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.
MOS 1.1 or MOS 3.5 MOS 5.4 or MOS 7.1.
[Please refer to the prerequisite list given by the registrar when the course choice opens]
Aeronautics, energy.