Original title: Návrh křídla letounu UAV v kategorii do 600 kg
Translated title: Wing design of UAV aircraft
Authors: Chabada, Martin ; Dubnický, Lukáš (referee) ; Jebáček, Ivo (advisor)
Document type: Master’s theses
Year: 2021
Language: slo
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
Abstract: [slo] [eng]
Hlavným cieľom tejto práce je návrh krídla UAV lietadla, vrátane voľby materiálu, výpočtu zaťaženia krídla a pevnostnej kontroly. Medzi ďalšie ciele patrí návrh umiestnenia a objem palivových nádrží a návrh zmenšovania rozpätia krídel po pristátí. The main aim of the this diploma thesis is the wing design of the UAV aircraft, including the appropriate material choice, calculation of the wing load and also strength analysis. Other goals include the design of the location and volume of fuel tanks, as well as the design of wingspan reduction after landing.
Keywords: certification UL2; composite wing; flight envelope; Wing construction; wing local calculations; wing stress analysis

Institution: Brno University of Technology (web)
Document availability information: Fulltext is available in the Brno University of Technology Digital Library.
Original record: http://hdl.handle.net/11012/197429

Permalink: http://www.nusl.cz/ntk/nusl-610498


The record appears in these collections:
Universities and colleges > Public universities > Brno University of Technology
Academic theses (ETDs) > Master’s theses