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Wing design of UAV aircraft
Chabada, Martin ; Dubnický, Lukáš (referee) ; Jebáček, Ivo (advisor)
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.
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Multi-shield wing construction options
Zemánek, Martin ; Löffelmann, František (referee) ; Šplíchal, Jan (advisor)
This bachelor’s thesis deals with the design possibilities of wing structures for gliders with a wingspan of 20m. The research section is focused on describing possible wing structural design solutions including multi-beam wing structure, as well as defining specific design parameters and requirements of gilder wings. The practical section is focused on the design and calculation of the structure of a wing with specified geometry and loading in two variants – single-spar and multi-spar. The output of this work consists of two final wing structure designs and a comparison of their mass. In the multi-spar design, the compared wing half has a mass of 33.507kg, while the single-spar variant has a mass of 37.04kg. The use of the multi-spar design therefore results in a mass saving of 3.53kg per wing half, the total mass saving is 7.07kg.
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Wing design of UAV aircraft
Chabada, Martin ; Dubnický, Lukáš (referee) ; Jebáček, Ivo (advisor)
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.
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