| 释义 |
- References
{{More citations needed|date=February 2017}}| Name | Status | Size | Use | Location | Comments |
|---|
| ACE Climatic Wind Tunnel | L 46 ft x W 14.7 ft x H 9.5 ft (L 14.3 m x W 4.5 m x H 2.9 m) | Full scale: automotive, motorsport, cycling, skiing, architectural, transit, truck, product development | Oshawa, Ontario, Canada | Available and accessible for all industries requiring wind tunnel services or climatic services | | A2 wind tunnel | Test section W ~14 ft x H ~10 ft x L ~20 ft | Full scale general purpose | Mooresville, NC, USA | ~$500/hr full scale race car, motorcycle, bicycle | | AeroDyn Wind Tunnel | Full scale NASCAR racecars | Mooresville, NC, USA | | Auto Research Center (ARC) | W 2.3 m x H 2.1 m (W 7.4 ft x H 6.9 ft) | Subsonic research and development including: 50% scale model automotive rolling road, wind turbine design and optimization, and cycling | Indianapolis, IN, USA | 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. | | Boeing Subsonic (low-speed) Wind Tunnel - BVWT | Operational | 20 x 20 ft | Philadelphia, PA | Contact Boeing Technology Services for additional information about or to use Boeing Facilities[1] | | Boeing Transonic Wind Tunnel – BTWT | Operational | 8 x 12 ft | Seattle, WA | | Boeing Polysonic (supersonic) Wind Tunnel – PSWT | Operational | 4 x 4 ft | St. Louis, MO | | Boeing Icing Wind Tunnel – BRAIT | Operational | 4 x 6 ft | Seattle, WA | | Boeing Low-speed Aero-Acoustic Facility – LSAF | Operational | Varies | Seattle, WA | | [https://aero.calpoly.edu/facilities/windtunnel Cal Poly's Low- Speed Wind Tunnel] | L 14 ft x W 4 ft x H 3 ft (L 4.3 m x W 1.22 m x H 0.91 m) | Low speed: Scale model testing, Aerospace, Automotive, IR industry | San Luis Obispo, CA, USA | Startups, major Aerospace corporations and other scientific equipment tested here. Rolling road implementation in progress. | | Calspan Wind Tunnel | Operational | 8|x|8|ft|abbr=on}} | Subsonic / Transonic | Buffalo, New York, USA | The only independently owned and operated wind tunnel in the United States. | | CSTB Jules Verne dynamic wind tunnel | operational | W 6m x H 5m x L 12m[2] | Automotive, Rail, Full scale general purpose | CSTB Nantes, France | Three test sections with wind speeds up to 280 km/h | | CSTB Jules Verne climatic wind tunnel | operational | W 10m x H 7m x L 20m[3] | Automotive, Rail, Building components, Icing, snow, hot and cold climates | CSTB Nantes, France | |
| CSTB Jules Verne atmospheric wind tunnels | operational | W 4m x H 2.5m x L 20m[4] | Wind Engineering, Scale buildings, Dispersion | CSTB Nantes, France | Two wind tunnels | | European transonic wind tunnel | Transonic | Cologne, Germany | | NASA Langley Eight-Foot High Speed Tunnel[5] | 8|ft|abbr=on}} | High speed | Hampton, Virginia, USA | | NASA Langley 30- by 60-Foot Full-Scale Wind Tunnel[6] | demolished | 30|ft|abbr=on}} by {{convert|60|ft|abbr=on}} | Full-scale aircraft | Hampton, Virginia, USA | NASA's oldest operating wind tunnel until its closing in October of 1995 | | Glenn L. Martin Wind Tunnel | Test section 7.75 ft x 11.04 ft (corner