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Tesi etd-05012011-151430
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Tipo di tesi Tesi di laurea specialistica
Autore VITI, ALBERTO
URN etd-05012011-151430
Titolo Structural design of a ULM PrandtlPlane wing system
Settore scientifico disciplinare INGEGNERIA, FACOLTA'
Corso di studi INGEGNERIA AEROSPAZIALE
Commissione
Nome Commissario Qualifica
Prof. Aldo frediani relatore
Dott. Ing. Vittorio Cipolla relatore
Parole chiave
  • structural
  • ULM
  • Plane
  • Prandtl
Data inizio appello 2011-06-14
Disponibilità unrestricted
Riassunto analitico
The task of the thesis is to optimize the wing structure of a non conventional very
light airplane starting from a Prandtl Plane prototype currently in phase of develop-
ment. This treatment is divided in several parts. In the rst part an introduction
about the main features of Prandtl Plane aircrafts is given.
In particular, the rst chapter explain what was the idea which led to this new
solution, its main advantages and the reasons which led to employ this con guration
in the branch of light aviation.
The second part depicts all the features of the prototype, in terms of regulation
observed, structures, materials used to build it, and loads that act on the structure.
The third part aims to the describe the optimization process and how the code used
to implement it works, starting from a previous tool and showing how this process can
be used in order to allows later development of this con guration.
Finally, in the third and last part of this job the results of the optimization pro-
cess will be veri ed through a nite element analysis, in order to allow a comparison
between the prototype and the optimized structure.
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