List of wind tunnels explained

This is an alphabetical list of wind tunnels.

Name	Status	Size (W x H x L)	Use	Country	Comments
A2 Wind Tunnel^[1]			Full scale general purpose	United States	~$500/hr full scale race car, motorcycle, bicycle
ACE Climatic Wind Tunnel^[2]			Full scale: automotive, motorsport, cycling, skiing, architectural, transit, truck, product development	Canada	Available and accessible for all industries requiring wind tunnel services or climatic services
Aerodium Sigulda^[3]	Operational		Testing, training, open to the public	Latvia	First vertical wind tunnel in Eastern Europe
AeroDyn Wind Tunnel^[4]			Full scale NASCAR racecars	United States
Aerodynamic and Propulsion Test Unit^[5]	Operational		Hypersonic	United States	Located at Arnold Air Force Base and operated by the United States Air Force
Aircraft Research Association^[6]	Operational		Transonic	United Kingdom	Transonic closed circuit, continuous flow wind tunnel. Mach number 0 - 1.4. Reynolds Number 3.5 to 16.7 million/m^[7]
Auto Research Center^[8]			Subsonic research and development including: 50% scale model automotive rolling road, wind turbine design and optimization, and cycling	United States	Wind tunnel has a moving ground plane as well as primary and secondary boundary layer suction. Subsonic testing capabilities for motorsports, production cars, commercial semi-trucking, cycling, wind turbines, architecture, aerospace, academic research, and industrial research and development.
RUAG Automotive Wind Tunnel Emmen^[9]	Operational		Low speed automotive and general purpose	Switzerland	Belt system for rolling road simulation
Boeing Icing Wind Tunnel^[10]	Operational			United States
Boeing Low-speed Aero-Acoustic Facility^[11]	Operational			United States
Boeing Polysonic (supersonic) Wind Tunnel^[12]	Operational			United States
Boeing Propulsion Wind Tunnel^[13]	Operational		Low-speed, atmospheric, non-return, induction-type facility. Typical models include engine inlets, exhaust nozzles, small engines or powered vehicles, aerodynamic half or full models, as well as thrust reversers.	United States
Boeing Subsonic (low-speed) Wind Tunnel^[14]	Operational			United States
Boeing Transonic Wind Tunnel^[15]	Operational			United States
Boundary Layer and Subsonic Wind Tunnel^[16]	Operational	Boundary Layer Test Section: Subsonic Test Section:	Boundary Layer Development / Low-Speed / Subsonic / General Purpose	United States
Building Research Establishment^[17]	Operational			United Kingdom	Two atmospheric boundary layer tunnels
Cal Poly's Low Speed Wind Tunnel^[18]			Low speed: Scale model testing, Aerospace, Automotive, IR industry	United States	Startups, major Aerospace corporations and other scientific equipment tested here. Rolling road implementation in progress.
Calspan Wind Tunnel^[19]	Operational		Subsonic / Transonic	United States	The only independently owned and operated wind tunnel in the United States.
Central Aerohydrodynamic Institute T-1		Diameter by		Russia
Central Aerohydrodynamic Institute T-2		Diameter by		Russia
Central Aerohydrodynamic Institute T-5		Diameter by		Russia
Central Aerohydrodynamic Institute T-101^[20]				Russia
Central Aerohydrodynamic Institute T-102				Russia
Central Aerohydrodynamic Institute T-103		(elliptical)		Russia
Central Aerohydrodynamic Institute T-104		Diameter		Russia
Central Aerohydrodynamic Institute T-105^[21]		Diameter by	Vertical wind tunnel	Russia
Central Aerohydrodynamic Institute T-106		Diameter by		Russia
Central Aerohydrodynamic Institute T-107		Diameter by		Russia
Central Aerohydrodynamic Institute T-109				Russia
Central Aerohydrodynamic Institute T-112				Russia
Central Aerohydrodynamic Institute T-113				Russia
Central Aerohydrodynamic Institute T-113				Russia
Central Aerohydrodynamic Institute T-116				Russia
Central Aerohydrodynamic Institute T-117				Russia
Central Aerohydrodynamic Institute T-124				Russia
Central Aerohydrodynamic Institute T-128				Russia
City, University of London Transonic Wind Tunnel^[22]	Operational	by by ; return: by by		United Kingdom	Mach 0.4 – 2.0; return max speed 12 m/s. Part of the UK National Wind Tunnel Facility
Cranfield University 8x4 Atmospheric Boundary Layer Wind Tunnel	Operational	by		United Kingdom
Cranfield University 8'x6' Low Speen Wind Tunnel^[23]	Operational	by		United Kingdom	Part of the UK National Wind Tunnel Facility
Cranfield University Weybridge Wind Tunnel	Operational	diameter jet		United Kingdom
Cranfield University Icing Tunnel^[24]	Operational	by ; octagonal; by		United Kingdom	Three test sections. Part of the UK National Wind Tunnel Facility
CRIACIV Boundary Layer Wind Tunnel - University of Florence^[25]	Operational		Building, bridges, general purpose	Italy	Closed circuit wind tunnel, T-shaped diffuser, one atmospheric test section (max speed).
