This diploma thesis deals with the calculation of composite wing loading and its stressanalysis. Furthermore work contains design of static strength test wing.
Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:228533 |
Date | January 2009 |
Creators | Freisleben, Michal |
Contributors | Juračka, Jaroslav, Jebáček, Ivo |
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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