Specification :

WT40 Aerodynamic Laboratory Subsonic Wind Tunnel.
Open Circuit Type Wind Tunnel
Test Section Dimension : 400 mm x 400 mm x 1000 mm
Total Length 4600 mm
Composite Fiberglass Construction
Air Speed 0 - 40 m/ s
Axial Fan Drive with 4 kW 380V 3ph Induction Motor
Desk Mounted Control Panel
Power required 5 KW 220/ 380 VAC 3Phase

Instrumentation and Measurement System ( Basic Configuration)
Pitot Tube, Wake Rake
Lift& Drag Balance w/ digital display
32 glass tubes Manometer
Digital air speed indicator
Equiped with aerodynamic models such as ball, cylinder, slender bodies, 3 NACA airfoils, model airplane.

PC Based Data Acquisition ( Optional for research laboratory)
Lift & Drag Measurement System
2x50 N Load, Airspeed, RPM, Air Temp Sensor
Pressure Distribution Measurement System consists of
32 channel Differential Pressure Sensor .
32 channel Real Time Data Acqusition.
Note book PC data processing & recorder.