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Competition Aircraft Model Tail Design
Hub, Pavel ; Šurkala, Martin (referee) ; Matějů, Jiří (advisor)
This bachelor’s thesis deals with an empennage design for a new competition aircraft. The introduction gives an overview of the Air Cargo Challenge 2019 competition and conceptual layout of the aircraft. The research part of the thesis is focused on possible tail configurations, tail parameters and a statistical analysis of commercially made aircrafts. The most suitable configurations are then compared in detail, during which basic longitudinal stability calculations are done. In the last part, load is calculated, followed by structural design and bearing components sizing.
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Proposal for the use of the Z 143 Lsi aircraft for aerobatic operation
Hub, Pavel ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This master thesis deals with the impact of given construction changes on the Zlín Aircraft Z 143 Lsi aircraft, the purpose of which is to enable the aircraft to operate in the aerobatic category in accordance with FAR-23 certification guidelines. An important part of the thesis is the definition of permitted flight configurations with respect to the aircrafts´ structural strength limits and flight performance. Furthermore, impact of these changes on flight within the normal and utility categories is investigated. An overview of neccessary certification procedures is provided as well. The goal of the thesis is to supply the company with relevant technical documentation to decide on adequacy of the concept.
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Proposal for the use of the Z 143 Lsi aircraft for aerobatic operation
Hub, Pavel ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This master thesis deals with the impact of given construction changes on the Zlín Aircraft Z 143 Lsi aircraft, the purpose of which is to enable the aircraft to operate in the aerobatic category in accordance with FAR-23 certification guidelines. An important part of the thesis is the definition of permitted flight configurations with respect to the aircrafts´ structural strength limits and flight performance. Furthermore, impact of these changes on flight within the normal and utility categories is investigated. An overview of neccessary certification procedures is provided as well. The goal of the thesis is to supply the company with relevant technical documentation to decide on adequacy of the concept.
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Porovnání klonů odrůdy Tramín po stránce kvalitativní a kvantitativní
Hub, Pavel
The aim of this work was to evaluate the qualitative and quantitative parameters of the clones of the Tramín variety. The introduction describes the Tramín variety, its origin, distribution, mutations and clones, and also deals with habitat requirements, variety resistance, cultivating properties And climatic conditions in the area of the experimental vineyard. In the experiment, the facts about individual clone analyzes are described, with methodology, site description, On which grapes were harvested and evaluated. Given the results of the comparison of the individual clones from the same site, it would be advisable not to focus on just one clone, but at least three clones to support each other. Not only in production technology, but also in sensory properties where one clone supports the second or third clone in one clone. It will also be appropriate to focus on the dependence of micro climatic conditions, soil conditions, The main objective was to recommend the suitability of a combination of Tramín clones with different properties for the production of quality wine according to the obtained data. Based on the results I would suggest focusing on the cultivation of French clones, Clones 47 and 1077, which provide a spice and a clone 46-106, which gives the wines of floral tones, fruity and delicate aroma. As they complement each other very well both in terms of yields and in terms of quality and aroma of the produced wines.
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Competition Aircraft Model Tail Design
Hub, Pavel ; Šurkala, Martin (referee) ; Matějů, Jiří (advisor)
This bachelor’s thesis deals with an empennage design for a new competition aircraft. The introduction gives an overview of the Air Cargo Challenge 2019 competition and conceptual layout of the aircraft. The research part of the thesis is focused on possible tail configurations, tail parameters and a statistical analysis of commercially made aircrafts. The most suitable configurations are then compared in detail, during which basic longitudinal stability calculations are done. In the last part, load is calculated, followed by structural design and bearing components sizing.
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