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Optimalizace konstrukce bezpilotního prostředku vyráběného technologií Fused Deposition Modelling (FDM) / Structural optimization of 3D-printed Unmanned Aerial Vehicle

This master thesis deals with the design of the internal wing structure of 3D printed flying wing VUT 714. As a part of this work was performed a load calculation, static strenght test, comparative FEM analysis and subsequently topology optimization was performed. The outcome of this master thesis is a rational design of the wing internal structure based on the load calculation and knowledge of effect of this load on the structure.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:443181
Date January 2021
CreatorsSladký, Martin
ContributorsŠplíchal, Jan, Löffelmann, František
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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