FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F13%3APU104190" target="_blank" >RIV/00216305:26210/13:PU104190 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure
Original language description
The article describes the evaluation of a progress of stiffness changes and stability failures of the fuselage structure. The two non-linear FE analyses were proved for a purpose of the stability and strength analysis of the L 410 NG aircraft. The results of the FE analyses and the additional analytical analysis were compared with the results of the static strength test. For the material non-linear characteristics, large deformations and the complex structure of the metal thin-walled fuselage the effectof used non-linear solvers, methods and input parameters were investigated.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
New Trends in Civil Aviation 2013
ISBN
978-80-7204-843-4
ISSN
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e-ISSN
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Number of pages
3
Pages from-to
90-92
Publisher name
Akademické nakladatelství CERM Brno
Place of publication
Brno
Event location
University of Žilina
Event date
Jun 21, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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