.9m x 0.9m x 2.3m

0.3 to 40 m/s

 

Return

France

Onera

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.

F1

4.5 x 3.5 x 11

0.05 - 0.36

8x106

F2

1.8 x 1.4 x 5

0 - 105 m/sec

1.1x106

Return

 

Germany / Netherlands

DNW - German-Dutch Wind Tunnels

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106)

LST
Low Speed Tunnel

3 x 2.5

0 - 0.23

1.4

NWB

3.25 x 2.8

0 - 0.26
(0 - 0.22 open)

1.8

LLF
Large Low Speed Facility

6 x 6
8 x 6
9.5 x 9.5

0 - 152 m/s
0 - 116 m/s
0 - 62 m/s

6
5.3
3.9

Cryogenic wind tunnel Cologne (KKK)

2.4 m x 2.4 m

up to 0.38

9.5

HDG
High Pressure Wind Tunnel

0.6 x 0.6 closed
0.6 x 0.4 closed
0.6 x 0.4 open

2 - 35 m/s

12

Return

India

Indian Institute of Science

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

Open Circuit LSWT

9 x 14 ft

upto 55 m/s

3

National Aerospace Laboratories

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

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)

Speed Range
(Mach No.)

Reynolds No.
(x106/m)

National Wind Tunnel Facility

3 x 2.25 m

upto 80 m/s

6

Return
Russia

Central Aerohydrodynamic Institute TsAGI

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per m x 106)

T 101

24 x 14 x 24  elliptical

5 - 55 m/sec

up to 3.3

T 102

4 x 2.33  elliptical

5 - 55 m/sec

up to 3.3

T 103

2.33 x 4  elliptical

5 - 110 m/sec

up to 7

T 104

7   round

15 - 125 m/sec

up to 8

T 30

1.2  round

10 - 65 m/sec

up to 4

Return

Institute of Theoretical and Applied Mechanics

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per m x 106)

T-324 (CC)

1 x 1

0.03 - 0.3

3

Return

 

Sweden

FOI - Swedish Defence Research Agency

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

LT1

3.6 dia

0 - 80 m/s

 

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United Kingdom - Great Britain

Flow Science - Goldstein Research Laboratory

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

0.5m x 0.5m Low Turbulence Tunnel

0.5 m x 0.5 m square cross section by 3.0 m long

42 m/s

 

1.35m x 0.95m Blow Down Tunnel

1.35 m x 0.95 m cross section with corner fillets by 2.0 m long

50m/s

 

Avro' 2.7m x 2.2m (9' x 7') Low Speed Closed Return Tunnel

2.75 m x 2.23 m octagonal cross section by 5.5 m long

70 m/s

 

4.5m x 1.5m (15' x 5') Environmental Wind Tunnel

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)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

10 x 5 Honda Wind Tunnel

3 x 1.5

up to 35 m/sec

 

Donald Campbell General Purpose Low Speed Wind Tunnel

1.37 x 1.22

 

 

Low Speed Wind-Tunnel

0.9 x 0.9

 

 

Flow Visualisation Tunnel

2 x 0.6

 

 

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DERA

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

5m Pressurized Low Speed

5m dia

 

 

13ft x 9ft Atmospheric Low Speed

13ft  x 9ft

 

 

boundary Layer Tunnel

 

up to 45 m/s

 

4ft x 3ft Low Speed Tunnel

4ft x 3ft

up to 30 m/s

 

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University of Glasgow

Wind Tunnel

Test Section (m)

Speed Range
(Mach No.)

Reynolds No.
(per meter)

Argyll Wind Tunnel

2.65 x 2.04

0 to 76 m/s

 

Handly-Page Wind Tunnel

2.13 x 1.61

0 to 60 m/s

 

The 1.15 x 0.95 Low Speed Wind Tunnel

1.15 x 0.95

0 to 30 m/s

 

Flow Visualisation Wind Tunnel

0.9 x 0.9

0 to 5 m/s

 

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