Goals

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

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.

Code

23_I_G_S09_PR3_1

Responsibles

  • Jérôme BOUDET
  • Laurent BLANC
  • Olivier DESSOMBZ
  • Stéphane Aubert

Language

English

Keywords

turbofan engine, compressor, turbine, aerodynamics, thermodynamics, structural mechanics, shaft dynamics