5 ECTS credits
130 u studietijd

Aanbieding 1 met studiegidsnummer 4016327FNR voor alle studenten in het 2e semester met een gespecialiseerd master niveau.

Semester
2e semester
Inschrijving onder examencontract
Niet mogelijk
Beoordelingsvoet
Beoordeling (0 tot 20)
2e zittijd mogelijk
Ja
Inschrijvingsvereisten
Registration for Aircraft Conceptual Design is allowed if one has successfully accomplished or is registered for 30 ECTS of (semi)common courses of the Master in Electromechanical Engineering, AE track (Dutch program idem).
Onderwijstaal
Engels
Onder samenwerkingsakkoord
Onder interuniversitair akkoord mbt. opleiding
Faculteit
Faculteit Ingenieurswetenschappen
Verantwoordelijke vakgroep
Toegepaste Mechanica
Externe partnerinstelling(en)
Université libre de Bruxelles
Onderwijsteam
Patrick Hendrick (titularis)
Onderdelen en contacturen
24 contacturen Hoorcollege
36 contacturen Werkcolleges, practica en oefeningen
Inhoud

The valid fiche can be found at the following link : MECA-H508. Change the language to English in the dropdown menu on top of the page.

This course is intended to focus on a first "system study" at the level of an aircraft for the students in aeronautical engineering. This course integrated a lot of matters that have been taught during the BA, the MA1 and the first part of the MA2 and these matters are now applied on a real case study integrating all of them.

24 hours of theory are given with a description of the different steps into the design process of an aircraft.  36 hours are devoted to the aircraft design project of the student working in a design team of 3-4-5 students supervised by a leader (depending on the aircraft and the number of students).

Bijkomende info

References : Thomas Corke, Design of aircraft / Daniel Raymer, Aircraft design : a conceptual approach

Course notes : course material is distributed to the students by the professor.  The tutorial and theory explanation of the software used (ADS) is also available.

Leerresultaten

Algemene competenties

After 4 and 1/2 years of the engineering degree including 1.5 year of the Master degree, the student will learn in this course and in the related aircraft design project to apply to a complete case study the different specialties he learnt in the aeronautical domain.

He will be able to visualize at the end the aircraft he has designed and to check its performance and its flight qualities.

The course is also intended to force the student to work in a small design team with other students under the supervision of a design leader who is the professor or the assistant.

An important feature is to be able to analyze the pro's and cons of the different design choices that the student will have to do at the level of a complete system and to do trade-off analysis of his proposed solutions.

Knowledge oriented competences

Having in-depth knowledge and understanding of exact sciences with the specificity of their application to engineering.

Knowledge oriented competences

Having in-depth knowledge and understanding of integrated structural design methods in the framework of a global design strategy.

Knowledge oriented competences

Having in-depth knowledge and understanding of the advanced methods and theories to schematize and model complex problems or processes.

Knowledge oriented competences

Having a broad scientific knowledge, understanding and skills to be able to design, produce and maintain complex mechanical, electrical and/or energy systems with a focus on products, systems and services. E.g. codepo project, courses around renewable, sustainable mobility,...

Knowledge oriented competences

Having an in-depth understanding of safety standards and rules with respect to mechanical, electrical and energy systems.

Scientific competences

Can correctly report on research or design results in the form of a technical report or in the form of a scientific paper.

Scientific competences

Can present and defend results in a scientifically sound way, using contemporary communication tools, for a national as well as for an international professional or lay audience.

Beoordelingsinformatie

De beoordeling bestaat uit volgende opdrachtcategorieën:
Examen Andere bepaalt 100% van het eindcijfer

Binnen de categorie Examen Andere dient men volgende opdrachten af te werken:

  • exam met een wegingsfactor 1 en aldus 100% van het totale eindcijfer.

Aanvullende info mbt evaluatie

The evaluation is based on an individual oral presentation of the aircraft design project done by the student and on his written report delivered after this project.

Toegestane onvoldoende
Kijk in het aanvullend OER van je faculteit na of een toegestane onvoldoende mogelijk is voor dit opleidingsonderdeel.

Academische context

Deze aanbieding maakt deel uit van de volgende studieplannen:
Master in de ingenieurswetenschappen: werktuigkunde-elektrotechniek: lucht- en ruimtevaart
Master of Electromechanical Engineering: Aeronautics (enkel aangeboden in het Engels)