Specialization Aeronautics

Director: Jérôme BOUDET, Laurent BLANC, Olivier DESSOMBZ
74 hTD

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.

Learning Outcomes

  • Formulate an engineering problem.
  • Use knowledge and know-how for the detailed design of a system.

Programme

Requirements

MOS 1.1 or MOS 3.5 MOS 5.4 or MOS 7.1.

Assesment

Participation, written report and defense