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The C30 – Computer Controlled Wind Tunnel enables the user to carry out advanced studies in the Aerodynamics fields including boundary layer experiments, flow visualisation, pressure distribution, study of turbulence and offering the possibility of developing self-design aerodynamics profiles to be tested.
The wind tunnel comprises outstanding features such as computer control, remote operation, datalogging and diagrams plotting in real time.
The system also benefits from clear visualisation of every model under test due to the architecture of the working section in transparent material and the compact design of all components.
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