Fatigue analyses and optimization of L 410 NG aircraft

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F16%3APU122180" target="_blank" >RIV/00216305:26210/16:PU122180 - isvavai.cz</a>

Result on the web

<a href="http://www.czaerospace.eu/en/2016-02-56.html" target="_blank" >http://www.czaerospace.eu/en/2016-02-56.html</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Fatigue analyses and optimization of L 410 NG aircraft

Original language description

The complementary participation of the Institute of Aerospace Engineering on L 410 NG commuter transport aircraft design is presented in this paper. For damage tolerance analyses and following modifications modern finite element methods were used. A specific load sequence, which includes gust, maneuver and ground loads, was designed. Then detailed damage tolerance analyses of lower wing integrally stiffened and riveted wing panels were investigated. Complex damage tolerance analyses, crack propagation simulations and utilization of modern topometry finite element optimization method are presented in this article.

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

Result was created during the realization of more than one project. More information in the Projects tab.

Continuities

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

Publication year

2016

Confidentiality

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

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2016

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

3

Pages from-to

39-41

UT code for WoS article

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EID of the result in the Scopus database

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