The master‘s thesis is focused to design and to calculation of tailwheel-type landing gear for ultralight aircraft JA-400 according to rules UL 2 part I. – ULL and LTF UL. In the first part is search about aiplanes with three types of landing gear. Then there is rule comparison, with result what rule will the calculation meet. Then the concept and design of landing gear is proved. In the end the improve of lift option is mentioned.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:417585 |
| Date | January 2020 |
| Creators | Rakušan, Miroslav |
| Contributors | Vaněk, František, Jebáček, Ivo |
| 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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