WAGNER: a new code for parametrical structural study of fuselages of civil transport aircraft

Aerotecnica Missili & Spazio

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Title WAGNER: a new code for parametrical structural study of fuselages of civil transport aircraft
 
Creator Picchi Scardaoni, Marco
Binante, Vincenzo
Cipolla, Vittorio
 
Subject Aircraft Structures; Aircraft Design; Preliminary aircraft design
FEM; PrandtlPlane; fuselage; PrP; Parsifal project; parametric code
FEM
 
Description In the present paper, a new code (named WAGNER) for a parametric and automatic Finite Element mesh generation of fuselages of civil transport aircraft is presented. The code aims at providing a time saving and reliable tool in the conceptual design phase in order to evaluate stresses and deformations in the whole fuselage structure; these data allows us a preliminary structural sizing to be used as a baseline for deeper investigations and to determine the empty weight of the fuselage in view of a preliminary prediction of the maximum take-off weight of the aircraft. As an example of application, two layouts have been analysed: a non conventional two aisle single-deck (SD) with 2-4-2 passengers abreastand a double-deck (DD) with 3-3 passengers abreast/deck. FEM results for two different load cases (combined loads at limit load factor and ultimate pressurization) with geometrical linear and non-linear solutions, are finally discussed.
 
Publisher Associazione Italiana di Aeronautica e Astronautica (AIDAA)
 
Contributor
 
Date 2017-12-29
 
Type info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
Peer-reviewed Article
Numerical; Simulation
 
Format application/pdf
 
Identifier http://131.114.27.37/index.php/AMS/article/view/311
10.19249/ams.v96i3.311
 
Source Aerotecnica Missili & Spazio; Vol 96, No 3 (2017); 136-147
0365-7442
 
Language eng
 
Relation http://131.114.27.37/index.php/AMS/article/view/311/pdf
http://131.114.27.37/index.php/AMS/article/downloadSuppFile/311/9
 
Rights Copyright (c) 2017 Aerotecnica Missili & Spazio
 

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