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 |
Page generated in 0.0017 seconds