The work presented in this thesis focuses on the design layout and analysis of some components of the Merlo, an experimental ultralight aircraft conceived at the University of Padova. In the first chapter, the wing geometry has been presented. An aerodynamic analysis on wings and tail has been carried out with cfd. The pressure distribution has been exported into to a FEM structural analysis of the wing, in the second chapter. In the third chapter, the landing gear has been sized with FEM
Progettazione aerodinamica e strutturale di alcuni componenti di un velivolo ultraleggero
Scalchi, Matteo
2014/2015
Abstract
The work presented in this thesis focuses on the design layout and analysis of some components of the Merlo, an experimental ultralight aircraft conceived at the University of Padova. In the first chapter, the wing geometry has been presented. An aerodynamic analysis on wings and tail has been carried out with cfd. The pressure distribution has been exported into to a FEM structural analysis of the wing, in the second chapter. In the third chapter, the landing gear has been sized with FEMFile in questo prodotto:
File | Dimensione | Formato | |
---|---|---|---|
Matteo_Scalchi_1040030_-_Tesi_di_Laurea_Magistrale.pdf
accesso aperto
Dimensione
2.49 MB
Formato
Adobe PDF
|
2.49 MB | Adobe PDF | Visualizza/Apri |
The text of this website © Università degli studi di Padova. Full Text are published under a non-exclusive license. Metadata are under a CC0 License
Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/17927