AE613E - Aircraft architecture and load calculation
Objectifs
Objectif général :
To be able to use the methods and means of calculating load distribution in the various parts of an aircraft (wings, fuselage, landing gear, etc.) as a function of its multiple operating phases, in order to determine the sizing of the structures
Objectifs détaillés :
Architecture and calculation of structures
- Wings and control surfaces
- Fuselage
- Assemblies
- Design philosophy
Calculation of loads
- In-flight loads
- Flight envelope
- Symmetrical manoeuvres
- Dissymetrical manoeuvres
- Gusts
- Ground loads
- Landing
- Ground manoeuvers
Fatigue of aeronautical structures
- Damage tolerance
Visit to the structures activity of Direction Générale de l’Armement techniques Aéronautiques (DGATA)
Volume horaire (h)
- Cours magistraux : 18
- Travaux dirigés : 12
Ce cours fait partie de la formation
En bref
Crédits ECTS : Cf UE
Nombre d'heures 30
Langue d'enseignement
Anglais