Aerodynamics Lab in Bangladesh

EDIBON teaching and research units for the aerodynamics laboratory, supplied, installed and commissioned in Bangladesh by Vvon with faculty training included. 13 units available.

13 products from 1 manufacturer: EDIBON.

Products

• TAS25/100C: Computer Controlled Supersonic Wind Tunnel — EDIBON: TAS25/100C is a computer controlled supersonic wind tunnel. Interchangeable nozzle blocks set the test section Mach number and a schlieren system shows shock waves and expansion fans around models. A three blower version, TAS25/100C-3B, is also published.
• TA50/250: Aerodynamic Tunnel, 50X250 mm — EDIBON: TA50/250 is a small subsonic wind tunnel with a 50 x 250 mm working section. Aerofoil models fitted with pressure tappings allow the pressure distribution, lift and drag to be measured at different angles of attack. A computer controlled version, TA50/250C, is also published.
• TA300/300: Aerodynamic Tunnel, 300X300 mm — EDIBON: TA300/300 is an open circuit subsonic wind tunnel with a 300 x 300 mm working section. A balance measures lift and drag on aerofoils, cylinders and other models over a range of speeds and angles of attack. A computer controlled version, TA300/300C, is also published.
• TA610/915C: Computer Controlled Aerodynamic Tunnel, 610X915 mm — EDIBON: TA610/915C is a computer controlled subsonic wind tunnel with a 610 x 915 mm working section. Lift, drag and pressure distribution on larger models are logged through the data acquisition system over a range of air speeds.
• TA1000/1000C: Computer Controlled Aerodynamic Tunnel, 1000X1000 mm — EDIBON: TA1000/1000C is a computer controlled subsonic wind tunnel with a 1000 x 1000 mm working section. It is used for aerodynamic testing of larger models, with forces, pressures and air speed logged through the data acquisition system.
• TA1200/1200C: Computer Controlled Aerodynamic Tunnel, 1200X1200 mm — EDIBON: TA1200/1200C is a computer controlled subsonic wind tunnel with a 1200 x 1200 mm working section. The larger section suits work on vehicle, building and aerofoil models, with forces and pressures logged during each run.
• TACL2000/2000C: Computer Controlled Closed Aerodynamic Tunnel, 2000X2000 mm — EDIBON: TACL2000/2000C is a computer controlled closed circuit wind tunnel with a 2000 x 2000 mm working section. The closed return gives steady, low turbulence flow for testing large models, with data logged through the acquisition system.
• TADV225/450: Aerodynamic Tunnel Flight Demonstration Unit — EDIBON: TADV225/450 is a wind tunnel arranged to demonstrate the forces acting on an aircraft in flight. A model aircraft free to move in pitch, roll and yaw shows how control surfaces and angle of attack change its attitude.
• ATBB: Aerodynamic Testing Bench — EDIBON: ATBB is a bench for basic aerodynamic experiments. Air is drawn over interchangeable models so that drag, boundary layer growth, pressure distribution and the flow around bluff and streamlined bodies can be measured.
• TAVF180/100: Aerodynamic Tunnel for Flow Visualization — EDIBON: TAVF180/100 is a tunnel with upward air flow for visualising two dimensional flow. Smoke filaments pass over aerofoils, cylinders and other shapes so streamlines, separation and wake formation can be seen and photographed.
• TAS25/100C-3B: Computer Controlled Supersonic Wind Tunnel (Three Blowers) — EDIBON: The three blower version of the EDIBON supersonic wind tunnel. Three computer controlled vacuum pumps or blowers on the discharge side draw air through the working section, where interchangeable contours give subsonic, transonic and supersonic flow over the models.
• TA50/250C: Computer Controlled Aerodynamic Tunnel, 50X250 mm — EDIBON: A bench top open circuit wind tunnel for subsonic, incompressible flow, with the fan speed set from the computer. Lips, a haven section and an 8 to 1 contraction develop the flow before it reaches a transparent working area fitted with a Pitot static tube.
• TA300/300C: Computer Controlled Aerodynamic Tunnel, 300X300 mm — EDIBON: A subsonic open circuit wind tunnel with a 300 by 300 mm working area and computer controlled fan. A 9.5 to 1 contraction and a diffuser outlet keep the flow well developed and free of turbulence over aircraft and body models.

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