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.
Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230766 |
Date | January 2013 |
Creators | Vlček, Dalibor |
Contributors | Juračka, Jaroslav, Augustin, Petr |
Publisher | Vysoké učení technické v Brně. Fakulta strojního inženýrství |
Source Sets | Czech ETDs |
Language | Czech |
Detected Language | English |
Type | info:eu-repo/semantics/masterThesis |
Rights | info:eu-repo/semantics/restrictedAccess |
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