Duration
26h Th, 26h Pr
Number of credits
| Master of Science (MSc) in Aerospace Engineering | 5 crédits |
Lecturer
Language(s) of instruction
English language
Organisation and examination
Teaching in the second semester
Schedule
Units courses prerequisite and corequisite
Prerequisite or corequisite units are presented within each program
Learning unit contents
- Compressible flows : thermodynamic losses, Fanno and Rayleigh problems, flow in the de Laval nozzle, thrust developed by an engine.
- Propulsion force and energy balance, performance parameters and classification of propulsive systems.
- Propellers: operating principles and characteristics, regulation and power shafts;
- Jet engines : engine types, nominal and off-design performances, operation limits, transients;
- Jet engine component technology: intakes, compressors, turbines, fans, combustors, nozzles;
- Recent evolutions in civil aviation and impact on turbofan technology;
- Rocket engines : performances, nozzle sizing, thermochemistry of the combustion chamber, chemical reactions in the nozzle, selection of the propergols;
- Electric propulsor classification and operating principles;
- Elements of scientific computation for the numerical resolution of the exercises.
Learning outcomes of the learning unit
The objectives of this course are to provide the student with
- the understanding of how a propulsion system is chosen and conceived according to its mission, to the technological limits and to the operating conditions;
- the comprehension of what influences its performances;
- the ability to estimate the operating point of the engine and the performance parameters;
- the ability to write small programs needed for computing estimates.
Prerequisite knowledge and skills
Thermodynamics, Heat Transfer and Fluid Mechanics
Planned learning activities and teaching methods
Mode of delivery (face to face, distance learning, hybrid learning)
Face-to-face course
Additional information:
The course is organised the whole quadrimester following sessions of 3h to 3h30 of theory and 30' to 1h of exercises. As the exercises are ment to be solved autonomously by the student, the latter consist mainly of Q&A, complemented by an introduction to the programming of computation scripts and the resolution of a few typical exercises.
Recommended or required readings
The course materials are available in electronic format on the e-campus site of the course. They include:
- Course notes; this year these will still be subject to regular updates;
- A collection of exercises including resolved exam exercises;
- Other standard works are referenced in the notes and made available if possible;
- Fora supporting discussions on the theory and exercises.
Assessment methods and criteria
Exam(s) in session
Any session
- In-person
written exam ( open-ended questions ) AND oral exam
- Remote
written exam ( open-ended questions ) AND oral exam
Additional information:
An oral examination on the theory and a written exercise exam is organized in June (1st session) and September (2nd session).
Work placement(s)
Organizational remarks
Contacts
- Teacher : Koen Hillewaert (koen.hillewaert@uliege.be)
- Assistent : Thomas Lambert (t.lambert@uliege.be)
Items online
Aerospace Propulsion course notes 2017-2018
Course notes for Aerospace Propulsion 2017-2018
Operating points and operating lines 2017-2018
Operating points and operating lines
WP & SSL Figures
WP & SSL Figures