Durham University 2m tunnel^[26]	Operational			United Kingdom	Subsonic; turbulence generation system; moving or fixed ground
Durham University 1m recirculating wind tunnel	Operational	by by		United Kingdom	–
Durham University – smaller tunnels	Operational			United Kingdom	Three tunnels; max speed 20 m/s
EDITH supersonic wind tunnel^[27]	Operational	Diameter by	Long shot time running (20 minutes).	France	Fundamental research on shock waves. Aerodynamic and aerothermal behaviour of probes and models. Fluidic thrust vectoring of supersonic nozzle
Energy Technology Centre	Operational	Working section by	Wind blade testing	United Kingdom
European Transonic Wind Tunnel^[28]			Transonic	Germany
Ferrari wind tunnel^[29]	Operational	wide by long		Italy
Focke's wind tunnel^[30]	Operational			Germany	Private laboratory of Henrich Focke, not discovered until 1977
Glenn L. Martin Wind Tunnel^[31]			Low speed: scale model testing, automotive, aerospace	United States
GVPM^[32]	Operational		Building, bridges, rail, aeronautical, general purpose	Italy	Vertically arranged closed circuit wind tunnel with two test sections: one atmospheric (max speed), one aeronautical (max speed) with possibility to test with open / closed jet.
Hypervelocity Wind Tunnel 9^[33]		Diameter		United States	Located at Arnold Air Force Base and operated by the United States Air Force
Imperial College London	Operational	Low speed tunnels: to		United Kingdom	Five low speed tunnels and other tunnels up to mach 9
Jules Verne climatic wind tunnel^[34] ^[35]	Operational		Automotive, Rail, Full scale general purpose	France	Three test sections with wind speeds up to
Klebanoff–Saric Wind Tunnel^[36]	Operational			United States
Large Amplitude Multi-Purpose (LAMP) Vertical Wind Tunnel Bihrle Applied Research^[37]	Operational	Diameter	Vertical, Subsonic, High AOA, Static or body-axis oscillatory	Germany	Privately owned wind tunnel. +- 180 degree AOA and +-90 degree sideslip. Diverse testing capability: static, wind body axis dynamic, Multi-body axis dynamic, simultaneous force moment and pressure data acquisition.
RUAG Large Wind Tunnel Emmen^[38]	Operational		Low speed aerospace, full scale automotive and general purpose	Switzerland
Lockheed Martin Low Speed Wind Tunnel^[39]	Operational		Aeronautics, Full Scale Automotive, V/STOL Aircraft, General Purpose	United States	Larger test section was designed for use of V/STOL aircraft but is not limited to such. Max speed of ~ in smaller test section and ~ in the larger test section.
Loughborough University Aeronautical and Automotive Engineering Low Turbulence Windtunnel	Operational			United Kingdom	AAE Large Windtunnel
Loughborough University Aeronautical and Automotive Engineering Large Windtunnel	Operational			United Kingdom
Loughborough University Automotive Wind Tunnel^[40]	Operational	by by		United Kingdom	'Rolling road' moving ground plane. Part of the UK National Wind Tunnel Facility
MARHy wind Tunnel^[41]	Operational	Diameter by	Hypersonic/supersonic rarefied wind tunnel. No limit running time. Reynolds number /cm: 26.3 < Re < 7522;Mach number: 0.8 < Mach < 20	France	Fundamental and applied research of fluid dynamic phenomena in rarefied compressible flows. Aerodynamic and aerothermal behaviour of probes and models; Plasma flow control in rarefied and super/hypersonic flows.
