Thursday, 17 September 2015

Wind Tunnel Testing


Wind Tunnel Test
Models of proposed aircraft, engines or components are aerodynamically tested using a variety of sensors options.

Environment
·      Control room

Typical inputs
Acceleration, pressure, load, displacement, torque, tilt, angle, temperature

DEWETRON benefits
Fully scalable systems provide variable input configurations for 100s or 1000s channels of accelerometers (IEPE) or strain gauges (bridge input) totally synced to further analogue, digital or video inputs.


Reference Customers
·         NASA Langley, USA
·         NASA Glenn, USA











If you require a fully scalable system that can provide Wind Tunnel Testing on your equipment or products and you are situated in either Australia or New Zealand contact Metromatics now on +61 7 3868 4255 or sales@metromatics.com.au

If outside this area, please contact Dewetron directly on +43 316 3070 or info@dewetron.com

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