Thesis etd-09222010-151820 |
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Thesis type
Tesi di laurea specialistica
Author
QUATTRONE, FLAVIO
URN
etd-09222010-151820
Thesis title
Preliminary design and FEM analysis of a new
conception non-standard wing structure: the
PrandtlPlane 250 wing structure
Department
INGEGNERIA
Course of study
INGEGNERIA AEROSPAZIALE
Supervisors
relatore Prof. Vannucci, Paolo
relatore Prof. Frediani, Aldo
relatore Prof. Frediani, Aldo
Keywords
- Nessuna parola chiave trovata
Graduation session start date
12/10/2010
Availability
Withheld
Release date
12/10/2050
Summary
The purpose of this thesis is to verify with a FEM analysis a preliminary
design of the PrP250 wing structure, made up in aluminum and previously
optimized with a multistep process shortly presented in chapter 3. Moreover,
a composite design of the structure is here investigated, with a preliminary
sizing of the wing, a FEM analysis and the checking of upper skin panels
buckling is accomplished. The results in term of weight and stress distribu-
tion are then shown, and a comparison between the two solutions is made.
design of the PrP250 wing structure, made up in aluminum and previously
optimized with a multistep process shortly presented in chapter 3. Moreover,
a composite design of the structure is here investigated, with a preliminary
sizing of the wing, a FEM analysis and the checking of upper skin panels
buckling is accomplished. The results in term of weight and stress distribu-
tion are then shown, and a comparison between the two solutions is made.
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