Modine Wind Tunnels^[42]				United States	Climatic wind tunnel testing, large truck and automotive
NASA Ames 7-by 10 Foot Wind Tunnel^[43]				United States
NASA Ames Hypersonic Propulsion Integration 16 Inch Shock		Diameter	Hypersonic propulsion	United States
NASA Ames Hypersonic Propulsion Integration Direct-Connect			Hypersonic propulsion	United States
NASA Ames National Full Scale Aerodynamic Complex^[44]			Subsonic	United States	Largest wind tunnel in the world
NASA Ames Subsonic 12 Foot High-Rn Pressure^[45]		Diameter	Subsonic	United States
NASA Ames 9-by 7-foot Supersonic Wind Tunnel^[46]			Supersonic	United States
NASA Ames 11-by 11-foot Transonic Wind Tunnel^[47]			Transonic	United States
NASA Ames Unitary Plan Wind Tunnel^[48]			Transonic/supersonic	United States
NASA Glenn 10- by 10-Foot Abe Silverstein Supersonic Wind Tunnel^[49]			Supersonic	United States
NASA Glenn 8- by 6-Foot Wind Tunnel^[50]			Transonic	United States
NASA Glenn 9- by 15-Foot Low-Speed Wind Tunnel^[51]			Subsonic	United States
NASA Glenn Aero-Acoustic Propulsion Laboratory Nozzle Acoustic Test Rig^[52]		Diameter	Acoustic testing of exhaust nozzles, subsonic	United States	Free-jet
NASA Glenn Engine Components Research Lab^[53]				United States
NASA Glenn Hypersonic Test Facility^[54]			Hypersonic	United States
NASA Glenn Icing Research Tunnel			Subsonic Icing	United States
NASA Glenn Propulsion Systems Laboratory^[55]	Active	Diameter by long	Full-Scale Engine Testing	United States	Four test cells: 1 & 2 demolished; 3 & 4 active. Cell 3 has icing capabilities
NASA Langley 14- by 22-Foot Subsonic Tunnel			Subsonic atmospheric	United States
NASA Langley 20-Foot Vertical Spin Tunnel		Diameter	Subsonic vertical spin	United States
NASA Langley Eight-Foot High Speed Tunnel^[56] -		Diameter	High speed	United States
NASA Langley Full-Scale Wind Tunnel^[57]	Demolished		Full-scale aircraft	United States	NASA's oldest operating wind tunnel until its closing in October 1995
NASA Langley High-Rn Transonic Dynamics Tunnel^[58]	Operational		Aeroelasticity, high-risk testing, active controls, rotorcraft performance and stability, transonic aerodynamics.	United States	Unique capability to manipulate fluid-structure scaling parameters with use of Heavy-Gas (R-134a) or air as a test medium and variable pressure.^[59] Good flow quality for large transonic tunnel (Mach 0–1.2)^[60]
NASA Langley Hypersonic 20 Inch Mach 6 Air^[61]		Diameter	Hypersonic	United States
NASA Langley Hypersonic 20 Inch Mach 6 Tetrafluoromethane^[62]	Demolished in 2016^[63]	Diameter	Hypersonic	United States
NASA Langley Hypersonic 31 Inch Mach 10 Air		Diameter	Hypersonic	United States
NASA Langley Hypersonic Propulsion Integration 15 Inch Mach 6 High-Temperature Tunnel^[64]		Diameter	Hypersonic	United States
NASA Langley Hypersonic Propulsion Integration 8 Foot High-Temperature Tunnel^[65]		Diameter	Hypersonic, high-temperature	United States
NASA Langley Hypersonic Propulsion Integration Arc-Heated Scramjet^[66]			Hypersonic	United States
