This master thesis deals with optimalization of stiffened integral wing panel of L-610 aircraft to its fatique life. Analysis has been made using FEM, AFGROW software and PYTHON language.
Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:442830 |
Date | January 2021 |
Creators | Bohýl, Tomáš |
Contributors | Katrňák, Tomáš, Vlček, Dalibor |
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 |
Page generated in 0.002 seconds