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Národní úložiště šedé literatury Nalezeno 3 záznamů.  Hledání trvalo 0.01 vteřin. 
Comparison of FEM models using 1D and 2D elements used to flutter analysis
 Zubaľ, Filip ; Navrátil, Jan (oponent) ; Šplíchal, Jan (vedoucí práce)
The diploma thesis deals with flutter, which is one of the most dangerous dynamic aeroelastic phenomena in aviation. The work includes the creation process and subsequent flutter analysis of two FEM models of the wing of the BUT 051 Ray experimental aircraft. The goal of the work is to compare individual FEM models and determine the critical flutter speed, to evaluate the effectiveness and usability of FEM models created by 1D or 2D elements.
Úplný záznam
Construction parts and Elements of the of Large transport aircraft Fuselage structure
 Zubaľ, Filip ; Dubnický, Lukáš (oponent) ; Juračka, Jaroslav (vedoucí práce)
Fuselage design is an area of aerospace engineering that combines aerodynamics with mechanical and material engineering. Many factors affect the construction and design of the fuselage. The bachelor thesis is focused on the processing and systematic ordering of individual structural units used in large transport aircraft. It points out the diversity of individual structural nodes in the design of the aircraft. The work is divided according to sections of the fuselage, where the specific design solutions for the node are then discussed. At the end of the work, I present a comparison of the two most famous competing aircraft models of Airbus and Boeing company. I pointed out the individual combinations of structural elements. Compared data are processed using tables and schematic figures. The bachelor thesis was also translated into a form of presentation intended for educational purposes.
Úplný záznam
Construction parts and Elements of the of Large transport aircraft Fuselage structure
 Zubaľ, Filip ; Dubnický, Lukáš (oponent) ; Juračka, Jaroslav (vedoucí práce)
Fuselage design is an area of aerospace engineering that combines aerodynamics with mechanical and material engineering. Many factors affect the construction and design of the fuselage. The bachelor thesis is focused on the processing and systematic ordering of individual structural units used in large transport aircraft. It points out the diversity of individual structural nodes in the design of the aircraft. The work is divided according to sections of the fuselage, where the specific design solutions for the node are then discussed. At the end of the work, I present a comparison of the two most famous competing aircraft models of Airbus and Boeing company. I pointed out the individual combinations of structural elements. Compared data are processed using tables and schematic figures. The bachelor thesis was also translated into a form of presentation intended for educational purposes.
Úplný záznam

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