NASA Langley Hypersonic Propulsion Integration Combustion Scramjet^[67]			Hypersonic	United States
NASA Langley Hypersonic Propulsion Integration Supersonic Combustion			Hypersonic	United States
NASA Langley NASA / GASL HYPULSE Propulsion Integration^[68]				United States
NASA Langley National Transonic Facility^[69]			Transonic	United States
NASA Langley Propeller Research Tunnel^[70]		Diameter	Full-scale aircraft used primarily in reducing drag caused by propellers and exposed engines	United States
NASA Langley Subsonic 12 Foot Atmospheric Lab^[71]		Diameter	Subsonic atmospheric	United States
NASA Langley Subsonic Low-Turbulence Pressure Tunnel^[72]			Subsonic low-turbulence	United States
NASA Langley Supersonic High-Rn			Supersonic	United States
NASA Langley Transonic 16 Foot Atmospheric^[73]			Transonic atmospheric	United States
NASA Langley Variable Density Tunnel		Diameter by long	Measuring aerodynamic qualities of airfoils	United States	World's first variable density wind tunnel
National Wind Tunnel Facility^[74]	Operational			United Kingdom	Twenty-two wind tunnels at twelve universities allowing open access
ODTÜ-RÜZGEM^[75]	Operational	High Speed Test Section: Boundary Layer Test Section: Open Jet: equivalent diameter octagonal jet	Wind energy, aeronautics, civil engineering	Turkey	High Speed Test Section: Max speed, TI<0.25% Boundary Layer Test Section: Max speed with spires and roughness elements Open Jet: Max speed Interchangeable modular test sections, 6x400 kW axial fan array, 750 kW heat exchanger
ONERA Modane S1MA wind tunnel^[76]	Operational	Diameter by	Subsonic atmospheric	France	Largest continuous blow-down wind tunnel in the world, Mach 0.05 to 1.
ONERA Modane S2MA wind tunnel^[77]	Operational		Supersonic	France	Continuous-flow wind tunnel, Variable pressure, Mach 0.1 to Mach 3.0.
PHEDRA (Arc-jet) high enthalpy wind tunnel^[78]	Operational	Diameter by	Supersonic high enthalpy rarefied wind tunnel. No limit running time . Averaged enthalpy, Mj/kg: few < Ho < 50; Mach number: 2 < Mach < 8;Working gas: N2, Air, CO2, CH4, Ar and extensive mixtures	France	Fundamental research of high enthalpy fluid dynamic phenomena in non-equilibrium flows. Aerodynamic and aerothermal behaviour of probes and models; Atmospheric entry research.
Poul la Cour Tunnel^[79]	Operational		Airfoil aerodynamics and aeroacoustics, 10 to 105 m/s, Re~7M	Denmark	Named for Poul la Cour
Propulsion Wind Tunnel Facility^[80]	Operational	Transonic: Supersonic:		United States	Part of the Arnold Engineering Development Complex located at Arnold Air Force Base and operated by the United States Air Force
Rail Tec Arsenal Climatic Wind Tunnel^[81]	Operational		Full scale: transit, locomotive, automotive, propeller and turbines, airfoils and aircraft Icing-, solar-, precipitatoin tests all subsonic	Austria	RTA operates the longest climatic wind channel in the world. Whole trains up can be tested under real world conditions from and variable climatic conditions.
