Casos de Estudio

Milton Keynes College Takes Off with TecQuipment AF1300 Wind Tunnel

The electronic and aeronautical test facility at Milton Keynes College, UK recently purchased an AF1300 Subsonic Wind Tunnel for the teaching of the Level 3 Aeronautical Engineering BTEC Diploma students, which is used on a regular basis as part of the course.

  • AF1300 Subsonic Wind Tunnel
Milton Keynes College May 2018 Btec Aero Engineering Students With Af1300

Addressing the Aeronautical Engineering Skills Shortage

In response to the world skills shortage of aeronautical engineers, in 2016 Milton Keynes College began a dedicated Aeronautical Engineering BTEC. This course, headed up by Sean Hainsworth, former RAF Aerospace Engineer, first began as a trial. Following the course’s success, Milton Keynes College has a full cohort of 40 applicants aiming to start in September 2018.

Wind Tunnel in the Syllabus

Students are required to complete projects that involve the design, manufacture and test of aerofoils throughout the year. As part of the course, students have a project to design and build three types of aerofoil, testing with three angles in the wind tunnel (0 degrees, 5 degrees and the critical 15 degree stall angle) and then applying three different equations (lift, drag and wind speed).

Pearson BTEC Level 3 Diploma in Aeronautical Engineering

The AF1300 Subsonic Wind Tunnel is used as a standard piece of equipment in specialist aeronautical engineering facilities across the globe. For the Pearson BTEC Level 3 Diploma in Aeronautical Engineering, the equipment utilised for the following learning units:

  • Unit 5 Mechanical Principles and Applications
  • Unit 48 Theory of Flight
  • Unit 68  Principles and Applications of Aircraft Mechanical Science




About the AF1300 Subsonic Wind Tunnel

The AF1300 is a widely used piece of aerospace engineering teaching equipment that allows undergraduate and research students to study the principles of aerodynamics. The compact size reduces space requirements and experiment time compared to full sized wind tunnels, due to the ease of model changeover, of which can be switched with minimal or no supervision. The wind tunnel is available with a range of different models (standard cylinder, NACA standard aerofoils, 3D drag models, flat plate drag models, flat plate boundary layer models with tapings and aircraft models with low and high wing configurations). For more information, click here