Thesis summarizes conceptual design of VUT 001 Marabu airplane modification to fulfill CS-22 regulation requirements. Aerodynamical optimalization of wing and horizontal tail geometry is solved. Aerodynamical characteristics, performance and stability is analysed and basic structural design of wing and horizontal tail is performed.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:228059 |
| Date | January 2008 |
| Creators | Navrátil, Jan |
| Contributors | Daněk, Vladimír, 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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