|
|
Preliminary aerodynamic analysis of remotely controlled model with jet propulsion
Novák, Ondřej ; Zikmund, Pavel (referee) ; Popela, Robert (advisor)
This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes to design of wing, its position and wing-fuselage junction. In this work emphasis is laid on flow separation, its interaction with other flow structures and its influence on aerodynamic properties. The goal of these changes to the aircraft is ensuring sufficient stability and controllability in low as well as high angle of attack flight. AVL, XFLR5 and CFD methods were used in the thesis. In case of inaccuracy of CFD calculation, two backup wing related modifications were prepared.
|
|
| |
|
|
International drone goods transportation
Říha, Vojtěch ; Zavadilová, Marta (referee)
International drone goods transportation - Abstract, key words The aim of this work is to explore the possibilities of liability concepts in relation to unmanned aerial vehicles that transport goods in the international transport of goods. For this purpose, a comparison of the normative theory of František Weyr and the way of functioning of formally logical systems is performed within the work. This normative theory has a great impact on the actual functioning of the information system itself, which is exempt from the content of its own rule contained in the norm itself. There are described methods of acknowledging machines and the method of interpretation and application of individual rules contained in norms themselves that are being interpreted by these machines. All this precisely with regard to the fact that unmanned aerial vehicles cannot learn to distinguish between inner values of norms, on which individual legal norms are based. This is because unmanned aerial vehicles cannot achieve this with the help of a tool of pure intelligence alone. Since unmanned aerial vehicles interpret and apply their own internal norms to the outside world only as they are set within their normative setting. This normative setting is also related to the protection against banal evil and the protection of notional...
|
|
|
International drone goods transportation
Říha, Vojtěch ; Růžička, Květoslav (advisor) ; Rozehnal, Aleš (referee) ; Brodec, Jan (referee)
International drone goods transportation - Abstract, key words The aim of this work is to explore the possibilities of liability concepts in relation to unmanned aerial vehicles that transport goods in the international transport of goods. For this purpose, a comparison of the normative theory of František Weyr and the way of functioning of formally logical systems is performed within the work. This normative theory has a great impact on the actual functioning of the information system itself, which is exempt from the content of its own rule contained in the norm itself. There are described methods of acknowledging machines and the method of interpretation and application of individual rules contained in norms themselves that are being interpreted by these machines. All this precisely with regard to the fact that unmanned aerial vehicles cannot learn to distinguish between inner values of norms, on which individual legal norms are based. This is because unmanned aerial vehicles cannot achieve this with the help of a tool of pure intelligence alone. Since unmanned aerial vehicles interpret and apply their own internal norms to the outside world only as they are set within their normative setting. This normative setting is also related to the protection against banal evil and the protection of notional...
|
|
|
Preliminary aerodynamic analysis of remotely controlled model with jet propulsion
Novák, Ondřej ; Zikmund, Pavel (referee) ; Popela, Robert (advisor)
This bachelor´s thesis deals with aerodynamic analysis of unmanned aircraft and subsequent changes to design of wing, its position and wing-fuselage junction. In this work emphasis is laid on flow separation, its interaction with other flow structures and its influence on aerodynamic properties. The goal of these changes to the aircraft is ensuring sufficient stability and controllability in low as well as high angle of attack flight. AVL, XFLR5 and CFD methods were used in the thesis. In case of inaccuracy of CFD calculation, two backup wing related modifications were prepared.
|
|
| |
guest ::
