5 ECTS credits
145 u studietijd

Aanbieding 1 met studiegidsnummer 4016329FNR voor alle studenten in het 1e semester met een gespecialiseerd master niveau.

Semester
1e semester
Inschrijving onder examencontract
Niet mogelijk
Beoordelingsvoet
Beoordeling (0 tot 20)
2e zittijd mogelijk
Ja
Inschrijvingsvereisten
Registration for Aircraft Performance and Stability is allowed if one has successfully accomplished or is registered for Aerodynamics and 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
Elmar Recker
Axel Coussement (titularis)
Onderdelen en contacturen
32 contacturen Hoorcollege
28 contacturen Werkcolleges, practica en oefeningen
Inhoud

The valid fiche can be found at the following link : https://www.ulb.be/en/programme/meca-h506-1

Aerodynamics and performance of aircraft

- Performance parameters : Coventions, Forces, Fundamental Parameters, Governing equations

- Steady flight : Symmetric flight, Parameters affecting performance curves, Climbing performance, Descending performance

- Accelerated flight : Accelerated straight level flight, Load factor, Turning flight, Accelerated climbs, Total energy, Flight envelope, Takeoff, Landing

- Stick-fixed and stick-free static stability, longitudinal stability, lateral static stability. General equations of motion, linearization around a steady flight configuration. Aerodynamic derivatives. Longitudinal dynamic stability : phugoid and short-period oscillation. Lateral dynamic stability. Response to controls.

Bijkomende info

References : Aerodynamics and performance of aircraft

- Asselin Mario 'An Introduction to Aircraft Performance';
- Corke Thomas 'Design of Aircraft';
- Cumpsty Nicholas 'Jet propulsion';
- Stengel Robert 'Flight Dynamics';
- Yechout Thomas 'Introduction to aircraft flight mechanics'
- G. Degrez 'Performances et stabilité des avions', Note de cours, 3e édition, printemps 2007
- B. Etkin 'Dynamics of atmospheric flight', Dover publications, 2009 (reprinted from original 1972 edition)
- B. Etkin & L.D. Reid 'Dynamics of flight. Stability and Control', Wiley, 1995

 

Leerresultaten

Algemene competenties

 

Aerodynamics and performance of aircraft

At the end of the course, it is expected from the student that :

- he describes the performance of an aircraft;

- he calculates the performance parameters;

- he is able to evaluate the longitudinal static stability characteristics (static margin) of an aircraft;

- he is able to compute the longitudinal and lateral modes of motion characteristics of an aircraft;

- he can describe the major aerodynamic mechanisms in action for each of the aerodynamic derivatives.

 

Attitudes

Having the flexibility and adaptability to work in an international and/or intercultural context.

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 the advanced methods and theories to schematize and model complex problems or processes.

Knowledge oriented competences

Having an in-depth scientific knowledge, understanding and skills in at least one of the subfields needed to design, produce, apply and maintain complex mechanical, electrical and/or energy systems.

Scientific competences

Can reformulate complex engineering problems in order to solve them (simplifying assumptions, reducing complexity).

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 collaborate in a (multidisciplinary) team.

Attitudes

Having a creative, problem-solving, result-driven and evidence-based attitude, aiming at innovation and applicability in industry.

Attitudes

Having a critical attitude towards one's own results and those of others.

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 final grade is composed based on the following categories :

- Other Exam determines 100% of the final mark.
Within the Other Exam category, the following assignments need to be completed :

The mark results from the combination of the following partial marks :
- Written test (performance exercises) : 20%
- Oral exam (performance theory) : 20%
- Written test (stability & control theory & exercises) : 40%
- Project report : 20%

Additional info with regard to grading

The number of tests/tasks and the weight factors for the daily work and the exam are only determined for the main course : Aerodynamics, performance and stability of aircraft

Daily work : One project report

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)