Detail publikace

The influence of material and geometric non-linearity to accuracy FEM stress analyses of landing gear

PÍŠTĚK, A. PLHAL, M.

Anglický název

The influence of material and geometric non-linearity to accuracy FEM stress analyses of landing gear

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

Originální abstrakt

The paper provides description of FEM stress analysis of several landing gears for new Czech aircraft. In all loading cases, there is considered material and geometric non-linearity, contacts and friction between some parts of landing gear and carried out verification of analysis results with comparative testing. The structural tests of the landing gears of Zlín Z143-L, small GA and aerobatics plane and KP2U-Sova, an ultralight plane , were tested in the IAE laboratory. The structural test of nose and main landing gear of Aero Vodochody s new commuter were tested in test laboratory of Technometra Radotín, the Czech producer of landing gear.

Klíčová slova anglicky

FEM, aircraft, stress analysis

Vydáno

2002-04-10

Nakladatel

MSC. Software

Místo

Toulouse

Kniha

WORLDWIDE AEROSPACE CONFERENCE AND TECHNOLOGY SHOWCASE 2002

Strany od–do

77–

Počet stran

8

BIBTEX


@inproceedings{BUT6961,
  author="Antonín {Píštěk} and Martin {Plhal}",
  title="The influence of material and geometric non-linearity to accuracy FEM stress analyses of landing gear",
  booktitle="WORLDWIDE AEROSPACE CONFERENCE AND TECHNOLOGY SHOWCASE 2002",
  year="2002",
  pages="8",
  publisher="MSC. Software",
  address="Toulouse"
}