Duration
30h Th, 30h Pr
Number of credits
| Master in aerospace engineering (120 ECTS) | 5 crédits |
Lecturer
Substitute(s)
Coordinator
Language(s) of instruction
English language
Organisation and examination
Teaching in the second semester
Units courses prerequisite and corequisite
Prerequisite or corequisite units are presented within each program
Learning unit contents
- Action, reaction, propulsion. Historical perspectives and classification of propulsive systems.
- Compressible flows : thermodynamic losses, Fanno and Rayleigh problems, thrust developed by an engine.
- Caracterization of the main components : intakes, compressors, turbines, fans, combustors, nozzles, propellers.
- Jet engines : nominal performances, off-design performances, transients, turbine cooling.
- Rocket engines : performances, nozzle sizing, thermochemistry of the combustion chamber, chemical reactions in the nozzle, selection of the propergols.
Learning outcomes of the learning unit
The objectives of this course are
- to understand how a propulsion system is conceived according to its mission, to the technological limits and to the operating conditions,
- to understand what influences its peformances and how they can be determined.
Prerequisite knowledge and skills
Thermodynamics, Heat Transfers and Fluid Mechanics
Planned learning activities and teaching methods
- Projects are organized by groups of two students. They consist in carrying out a preliminary draft of turbojet that must achieve required performances.
- A laboratory session is organized in order to test a small turbojet, to acquire and to analyse measurements of pressure, temperature, rotational speed, thrust and flow rates.
Mode of delivery (face-to-face ; distance-learning)
This course is organized throughout the second half of the academic year, by 4 hour sessions, at a rate of about 30 hours of theory and 15 hours of exercises.
Recommended or required readings
Course notes are available, as well as a collection of solved exercises. These notes are regularly updated and are distributed during the course. Reference books are proposed. The slides are in English.
Assessment methods and criteria
An oral examination on the theory is organized in June (1st session) and September (2nd session). The project is subject to a report which is also evaluated.
Work placement(s)
Organizational remarks
Contacts
To come
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