Aircraft propulstion systems. [ LMECA2550 ]
4.0 crédits ECTS
30.0 h + 15.0 h
1q
Teacher(s) |
Chatelain Philippe ;
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Language |
French
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Place of the course |
Louvain-la-Neuve
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Prerequisites |
MECA 1855 Thermodynamique et énergétique
MECA 2322 Mécanique des fluides et transferts 2 (can be taken simultaneously)
MECA 2323 Aérodynamique (recommanded)
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Main themes |
1. Fundamentals of air-breathing propulsion
1.1) Dynamical and energetic aspects
1.2) Concepts and domains of use
2. Analysis of propulsion systems
2.1) The airscrew
2.2) The jet engine
2.3) The Ramjet and Scramjet engines
2.4) Inlets and nozzles
2.5) Technological aspects
3. Advanced concepts and future trends
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Aims |
Aims to provide an analytical description of systems used in aircraft propulsion, to model their behaviour and to introduce students to performance evaluation and component dimensioning.
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Evaluation methods |
Written exam in 2 parts: 1) theoretical questions and 2) exercises
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Teaching methods |
Course notes are being prepared and will be made available in electronic format during the term.
Lecture slides will also be available
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Content |
1. Fundamentals of air-breathing propulsion
1.1) Dynamical and energetic aspects
1.2) Concepts and domains of use
2. Analysis of propulsion systems
2.1) The airscrew
2.2) The jet engine
2.3) The Ramjet and Scramjet engines
2.4) Inlets and nozzles
2.5) Technological aspects
3. Advanced concepts and future trends
|
Cycle et année d'étude |
> Master [120] in Mechanical Engineering
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Faculty or entity in charge |
> MECA
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