Publication detail
THE INFLUENCE OF MATERIAL AND GEOMETRIC NON-LINEARITIES TO ACCURANCY FEM STRESS ANALYSIS OF LANDING GEAR
PÍŠTĚK, A. PLHAL, M.
English title
THE INFLUENCE OF MATERIAL AND GEOMETRIC NON-LINEARITIES TO ACCURANCY FEM STRESS ANALYSIS OF LANDING GEAR
Type
Paper in proceedings (conference paper)
Language
en
Original abstract
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.
Keywords in English
aircraft design, stress analysis, landing gear, structural mechanics, structural testing
Released
2004-01-01
Publisher
Optimage Ltd., Edinburgh,UK
Location
Yokohama
ISBN
0-9533991-6-8
ISSN
1213-4198
Book
ICAS 2004 PROCEEDINGS
Journal
Vědecké spisy Vysokého učení technického v Brně Edice PhD Thesis
Volume
2002
Number
137
Pages from–to
511–
Pages count
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"
}