R J Mitchell Wind Tunnel^[82]	Operational			United Kingdom	Largest university owned wind tunnel in the United Kingdom, named for R. J. Mitchell
RWDI Wind Tunnels^[83]	Operational		Wind engineering, scale buildings	Canada	Two wind tunnels
San Diego Wind Tunnel^[84]				United States	Major airframers, bicycle manufacturers and professional athletes
T3 Hypersonic wind tunnel^[85]				Brazil
Texas A&M Oran W. Nicks Low Speed Wind Tunnel^[86]			Scale aircraft, UAV, rocket, missile, academic research, automotive, motorsport, cycling, skiing, architectural, transit, truck, product development 0-200MPH	United States
TitanX Jamestown Vehicle Climatic Wind Tunnel^[87]			Climatic testing of vehicle systems and entire trucks	United States	Open for external clients
Trisonic Wind Tunnel^[88]				United States
Trudelturm^[89]		Height		Germany
University of Bristol	Operational	Large Low Speed Wind Tunnel by Low Turbulence Wind Tunnel by Open Jet Wind Tunnel diameter		United Kingdom
University of British Columbia Boundary Layer Wind Tunnel^[90]			Boundary layer, architectural, and wind-engineering studies	Canada	Speed range:
University of British Columbia Parkinson Wind Tunnel^[91]			Aeronautical research, studies of flow-induced oscillations, studies of wind tunnel blockage effects	Canada	Speed range:
University of Glasgow	Operational	De-Havilland Wind Tunnel by Handley-Page Wind Tunnel by Low Speed Wind Tunnel by Flow Visualisation Wind Tunnel by		United Kingdom
University of Manchester	Operational	Hypersonic wind tunnel diameter Trisonic wind tunnel by Open-circuit boundary layer tunnel by by Open-circuit wind tunnel by by Open-circuit wind tunnel by by Closed-circuit water tunnel by by Tilting flume by by		United Kingdom	Hypersonic wind tunnel: Mach 4, 5, 6; trisonic wind tunnel: Mach 0 to 0.8, 1.8
University of Southampton	Operational	3' x 2' tunnel by by 7' x 5' tunnel by R J Mitchell Wind Tunnel by		United Kingdom
University of Surrey	Operational	EnFlo Laboratory meteorological wind tunnel by by		United Kingdom
University of Washington Aeronautical Laboratory, Kirsten Wind Tunnel^[92]			Subsonic	United States
University of Washington Department of Aeronautics & Astronautics 3x3^[93]			Velocity range approx.	United States	The original "Boeing Aerodynamical Chamber", built in 1918 with an Eiffel and updated in the early 1990s with new power systems and a higher velocity EDL
Virginia Tech Stability Wind Tunnel^[94]				United States
Von Karman Gas Dynamics Facility^[95]	Operational			United States	Three tunnels at the Arnold Engineering Development Complex
Williams F1 Wind Tunnel 2^[96]	Operational		Motorsport / Automotive	United Kingdom
WindShear Full Scale, Rolling Road, Automotive Wind Tunnel^[97]			Wind shear	United States
Windtech Boundary Layer Wind Tunnel^[98]	Operational		Low-Speed / Boundary Layer Wind Tunnel	Australia	Windtech owns and operates one of the largest boundary layer wind tunnel labs in the world with a total of 3 wind tunnels under one roof. Each wind tunnel is

Notes and References

1. Web site: A2 wind tunnel. 26 January 2024.
2. Web site: ACE Climatic Wind Tunnel. 26 January 2024.
3. Web site: Fly for Real. 27 January 2024.
4. Web site: AeroDyn Wind Tunnel. 26 January 2024.
5. Web site: Aerodynamic and Propulsion Test Unit (APTU). 27 January 2024.
6. Web site: Aircraft Research Association. 26 January 2024.
7. Web site: Transonic Wind Tunnel Testing . Aircraft Research Association . www.ara.co.uk . 14 September 2019.
8. Web site: Auto Research Center Wind Tunnel. 26 January 2024.
9. Web site: Automotive Wind Tunnel Emmen (AWTE). 26 January 2024.
10. Web site: Boeing Research Aero-Icing Tunnel. 26 January 2024.
11. Web site: Low-Speed Aero acoustic Facility. 26 January 2024.
12. Web site: Polysonic Wind Tunnel. 26 January 2024.
13. Web site: Propulsion Laboratory. 26 January 2024.
14. Web site: Boeing Vertical/Short Takeoff and Landing Wind Tunnel. 26 January 2024.
15. Web site: Boeing Transonic Wind Tunnel. 26 January 2024.
16. Web site: Boundary Layer and Subsonic Wind Tunnel (BLAST) at the University of Texas at Dallas. 26 January 2024.
17. 10.15128/r1ms35t864n. Directory of UK Based Test and Demonstration Facilities for Wind Technologies. Durham University . Zappalá. Donatella. Crabtree. Christoper. Hogg. Simon. 6 November 2018. 7, 98–108.
