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Pevnostní kontrola a topologická optimalizace dílu podvozku letounu / Strength Analysis and Topology optimization of the aircraft landing gear

This master thesis is about stress analysis of landing gear for accomplishment CS-23 regulation. The first part examines all alternatives of landing gear regarding for accomplishment of regulation. Next part is stress analysis of main and nose landing gear using FEM analysis in MSC Nastran software. Last part of master thesis describes topology optimization of two parts of landing gear.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:417462
Date January 2020
CreatorsBaláš, Martin
ContributorsSymonov, Volodymyr, Šplíchal, Jan
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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