The main aim of the this diploma thesis is the wing design of the UAV aircraft, including the appropriate material choice, calculation of the wing load and also strength analysis. Other goals include the design of the location and volume of fuel tanks, as well as the design of wingspan reduction after landing.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:442849 |
| Date | January 2021 |
| Creators | Chabada, Martin |
| Contributors | Dubnický, Lukáš, Jebáček, Ivo |
| Publisher | Vysoké učení technické v Brně. Fakulta strojního inženýrství |
| Source Sets | Czech ETDs |
| Language | Slovak |
| Detected Language | English |
| Type | info:eu-repo/semantics/masterThesis |
| Rights | info:eu-repo/semantics/restrictedAccess |
Page generated in 0.0024 seconds