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 |
Page generated in 0.0012 seconds