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1m - Wind Tunnel (1MG)
Göttingen-type low speed wind tunnel with open jet test section and closed return
1m Wind Tunnel
Airbus - half model in the 1m Wind Tunnel
Generic truc model in the 1m Wind Tunnel
1m Wind Tunnel, Göttingen
1m Wind Tunnel, Göttingen:
Operational date: 1962
Test section size:
1.0 m x 0.7 m elliptic or rectangular
Length: 1.3 m or 2.3 m
Nozzle contraction ratio: 4.8
Maximum velocity: 65 m/s
Installed power: 88 kW
Applied testing techniques:
Balances for forces and moments,
mean and unsteady pressure distributions,
hot-wire anemometry,
surface hot film technique,
oil flow visualization,
Laser light sheet visualization,
Particle image velocimetry (PIV),
Field of application:
Fundamental experiments on boundary layer transition and separation,
Investigation of vortex flows,
Probe calibrations (cup anemometers, multi-hole pressure probes, thermal anemometers)
Measurements in the field of industrial and vehicle aerodynamics
Related Articles
Department Helicopters (AS-HEL)
Experimental investigations
Related Topics
Aerodynamic
Fluid Mechanics and Thermodynamics
Meteorology and Climatology
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