Development of a subsonic wind tunnel for academical usageAircraft Design
Unlimited aerobatic airplane (215 hp).
Single engine aircraft (65 hp) that fits in the category FAI c.1-a0 (maximum takeoff weight of 300 kg).
Low wing airplane (115 hp), with retractable landing gear, wood and composites structure, biplace, fully aerobatic when transporting one person.
Light Airplane (80 hp), low wing, tricicle landing gear, wood and composite structure, biplace. An evolution of Curumim project.
The Brazilian Association of Experimental Aviation (ABRAEX) and CEA firmed an unprecedent partnership on behalf of light airplane aviation, the design of the ABRAEX-6. An airplane matching the requirements of brazilian sport aviation.
Group that designs and builds light radio-controlled airplanes for SAE AeroDesign competition.
Check the students' reports for the Aircraft Design Course at UFMG (in portuguese).
SiDeVAAN Project
Development of Unmanned Aerial Vehicles. Partnership between CEA, Verlab-DCC and MACSIM-DELT.
Wind Tunnel
Development of a subsonic wind tunnel for academical usage