Landing Gear FEM Analysis and Comparative Testing Considering the Material and Geometric Non- Linearities

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F99%3A00000022" target="_blank" >RIV/00216305:26210/99:00000022 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Landing Gear FEM Analysis and Comparative Testing Considering the Material and Geometric Non- Linearities

Original language description

The certification processes require the structural testing of all parts. It means that each modificatio should be verified by a structural test. tehe aero nautical regulations for the aircraft from category FAR23 and JAR23 provide a possibility to certify the aircraft component without verification by structural test on condition that the employed analysis was proved reliable in the past for a very similar component. the aim of our research was to confirm the reliability of two landing gears FEM modelsto reduce time and costs necessary for their development.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/FB-CV%2F20" target="_blank" >FB-CV/20: The Centre of Aeronautical Research and Testing.</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

1999

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Letecký zpravodaj 3/99

ISSN

1211-877X

e-ISSN

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Volume of the periodical

99

Issue of the periodical within the volume

3

Country of publishing house

US - UNITED STATES

Number of pages

4

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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