Detail publikace

FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure

SYMONOV, V. KATRŇÁK, T.

Originální název

FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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 effect of used non-linear solvers, methods and input parameters were investigated.

Klíčová slova

thin-walled stiffened structure, aircraft fuselage, non-linear analysis, FEM, FEA, local and global buckling

Autoři

SYMONOV, V.; KATRŇÁK, T.

Rok RIV

2013

Vydáno

21. 6. 2013

Nakladatel

Akademické nakladatelství CERM Brno

Místo

Brno

ISBN

978-80-7204-843-4

Kniha

New Trends in Civil Aviation 2013

Edice

1

Číslo edice

1

Strany od

90

Strany do

92

Strany počet

3

BibTex

@inproceedings{BUT100420,
  author="Volodymyr {Symonov} and Tomáš {Katrňák}",
  title="FEM Approach to Estimate Large Deformations of Stiffened Fuselage Structure",
  booktitle="New Trends in Civil Aviation 2013",
  year="2013",
  series="1",
  number="1",
  pages="90--92",
  publisher="Akademické nakladatelství CERM Brno",
  address="Brno",
  isbn="978-80-7204-843-4"
}