Aeronautics

Director: Olivier DESSOMBZ
74 hTD

Introduction

Design of a turbojet engine, with aerodynamic and mechanical specifications. Multi-disciplinary project organization. Keywords: turbojet engine, compressor, turbine, aerodynamics, thermodynamics, structural mechanics, ensemble dynamics

Learning Outcomes

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

Programme

Assesment

Participation, written report and defense