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  2. Arnold Engineering Development Complex - Wikipedia

    en.wikipedia.org/wiki/Arnold_Engineering...

    While AEDC's primary location is in Tennessee, it also operates two geographically separated facilities—the Hypervelocity Wind Tunnel 9 in Maryland, and the National Full-Scale Aerodynamics Complex (NFAC), in California. AEDC's economic impact to the local area for fiscal year 2008 exceeded $728 million.

  3. Hypervelocity Wind Tunnel 9 - Wikipedia

    en.wikipedia.org/wiki/Hypervelocity_Wind_Tunnel_9

    After World War II, the United States brought German scientists and several critical facilities built by Nazi Germany to continue research into supersonic missiles. In July 1945, the custody of the Kochel wind tunnel facilities was awarded to the Navy to be installed at the Naval Ordnance Laboratory at White Oak, Maryland. In 1967, Congress ...

  4. Hypersonic wind tunnel - Wikipedia

    en.wikipedia.org/wiki/Hypersonic_wind_tunnel

    NASA Langley's Hypersonic Facilities Complex, 1969. A hypersonic wind tunnel is designed to generate a hypersonic flow field in the working section, thus simulating the typical flow features of this flow regime - including compression shocks and pronounced boundary layer effects, entropy layer and viscous interaction zones and most importantly high total temperatures of the flow.

  5. List of wind tunnels - Wikipedia

    en.wikipedia.org/wiki/List_of_wind_tunnels

    Part of the UK National Wind Tunnel Facility: CRIACIV Boundary Layer Wind Tunnel - University of Florence [25] Operational 2.44 m × 1.6 m × 10 m (8 ft 0 in × 5 ft 3 in × 32 ft 10 in) Building, bridges, general purpose Italy Closed circuit wind tunnel, T-shaped diffuser, one atmospheric test section (max speed 31 m/s [100 ft/s]).

  6. Aerodynamic and Propulsion Test Unit - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_and_Propulsion...

    The facility was designed to provide ground-based simulations of supersonic and hypersonic flight conditions. The combustion air heater can provide total pressures from 200 psia to 2,800 psia (13.6 atm to 190.5 atm) and a total temperatures from 1,200°R to 4,700°R (667 K to 2,611 K).

  7. With the ability to travel commercially at speeds near or above Mach 5, we stand on the brink of revolutionizing global mobility, shrinking the vast distances that separate us. However, that is ...

  8. High-Enthalpy Arc Heated Facility - Wikipedia

    en.wikipedia.org/wiki/High-Enthalpy_Arc_Heated...

    The HEAT-H2 Test Unit is an arc-heated aerothermal tunnel providing high-enthalpy flow at high Mach numbers and dynamic pressures simulating hypersonic flight at pressure altitudes up to 120 atm. H2 utilitzes an N-4 Huels-type arc heater to generate high-temperature, high-pressure air for expansion through a hypersonic nozzle into the evacuated test cell.

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