AF1300C - Experiment

NACA 2412 AEROFOIL MODEL WITH FLAP

PDF datasheet

A 150 mm chord NACA2412 unsymmetrical section aerofoil with 300 mm span and adjustable flap for use with the AF1300 Subsonic Wind Tunnel.

OR CALL US TO DISCUSS+44 1159 722 611

NACA 2412 AEROFOIL MODEL WITH FLAP

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 AF104 symmetrical aerofoils. The Three-Component Balance (AFA3, 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. They can compare these results with the direct measurements from a balance. TecQuipment’s Smoke Generator (AFA10, not included) increases the educational value of the experiments by showing the flow of air around the model.

View the AF1300 experiment flyer here. 

Case Study
Texas A&M University Zachry Engineering Education Complex

Recently one of the USA’s largest engineering schools, Texas A&M University, invested in a new engineering education complex that would revolutionise the way they teach their 20,000 engineering students. One element of this new complex was a new model for laboratories that would allow them to fully utilise equipment and space by creating “common labs”,  shared facilities within Zachry Engineering Education Complex completed in 2018. The new building was only part of the story; they invested heavily in new teaching equipment to be housed in this facility, including a vast range of practical engineering teaching products from TecQuipment.

Read the full Case Study here.

NEED MORE INFORMATION?

We're here to answer your questions