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The AARL houses four active wind tunnels (dimensions of test section given in name): -3'x5'(.9m x 1.5m) Subsonic Wind Tunnel, an open circuit, Eiffel wind tunnel with top speeds of 150 ft/s (45m/s) [3]-6"x22" (15cm x 56cm) Transonic Windtunnel, a blowdown wind tunnel used specifically for airfoil research [4]
wind tunnels, jet engine test cell design: Ames Laboratory: Iowa State University: Ames, IA: separated and studied rare earth elements [note 1] Applied Physics Laboratory: Johns Hopkins: Laurel, MD: development of guided missile technology and drones. Applied Research Laboratory: Pennsylvania State University: State College, PA: hydrodynamics ...
Wind tunnel testing of automobiles began in the 1920s, [32] on cars such as the Rumpler Tropfenwagen, and the Chrysler Airflow. Initially, scale models were tested, then larger wind tunnels were built to test full-scale cars with the capability to measure aerodynamic drag which enables improvements to be made for reducing fuel consumption.
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.
Wind tunnel testing 717th Test Squadron: Arnold AFB: Turbine engine testing 718th Test Squadron: ... Test and Evaluation Squadrons: Squadron Shield Location Nickname
The 40 by 80 Foot Wind Tunnel is primarily used for determining the low- and medium-speed aerodynamic characteristics of high-performance aircraft, rotorcraft, and fixed wing, powered-lift V/STOL aircraft. The 80 by 120 Foot Wind Tunnel is the world's largest wind tunnel test section.
16S is a supersonic wind tunnel that can be configured for Mach numbers from 1.5 to 4.750. The test section is also 16-foot-square and 40-foot long. The facility can simulate unit Reynolds numbers from approximately 0.1 to 2.4 million per foot or altitude conditions from 43,000 to 154,000 feet.
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.