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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]).
In 1967, Congress granted approval for the construction of Tunnel 9. The facility became operational in 1976 and has since been providing aerodynamic simulation in critical altitude regimes associated with strategic offensive missile systems, advanced defensive interceptor systems, and hypersonic vehicle technologies.
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.
The Hypervelocity Wind Tunnel 9 is located in Silver Spring, Maryland; The National Full-Scale Aerodynamics Complex (NFAC) is located at NASA Ames Research Center, Moffett Field, California. The NFAC was closed by NASA in 2003. In February 2006, AEDC entered into an agreement with NASA to lease the facility for a period of up to 25 years.
The hypersonic shock tunnel is another impulse facility with a run time of 0.5 to 5.0 ms. The tunnel has a test section of 0.44 meters (diameter) by a length of 1 meter. The inviscid core is 0.17 m at Mach 8. It is capable of testing at Mach numbers from 5 to 16 and Reynolds numbers from 100 to 20 million per meter.
The Hypersonic Air-breathing Weapon Concept, or HAWC, is a joint project between the U.S. Air Force and the Defense Advanced Research Projects Agency (DARPA) to develop and test air-launched ...
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).
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