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| AERO0014-1

 | Aeronautic and Space Propulsion

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| Duration : | 30h Th, 30h Pr | |
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| Credits/ECTS : |
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| Holder(s) : | Olivier Léonard | |
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| Course contents :
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- 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.
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| Course objective :
| 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.
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| Prerequisites :
| Thermodynamics, Heat Transfers and Fluid Mechanics | |
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| Workshops :
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- 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.
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| Organization :
| 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. | |
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| Written notes :
| 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. | |
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| Assessment :
| 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. | |
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| Contacts :
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