Résumé:
The purpose of this thesis is the study, design and installation of measuring equipment for a subsonic Wind Tunnel. The measuring equipment is mainly digital and that is to accomplish as much precision as possible in the results obtained in the wind tunnel.
The testing will consist of measuring the aerodynamic properties and the wind speed when it comes to various aerofoils and wings designed and made by our team. In addition to that, the goal is to be able to do the measuring simultaneously.