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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, 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
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Texte zu diesem Artikel
Department Helicopters (AS-HEL) (http://www.dlr.de/as/en/desktopdefault.aspx/tabid-192/402_read-571/usetemplate-print/) |
Experimental investigations (http://www.dlr.de/as/en/desktopdefault.aspx/tabid-192/402_read-1624/usetemplate-print/) |
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