fillets) | Low speed: scale model testing, automotive, aerospace | University of Maryland, College Park, Maryland, USA | | NASA Glenn Hypersonic Test Facility] Hypersonic | Sandusky, Ohio, USA | | Modine Wind Tunnel | 46 L x 14 W x 13.5 H ft | Racine, Wisconsin, USA | Climatic wind tunnel testing, large truck and automotive | | Ames 7×10 foot Wind Tunnel (operated by the US Army) | 7|x|10|ft|abbr=on}} | Mountain View, California, USA | | San Diego Wind Tunnel | San Diego, CA, USA | Major airframers, bicycle manufacturers and professional athletes | | NASA Ames Trisonic wind tunnel | El Segundo, California, USA | | NASA Ames National Full Scale Aerodynamic Complex (operated by the US Air Force) | 40|x|80|ft|abbr=on}} | Subsonic | Mountain View, California, USA | | NASA Ames Unitary Plan Wind Tunnel | Mountain View, CA, USA | | Variable Density Tunnel | Variable density | Hampton, Virginia, USA | | Vertical wind tunnel; Central Aerohydrodynamic Institute | Vertical | Moscow, Russia | | Wind Shear's Full Scale, Rolling Road, Automotive Wind Tunnel | Wind shear | Concord, NC, USA | | NASA Ames Hypersonic Propulsion Integration 16 Inch Shock | 16|in|cm|abbr=on}} | Hypersonic propulsion | Mountain View, CA, USA | | NASA Ames Hypersonic Propulsion Integration Direct-Connect | Hypersonic propulsion | Mountain View, CA, USA | | NASA Ames National Full Scale Aerodynamic Complex (operated by the US Air Force) | 80|x|120|ft|abbr=on}} | Subsonic atmospheric | Mountain View, CA, USA | Largest wind tunnel in the world | | NASA Ames Subsonic 12 Foot High-Rn Pressure | 12|ft|abbr=on}} | Subsonic | Mountain View, CA, USA | | NASA Ames Supersonic 9×7 Foot High-Rn | 9|x|7|ft|abbr=on}} | Supersonic | Mountain View, CA, USA | | NASA Ames Transonic 11 Foot High-Rn | 11 ft | Transonic | Mountain View, CA, USA | | NASA Glenn 10- by 10-Foot Abe Silverstein Supersonic Wind Tunnel | 10|x|10|ft|abbr=on}} | Supersonic | Cleveland, OH, USA | | NASA Glenn 9- by 15-Foot Wind Tunnel | 9|x|15|ft|abbr=on}} | Subsonic | Cleveland, OH, USA | | NASA Glenn 8- by 6-Foot Wind Tunnel | 8|x|6|ft|abbr=on}} | Transonic | Cleveland, OH, USA | | NASA Glenn Aero-Acoustic Propulsion Laboratory Nozzle Aeroacoustic Test Rig | 53|in|abbr=on}} | Acoustic testing of exhaust nozzles, subsonic | Cleveland, OH, USA | Free-jet | | NASA Glenn Engine Components Research Lab | Cleveland, OH, USA | | NASA Glenn Icing Research Tunnel | Subsonic Icing | Cleveland, OH, USA | | NASA Glenn Propulsion Systems Laboratory | active | Full-Scale Engine Testing | Cleveland, OH, USA | Four test cells: 1 & 2 demolished; 3 & 4 active. Cell 3 has icing capabilities | | TitanX Jamestown Vehicle Climatic Wind Tunnel | 9.4 ft x 11.4 ft (3.0 m x 3.5 m) | Climatic testing of vehicle systems and entire trucks | Jamestown, NY, USA | Open for external clients | | NASA Langley Hypersonic 20 Inch Mach 6 Air | 20|in|cm|abbr=on}} | Hypersonic | Hampton, VA | | NASA Langley Hypersonic 31 Inch Mach 10 Air | 31|in|cm|abbr=on}} | Hypersonic | Hampton, VA, USA | | NASA Langley Hypersonic 20 Inch Mach 6 Tetrafluoromethane | Demolished in 2016[7] | 