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Tesi etd-06252020-112854


Tipo di tesi
Tesi di laurea magistrale
Autore
MICHELI, BORIS
URN
etd-06252020-112854
Titolo
A NEW APPROACH FOR LOADING A FUSELAGE STRUCTURE
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Cipolla, Vittorio
tutor Dott. Loukota, Juan
supervisore Ing. Soru, Giovannantonio
Parole chiave
  • aerodynamic loads
  • aeroelasticity
  • CFD
  • FEM
  • fuselage
  • inertial loads
  • loads
  • MAC
  • modal analysis
Data inizio appello
14/07/2020
Consultabilità
Non consultabile
Data di rilascio
14/07/2090
Riassunto
General Information: The study was developed in the context of a seven month long internship held at the Gust Loads and Aeroelastics team of Airbus in Hamburg.

Topic: During this internship, a new modeling strategy has been proposed to idealize the fuselage from a dynamic perspective. This new dynamic model has allowed to handle non-structural masses and to take into account the flexibility of the section of the fuselage in loads estimation.
The feasibility of the model has been proved performing a full Aeroelastic Gust Loads computation with the FE dynamic model coupled to a LFD (Linearized Frequency Domain) Aerodynamic model to consider unsteady aerodynamic effects.
After the selection of the sizing cases, a new approach to recover loads and subsequent loading the FEM considering the local introduction of inertial loads has been proposed, thus ensuring coherence between the loads computation and the loading of the FEM for the following sizing process.
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