Aeronautics

Lecturer(s): Jérôme BOUDET, Laurent BLANC, Olivier DESSOMBZ

Objectives

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

Programme

  • Definition of architecture and thermodynamic cycle.
  • Preliminary design of the compression stages.
  • Detailed design of the compressor blades. 3D mechanical and flow simulations.
  • Shaft dynamics analysis.

Learning Outcomes

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

Assesment

Participation, report and oral presentation.