Aerodynamics and Combustion - 5EUS5AIE
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Goals
The module is structured around 2 courses: “Applied aerodynamics”, dedicated to the external aerodynamics and “Combustion”.
Content Applied aerodynamics
Objective: The course goes through all the basic concepts of aerodynamics for engineers, focusing on the external aerodynamics of aircraft.
Content: Aerodynamic forces. Aerodynamic characteristic of aircraft. Shockwaves. Transonic flows. Swept wing. Delta wing. Boundary layer. Hyperlift. Air intakes. Challenges of current warplanes. Aerodynamics outside aircraft.
The course of combustion presents the fundamental principles of combustion, with an application to aerospace propulsion
PrerequisitesModélisation et analyse d’écoulements 1
Modélisation et analyse d’écoulements 2,
Heat and Mass transfers
Tests - Specific credits: this course brings 6.0 ECTS to students in Year 2 Master Fluid Mechanics and Energetics (M2 FME)
First session
ER assessment : 3 hours supervised written exam (1H30 aéro / 1H30 combustion)
EN assessment : 2 homeworks (1 on aéro + 1 on combustion)
If distant learning mandatory:
ER assessment : 3 hours remote written exam (1H30 aéro / 1H30 combustion)
EN assessment : 2 homeworks (1 on aéro + 1 on combustion)
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Second session
2 hours supervised written exam (1H aéro / 1H combustion)
EN 30% + ER 70%
The exam is given in english only 
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Date of update February 8, 2017