The subject of this diploma thesis is a design of rudder aerodynamic balance and its optimization with regard to control forces and vertical tail and fuselage loading in critical flight modes – critical engine failure.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:417582 |
| Date | January 2020 |
| Creators | Pištěcká, Kateřina |
| Contributors | Doupník, Petr, Popela, Robert |
| 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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