TOPOMETRICAL FEM OPTIMIZATION OF L 410 NG AIRCRAFT WING STRUCTURE

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F14%3APU110799" target="_blank" >RIV/00216305:26210/14:PU110799 - isvavai.cz</a>
Result on the web
<a href="http://www.mmk.econference.cz/czech/prihlasene-prispevky_cs.html" target="_blank" >http://www.mmk.econference.cz/czech/prihlasene-prispevky_cs.html</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
TOPOMETRICAL FEM OPTIMIZATION OF L 410 NG AIRCRAFT WING STRUCTURE
Original language description
The article presents a topometrical optimization of the critical semi-shell wing structure of the aircraft in the CS-23 Commuter category. The modern FE optimization methods were used and significant weight savings were achieved mainly on the milled integral lower wing panel. A FE model validation with the analytical software and a selection of limits and requirements for an optimization are described in this article. Also a final stress analysis and a complex load capacity analysis are proved for designed structure modifications with an optimal stress distribution.
Czech name
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Czech description
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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
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Sborník příspěvků Mezinárodní Masarykovy konference pro doktorandy a mladé vědecké pracovníky 2014. Hradec Králové: MAGNANIMITAS.
ISBN
978-80-87952-07-8
ISSN
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e-ISSN
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Number of pages
9
Pages from-to
1-9
Publisher name
MAGNANIMITAS
Place of publication
Hradec Králové
Event location
Hradec Králové
Event date
Dec 15, 2014
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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