This master‘s thesis is focused on the design of four-seat metal aircraft with low take-off weight in accordance with CS-23. Main dimensions of aircraft are designed, weight analysis, aerodynamic characteristics and flight performance are calculated in this thesis. In conclusion, the estimated costs of development and production are determined.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:254338 |
| Date | January 2016 |
| Creators | Mikulášek, Miloš |
| Contributors | Vaněk, František, Píštěk, Antonín |
| 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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