18. Web site: Low Speed Wind Tunnel. 26 January 2024.
19. Web site: Calspan Wind Tunnel Technical Specifications. 26 January 2024.
20. Web site: Wind tunnel T-101 - Experimental base - TsAGI.
21. Web site: Wind tunnel T-105 - Experimental base - TsAGI.
22. Web site: Transonic/Supersonic. National Wind Tunnel Facility. 24 July 2024.
23. Web site: 8ft x 6ft Low Speed. National Wind Tunnel Facility. 24 July 2024.
24. Web site: Icing Tunnel. National Wind Tunnel Facility. 24 July 2024.
25. Web site: CRIACIV Boundary Layer Wind Tunnel - University of Florence. 26 January 2024.
26. Web site: Research Facilities. Department of Engineering, Durham University. 24 July 2024.
27. Web site: -EDITH- Institut de Combustion Aérothermique Réactivité et Environnement. 26 January 2024.
28. Web site: European Transonic Windtunnel Test Section. 26 January 2024.
29. Web site: Ferrari Wind Tunnel. 27 January 2024.
30. Web site: VFS Recognizes Focke's Wind Tunnel as Vertical Flight Historic Site. 27 January 2024.
31. Web site: Our Capabilities. 26 January 2024.
32. Web site: GVPM. 26 January 2024.
33. Web site: Hypervelocity Wind Tunnel 9. 27 January 2024.
34. Web site: Jules Verne Climatic Wind Tunnel. CSTB . 2 October 2017. 26 January 2024.
35. Web site: CSTB Atmospheric. 26 January 2024. CSTB . 2 October 2017.
36. Web site: Klebanoff–Saric Wind Tunnel. 27 January 2024.
37. Web site: Large Amplitude Multi-Purpose (LAMP) Wind Tunnel Facility. 26 January 2024.
38. Web site: Large Wind Tunnel Emmen (LWTE). 26 January 2024.
39. Web site: Lockheed Martin Low Speed Wind Tunnel. 26 January 2024.
40. Web site: Automotive. National Wind Tunnel Facility. 24 July 2024.
41. Web site: -MARHY- Institut de Combustion Aérothermique Réactivité et Environnement. 26 January 2024.
42. Web site: Modine Wind Tunnels. 26 January 2024.
43. Web site: A Summary of the Experimental Results for a Generic Tractor-Trailer in the Ames Research Center 7- by 10-Foot and 12-Foot Wind Tunnels. 26 January 2024.
44. Web site: National Full-Scale Aerodynamics Complex. 26 January 2024.
45. Web site: 12-Foot Low-Speed Tunnel (Building 644). 26 January 2024.
46. Book: Unitary Plan Wind Tunnel 9-by 7-foot SWT Test Section. 26 January 2024.
47. Web site: UPWT 11-by 11-foot TWT Test Section. 26 January 2024.
48. Web site: Ames Unitary Plan Wind Tunnel. 26 January 2024.
49. Web site: 10×10 Supersonic Wind Tunnel. 26 January 2024.
50. Web site: 8- by 6-Foot Supersonic Wind Tunnel Description. 26 January 2024.
51. Web site: AETC Subsonic Facilities. 26 January 2024.
52. Web site: Nozzle Acoustic Test Rig. 26 January 2024.
53. Web site: Engine Research Building. 26 January 2024.
54. Web site: NASA Glenn Hypersonic Test Facility. 26 January 2024.
55. Web site: Propulsion Systems Laboratory. 26 January 2024.
56. Web site: 8-Foot High-Speed Tunnel (Building 641)l. nasa.gov. 3 February 2016. National Aeronautics and Space Administration. 10 February 2018.
57. Web site: 30 x 60-Foot Full Scale Tunnel (Building 643)l. nasa.gov. National Aeronautics and Space Administration. 10 February 2018.
58. Web site: Transonic Dynamics Tunnel. 26 January 2024.
59. Ivanco. Thomas G.. 24 June 2013. 26 January 2024. Unique Testing Capabilities of the NASA Langley Transonic Dynamics Tunnel, an Exercise in Aeroelastic Scaling. AIAA Ground Testing Conference. Fluid Dynamics and Co-located Conferences. San Diego, CA. American Institute of Aeronautics and Astronautics. 10.2514/6.2013-2625. 2060/20140000340. free.
60. Book: A Survey of Transition Research at AEDC. Unknown. Arnold Engineering Development Center Arnold AFS TN. Whitfield. Jack D. . Dougherty, Jr . N. S.. July 1977. 832032113.
