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Hmotnostní optimalizace kesonu křídla letounu L 410 NG / Wing structure weight optimization of the aircraft L 410 NG

Presented diploma thesis deals with parametric optimization of wing caisson of L 410 NG aircraft to reduce its‘structure weight. The paper is mainly focused on description and application of optimization methods with the use of finite element methods in MSC Nastran. Moreover the thesis contains loading state check of optimized design, done in STAUNO software.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230776
Date January 2013
CreatorsJurek, Peter
ContributorsMališ, Michal, Katrňák, Tomáš
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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