AERODYNAMIC LABORATORY WIND TUNNEL

KOMPONEN: Wind Tunnel Open Circuit Type Wind Tunnel Total Length 3,600 mm 900 mm X 900mm Inlet section Honeycomb Flow Strightener Composite Fiberglass Construction Air Speed 0 - 30 m/ s Test Section: 300 mm x 300 mm x 1,000 mm Axial Fan Drive with 3 HP Motor Control Panel Sturdy steel construction Support Cabinet for Tools Instrumentation and Measurement System Pitot Tube, 8 pipe Wake Rake PC Based Wind Tunnel DAQ (L, D, V, T, RPM) PC Notebook 14LED, 2GB DDR3, 500GB HDD PC Based 32 channel Pressure Data Logger 2 x 50 N Load Sensor with mounting Lift amp; Drag Balance w/ Model Holder Digital Anemometer amp; Thermometer 36 Tubes Water Manometer 32 Channel Pressure Sensor Digital Manometer Aerodynamics Models Ball, Cylinder (L,D) Airfoil NACA 0012, NACA 6412 (L,D) Airfoil NACA 2412 with Flap (L,D) Airfoil NACA 6417 Pressure Distribution