This thesis addresses the design of ultralight aircraft as a one regulation UL-2 and basic aerodynamics characteristics of the individual parts of the airplane. Furthermore, we discuss the production process and the production itself tail and static strenght tests.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230058 |
| Date | January 2012 |
| Creators | Plaček, Jiří |
| Contributors | Jebáček, Ivo, Mališ, Michal |
| 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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