Detail publikace

THE INFLUENCE OF MATERIAL AND GEOMETRIC NON-LINEARITIES TO ACCURANCY FEM STRESS ANALYSIS OF LANDING GEAR

PÍŠTĚK, A. PLHAL, M.

Anglický název

THE INFLUENCE OF MATERIAL AND GEOMETRIC NON-LINEARITIES TO ACCURANCY FEM STRESS ANALYSIS 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. The certification processes require the structural testing of all parts.

Klíčová slova anglicky

aircraft design, stress analysis, landing gear, structural mechanics, structural testing

Vydáno

2004-01-01

Nakladatel

Optimage Ltd., Edinburgh,UK

Místo

Yokohama

ISBN

0-9533991-6-8

ISSN

1213-4198

Kniha

ICAS 2004 PROCEEDINGS

Časopis

Vědecké spisy Vysokého učení technického v Brně Edice PhD Thesis

Ročník

2002

Číslo

137

Strany od–do

511–

Počet stran

6

BIBTEX


@inproceedings{BUT7308,
  author="Antonín {Píštěk} and Martin {Plhal}",
  title="THE INFLUENCE OF MATERIAL AND GEOMETRIC NON-LINEARITIES TO ACCURANCY FEM STRESS ANALYSIS OF LANDING GEAR",
  booktitle="ICAS 2004 PROCEEDINGS",
  year="2004",
  journal="Vědecké spisy Vysokého učení technického v Brně 
Edice PhD Thesis",
  volume="2002",
  number="137",
  pages="6",
  publisher="Optimage Ltd., Edinburgh,UK",
  address="Yokohama",
  isbn="0-9533991-6-8",
  issn="1213-4198"
}