AEDC Aerodynamic and Propulsion Test Unit (APTU) is a blowdown hypersonic wind tunnel driven by a combustion air heater (CAH). The facility is owned by the United States Air Force and operated by Aerospace Testing Alliance.

History

The AEDC Aerodynamic and Propulsion Test Unit started out as a vitiated air heater (VAH) conducting over 275 experiments for the development of many different aerodynamic and aerothermal systems. Upgrades to the facility started in 2002 in order to provide ground-test capability for supersonic and hypersonic systems up to flight speeds of Mach 8.

Capabilities

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). Five nozzles ranging from Mach 3.2 to Mach 7.1 are currently available.

See also

  • Arnold Air Force Base
  • Supersonic wind tunnel
  • Scramjet

References

External links

  • Arnold Engineering Development Center (official)

Analysis of propulsion units dedicated to test stands for aviation systems

Aerodynamics and Propulsion PhD in Aerospace Engineering UC3M

DVIDS Images HighSpeed Aerodynamics and Propulsion Laboratory

aerodynamicstest Nussbaum Transportation

AERODYNAMIC AND PROPULSION TEST UNIT > Arnold Air Force Base > Display