Subsonic Reverse Wind Tunnel.
Subsonic Reverse Wind Tunnel
This wind tunnel generates an airstream
(60m/s max.) in a transparent test section (300 x 300 mm). Different
accessories (aerofoil section, static tube) can be installed in the test
section to test the subsonic aerodynamic laws.
This wind tunnel has a reduced volume and is fitted into laboratories and test floors without necessitating installation or civil engineering works.
It allows some very demonstrative experiments in aerodynamics to be carried out, such as.
A test section comprising two vertical glass surfaces, one of which is entirely hinged to allow access to the interior of the test section. The upper part has a lengthwise slit fitted with joints to allow a probe to be attached. A movement system with one, two or three axes can be inserted on the test section.