NACA 2412 AEROFOIL MODEL WITH FLAP

A 150 mm chord NACA2412 unsymmetrical section aerofoil with 300 mm span and adjustable flap for use with the Subsonic Wind Tunnel.

An unsymmetrical section (cambered) aerofoil with adjustable flap. The adjustable flap allows students to study the effects of control surfaces such as flaps, ailerons, elevator or rudder. Students can also examine the difference between unsymmetrical and symmetrical aerofoils, by comparing the results to the symmetrical aerofoils. Learn about NACA 2412 AEROFOIL MODEL WITH FLAP specifications for optimal educational outcomes.. The Three-Component Balance (available separately) can hold the aerofoil to measure lift, drag and pitching moment. Using a Pitot tube, students can traverse the aerofoil wake to find the downstream pressure distribution and find the drag on the aerofoil. Learn about NACA 2412 AEROFOIL MODEL WITH FLAP for educational labs for optimal educational outcomes.. They can compare these results with the direct measurements from a balance. A Smoke Generator (not included) increases the educational value of the experiments by showing the flow of air around the model. Learn about NACA 2412 AEROFOIL MODEL WITH FLAP suppliers for optimal educational outcomes..