Flight demonstration wind tunnel testing device
Flight demonstration wind tunnel experimental device
This is a device specially designed to conduct extensive experiments on the takeoff, flight, and landing of aircraft. The aircraft model in the suction-type open wind tunnel consists of two propellers, a main wing with a chord length of 152mm (NACA2412), and a fully movable tail with a chord length of 76mm. Air flowing in from the bell mouth is discharged from the device through a straightening honeycomb, the experimental area equipped with the aircraft, a diffusion body, an axial fan, and a silencing duct. The control wheel located at the front of the experimental area manipulates the tail angle of the aircraft model, while the lever simulating the engine throttle on the right side controls the wind speed within the wind tunnel.
- Company：メガケム
- Price：Other