61. Web site: NASA Langley Aerothermodynamics Laboratory: Hypersonic Testing Capabilities. 26 January 2024.
62. Web site: Taking Apart a Wind Tunnel. 26 January 2024.
63. News: NASA Langley dismantles wind tunnel, part of Columbia disaster probe. Dietrich. Tamara. dailypress.com. 2018-07-24.
64. Web site: The Langley 15-inch Mach 6 High Temperature Tunnel. Jeffery. Hodge. 17 August 2012. 10.2514/6.1992-3938. 26 January 2024.
65. Web site: 8-Foot High Temperature Tunnel (HTT). 26 January 2024.
66. Web site: Current Test Capabilities of NASA Langley’s Arc-Heated Scramjet Test Facility. 26 January 2024.
67. Web site: The NASA Langley Scramjet Test Complex. 26 January 2024.
68. Web site: NASA's HYPULSE Facility at GASL A Dual Mode, Dual Driver Reflected-Shock/Expansion Tunnel. 26 January 2024.
69. Web site: National Transonic Facility. 26 January 2024.
70. Web site: 100 Years of Rocketry and Research at NASA’s Langley Facility. 26 January 2024.
71. Web site: 12 Foot Low-Speed Tunnel (12 FT LST). 26 January 2024.
72. Web site: Low Turbulence Pressure Tunnel (Building 582A). 26 January 2024.
73. Web site: 16-Foot Transonic Tunnel (Building 1146). 26 January 2024.
74. Web site: National Wind Tunnel Facility. 27 January 2024.
75. Web site: ODTÜ-RÜZGEM Large Scale Wind Tunnel at The Middle East Technical University (METU). 26 January 2024.
76. Web site: ONERA Mondane Wind Tunnel. ONERA. 16 November 2017. 26 January 2024.
77. Web site: S2MA Continuous-flow wind tunnel, Variable pressure, Mach 0.1 to Mach 3.0 . ONERA.
78. Web site: -PHEDRA- Institut de Combustion Aérothermique Réactivité et Environnement. 26 January 2024.
79. Web site: Poul la Cour Tunnel (PLCT). 26 January 2024.
80. Web site: Propulsion Wind Tunnel Facility. 27 January 2024.
81. Web site: Rail Tec Arsenal Climatic Wind Tunnel. 26 January 2024.
82. Web site: R J Mitchell Wind Tunnel. 27 January 2024.
83. Web site: RWDI's Wind Tunnels and Model Shop . RWDI . 26 January 2024.
84. Web site: San Diego Wind Tunnel. 26 January 2024.
85. Web site: Tunel de vento hipersônico T3 entra em fase de qualificação.. https://web.archive.org/web/20110706155336/http://www.ieav.cta.br/Comunicacao_Social/noticias/T3_NOTAER2_2007.pdf . 6 July 2011. IEAv. 18 January 2011. pt.
86. Web site: Texas A&M University Oran W. Nicks Low-Speed Wind Tunnel (TAMU LSWT) . 26 January 2024.
87. Web site: Vehicle Climatic Wind Tunnel. 26 January 2024.
88. Web site: The George C. Marshall Space Flight Center's 14 x 14-Inch Trisonic Wind Tunnel - A historical perspective. 26 January 2024.
89. Web site: Deutsche Versuchsanstalt für Luftfahrt (DVL). de. 27 January 2024.
90. Web site: University of British Columbia Boundary Layer Wind Tunnel. 26 January 2024.
91. Web site: University of British Columbia Parkinson Wind Tunnel. 26 January 2024.
92. Web site: Kirsten Wind Tunnel (KWT). 26 January 2024.
93. Web site: 3x3 Low-Speed Wind Tunnel. 26 January 2024.
94. Web site: Virginia Tech Stability Wind Tunnel. 26 January 2024.
95. Web site: The von Karman Gas Dynamics Facility Wind Tunnels. 27 January 2024.
96. Web site: Team Lotus signs Williams tunnel deal. Jonathan. Noble. 13 June 2011. 26 January 2024.
97. Web site: Windshear. 26 January 2024.
98. Web site: Windtech Boundary Layer Wind Tunnel. 26 January 2024.