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Stanovení modálních charakteristik celokompozitového křídla s využitím MKP metod / Determination of modal characteristics of composite wings using FEM

The diploma thesis deals with the creation of a detail FEM model all-composite wing of glider. Reduction created FEM model of the beam model. The models are calculated natural frequencies, vibration shapes wings and then subsequently compared the results of analyzes of both models.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230924
CreatorsChurý, Tomáš
ContributorsCejpek, Jakub, 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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