20|in|cm|abbr=on}} | Hypersonic | Hampton, VA, USA | | NASA Langley Hypersonic Propulsion Integration 8 Foot High-Temperature Tunnel | 8|ft|abbr=on}} | Hypersonic, high-temperature | Hampton, VA, USA | | NASA Langley Hypersonic Propulsion Integration Arc-Heated Scramjet | Hypersonic | Hampton, VA, USA | | NASA Langley Hypersonic Propulsion Integration Combustion Scramjet | Hypersonic | Hampton, VA, USA | | NASA Langley Hypersonic Propulsion Integration Supersonic Combustion | Hypersonic | Hampton, VA | | NASA Langley Hypersonic Propulsion Integration 15 Inch Mach 6 High-Temperature Tunnel | 15|in|cm|abbr=on}} | Hypersonic | Hampton, VA, USA | | NASA Langley Subsonic 12 Foot Atmospheric Lab | 12|ft|abbr=on}} | Subsonic atmospheric | Hampton, VA, USA | | NASA Langley Subsonic 20 Foot Vertical Spin Tunnel | 20|ft|abbr=on}} | Subsonic vertical spin | Hampton, VA, USA | | NASA Langley Subsonic 14×22 foot Atmospheric | 14|x|22|ft|abbr=on}} | Subsonic atmospheric | Hampton, VA, USA | | NASA Langley Subsonic Low-Turbulence Pressure Tunnel | Subsonic low-turbulence | Hampton, VA, USA | | NASA Langley Supersonic High-Rn | Supersonic | Hampton, VA, USA | | NASA Langley High-Rn Transonic Dynamics Tunnel | Transonic | Hampton, VA, USA | | NASA Langley Transonic 16 Foot Atmospheric | 16|ft|abbr=on}} | Transonic atmospheric | Hampton, VA, USA | | NASA Langley National Transonic Facility | Transonic | Hampton, VA, USA | | NASA Langley NASA/GASL HYPULSE Propulsion Integration | Hampton, VA, USA | | ONERA Modane wind tunnel | Operational | D 8m x L 14m[8] | Subsonic atmospheric | ONERA Modane, France | Largest continuous blow-down wind tunnel in the world, Mach 0.05 to 1.[9] | | RWDI Wind Tunnels | operational | 24 ft, 12 ft[10] | Wind engineering, scale buildings | Guelph, Ontario, Canada | Two wind tunnels | | Texas A&M Oran W. Nicks Low Speed Wind Tunnel | L 12 ft x W 10 ft x H 7 ft | Scale aircraft, UAV, rocket, missile, academic research, automotive, motorsport, cycling, skiing, architectural, transit, truck, product development 0-200MPH | Texas A&M University, College Station, TX, USA | 7ft x 7ft, capable of mach 0.4 | | [https://web.archive.org/web/20160128224822/http://www.uwal.org/ University of Washington Aeronautical Laboratory ("UWAL"), Kirsten Wind Tunnel] | 8 ft x 12 ft | Subsonic | Seattle, WA, USA | | [https://www.uw.edu/ University of Washington Dept. of Aero&Astro 3X3] | 3 ft x 3 ft | Velocity range approx. 20 to 135 mph | Seattle, WA, USA | The original "Boeing Aerodynamical Chamber", built in 1918 with an Eiffel 4 ft by 4ft and updated in the early 1990s with new power systems and a higher velocity EDL 3 ft by 3 ft | | Virginia Tech Stability Wind Tunnel | 6|x|6|ft|abbr=on}} | Blacksburg, Virginia | | MARHy wind tunnel(Experimental plateform FAST) | operational | 5m x 2.5m cylindrical test chamber | Hypersonic/supersonic rarefied wind tunnel. No limit running time. Reynolds number /cm: 26.3 < Re < 7522;Mach number: 0.8 < Mach < 20 | Laboratoire ICARE, CNRS, Orleans, FRANCE | Fundamental and applied research of fluid dynamic phenomena in rarefied compressible