Computer Controlled Subsonic Wind Tunnel

Wind tunnel is a facility for creating a uniform wind of known value in a test section where fluid flow phenomena can be investigated, models, of Aircrafts etc., can be tested from their performance, and also students training/teaching in fluid mechanics/aerodynamics. The facility can also be used for industrial aerodynamics testing and simulation studies on many of fluid problems. The main part of the tunnel are Honey comb section, screens, contraction cone, test section, diffuser, safety screens, fan section, fan, motor and speed control drivers. KEY SPECIFICATION Computerised Data System�Type of tunnel: Open circuit-suction type.Test section size: 0 - 1500 mm (As per Need)Maximum speed: 0- 50 m/secFan: Axial flow fan, Maximum rpm 1440Contraction Ratio: 9:1