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Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance / Damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel

Master’s thesis deals with the damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel including crack growth and residual strength analyses and inspection program proposal. Presented DT evaluation has been done using FE model of the wing and AFGROW software.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230766
Date January 2013
CreatorsVlček, Dalibor
ContributorsJuračka, Jaroslav, Augustin, Petr
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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