Introduction

Design of a turbofan engine, with aerodynamic and mechanical specifications. Multi-disciplinary project organization.

Keywords: turbofan engine, compressor, turbine, aerodynamics, thermodynamics, structural mechanics, shaft dynamics.

Requirements

MOS 1.1 or MOS 3.5 MOS 5.4 or MOS 7.1.

Career opportunities

Aeronautics, energy.

Managers

  • Jérôme BOUDET
  • Laurent BLANC
  • Olivier DESSOMBZ

Credits

ECTS