flows. Aerodynamic and aerothermal behavior of probes and models;Plasma flow control in rarefied and super/hypersonic flows. | | PHEDRA (Experimental plateform FAST) | operational | 4.5m x 2.1 m cylindrical test chamber | 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 | Laboratoire ICARE, CNRS, Orleans, FRANCE | Fundamental research of high enthalpy fluid dynamic phenomena in non-equilibrium flows. Aerodynamic and aerothermal behavior of probes and models; Atmospheric entry research. | | EDITH supersonic wind tunnel (Experimental plateform FAST) | operational | 1.2 m x 1.7 m cylindrical test chamber | Long shot time running (20 minutes). | Laboratoire ICARE, CNRS, Orleans, FRANCE | Fundamental research on shock waves. Aerodynamic and aerothermal behavior of probes and models. Fluidic thrust vectoring of supersonic nozzle | | Large Amplitude Multi-Purpose (LAMP) Vertical Wind Tunnel Bihrle Applied Research | Operational | 10 ft Test Section | Vertical, Subsonic, High AOA, Static or body-axis oscillatory | Neuburg a.d. Donau, 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. | |
References1. ^{{Cite web|url=http://www.boeing.com/company/key-orgs/boeing-technology-services/wind-tunnels-and-propulsion.page|title=Boeing: Wind Tunnels and Propulsion Testing Services|website=www.boeing.com|access-date=2017-11-21}}
2. ^{{cite web |url=http://recherche.cstb.fr/en/facilities/climatic-wind/ |title=JULES VERNE CLIMATIC WIND TUNNEL |publisher=CSTB |date=2017-10-02}}
3. ^{{cite web |url=http://recherche.cstb.fr/en/facilities/climatic-wind/ |title=JULES VERNE CLIMATIC WIND TUNNEL |publisher=CSTB |date=2017-10-02}}
4. ^{{cite web |url=http://recherche.cstb.fr/en/facilities/atmospheric-wind-tunnels/ |title=CSTB Atmospheric Wind Tunnels |publisher=CSTB |date=2017-10-02}}
5. ^{{cite web|title=8-Foot High Speed Tunnel|url=https://crgis.ndc.nasa.gov/historic/8-Foot_High_Speed_Tunnel|website=nasa.gov|publisher=National Aeronautics and Space Administration|accessdate=10 February 2018}}
6. ^{{cite web|title=NASA Langley's 30- by 60-Foot Tunnel|url=https://www.nasa.gov/centers/langley/news/factsheets/30X60.html|website=nasa.gov|publisher=National Aeronautics and Space Administration|accessdate=10 February 2018}}
7. ^{{Cite news|url=http://www.dailypress.com/news/science/dp-nws-nasa-wind-tunnel-20161011-story.html|title=NASA Langley dismantles wind tunnel, part of Columbia disaster probe|last=Dietrich|first=Tamara|work=dailypress.com|access-date=2018-07-24|language=en-US}}
8. ^{{cite web |url=http://www.onera.fr/windtunnel/s1ma-continuous-flow-wind-tunnel-atmospheric-mach-005-mach-1|title=ONERA MODANE WIND TUNNEL|publisher=ONERA|date=2017-11-16}}
9. ^{{cite web |url=http://www.onera.fr/windtunnel/s1ma-continuous-flow-wind-tunnel-atmospheric-mach-005-mach-1|title=ONERA MODANE WIND TUNNEL|publisher=ONERA|date=2017-11-16}}
10. ^{{cite web |url=https://www.youtube.com/watch?v=tccGoXYY6p8 |title=Our New State-of-the-Art Facility |publisher=RWDI |date=2016-12-02}}
7. http://www.boeing.com/company/key-orgs/boeing-technology-services/wind-tunnels-and-propulsion.page 1 : Wind tunnels |