Abstract

In this work, a scheme of representation of structural concepts for the aeronautical field is identified. It is based on an original set of 2D and 3D primitives, representing the main structural components of the aeronautical concept. Starting from them, an associative parametric geometrical modelling of the aeronautic structure, consisting in a quad-mapped mesh, is obtained. The automatic propagation of modifications is implemented so that several structural concepts can be efficiently modelled and modified during the very early phases of the design process. The propagation process aims at the automatic regeneration of the whole mesh thanks to a well-defined hierarchy (or relationship of dependences) among the parametrically defined primitives. Based on the above-mentioned considerations, a CAD/CAE tool, called MeshFEM, has been developed using C++ and Matlab languages and the VTK library for the 3D graphic visualization.

Autore Pugliese

• Morabito Anna , Dattoma Vito

Tutti gli autori

• V. Dattoma , M. De Giorgi , S. Giancane , P. Manco , A.E. Morabito

Titolo volume/Rivista

Non Disponibile

Anno di pubblicazione

2010

ISSN

Non Disponibile

ISBN

Non Disponibile

Numero di citazioni Wos

Nessuna citazione

Ultimo Aggiornamento Citazioni

Non Disponibile

Numero di citazioni Scopus

Non Disponibile

0

Ultimo Aggiornamento Citazioni

26/04/2018

Settori ERC

Non Disponibile

Codici ASJC

Non Disponibile