Aircraft Propulsion Systems

Module code: EMS614U

Credits: 15.0
Semester: SEM2

Contact: Dr Amin Paykani

This module will introduce concepts of propulsion and to show how thrust and fuel consumption can be calculated for a variety of propulsion systems at design and off conditions. It will cover the operation of
important components of propulsion systems (i.e. intakes, compressors, combustion chambers, turbines, and nozzles) and introduce the way in which materials constraints limit the performance, particularly of
turbines and compressors.

Connected course(s): UDF DATA
Assessment: 70.0% Examination, 30.0% Coursework
Level: 6