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Pevnostní analýza vybrané části trupu letounu / Strain-stress analysis of selected parts of the airplain

This work describes the creation of detailed FEM models of the selected area. Primarily is focused on the process of creating a detailed FEM model of the part of airplane using the static condensation. This work also contains a description of the process stress analysis of part of the fuselage of the airplane EV-55 Outback.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230928
Date January 2013
CreatorsMareček, Jiří
ContributorsŠtěrba, Petr, Návrat, 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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