Computer Controlled Wind Tunnel Deluxe

Enables the user to carry out advanced studies in aerodynamics fields including boundary layer experiments, flow visualization, pressure distribution, turbulence study and development of self-designed aerodynamic profiles.

Enables the user to carry out advanced studies in aerodynamics fields including boundary layer experiments, flow visualization, pressure distribution, study of turbulence and offering the possibility of developing self-design aerodynamics profiles to be tested.

• Stand-alone computer controlled subsonic wind tunnel
• Mounted on steel base with wheels for mobility
• Working section: 310mm x 310mm x 660mm long
• Open circuit operation system
• Inverter controlled AC suction fan
• Accurate speed control up to 40m/s
• Honeycomb flow straightener for even flow direction
• Three tappings in top section for pitot tubes
• Circular hatch of 160mm diameter for model insertion
• Angular scale on accessories for manual rotation
• Linear speed: 0-40m/s
• Axial fan power: Approx. 4kW
• Fan turning speed: 3000rpm
• Manometer range: 0-250mm H₂O
• Angle of inclination: +/- 180°
• Lift force: +/- 10N
• Drag force: +/- 10N
• Pitching moment: +/- 3N