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| AERO0023-1 | Aircraft design
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| Duration : | 30h Th, 30h Pr |
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| Number of credits : |
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| Lecturer : | Grigorios Dimitriadis, Ludovic Noels |
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Language(s) of instruction :
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| French language |
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Course contents :
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| During these classes, the students will learn about the integrated design of an aircraft. Indeed, each technical field is seen as a sub-system interacting with the others.
Therefore, the organisation is as follows. An introductive talk describes, through history, these interactions, and a concluding talk will introduce the project of designing an aircraft.
Between these two classes, professors will introduce the concepts of
- Aerodynamics
- Structures
- Propulsion (flow and mechanical design)
- Performances
- Stability
- Aeroelasticity
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Learning outcomes of the course :
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| To acquire the methodology to conduct a conceptual design in aeronautics. |
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Prerequisites and co-requisites/ Recommended optional programme components :
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| Elementary knowledge in
- Solid mechanics
- Fluid mechanics
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Planned learning activities and teaching methods :
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| Industrial partners are invited to give lectures during which they illustrate the theoretical concepts with realizations of aeronautic companies. |
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Mode of delivery (face-to-face ; distance-learning) :
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| Face to face |
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Recommended or required readings :
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| Aircraft Design: Synthesis and Analysis, Ilan Kroo, Stanford University, http://adg.stanford.edu/aa241/AircraftDesign.html (http://adg.stanford.edu/aa241/AircraftDesign.html) |
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Assessment methods and criteria :
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| The evaluation is based on a project, which consists in the pre design of a turbojet. This project will be presented in front of the professors and the classmates.
Participation to the talks of the invited lecturers and to the project presentations is mandatory. |
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Organizational remarks :
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| Classes are taught during first term; project is accomplished during the 2 terms and is presented during the 2nd term. |
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| Items online : |
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