National Repository of Grey Literature 10 records found  Search took 0.00 seconds. 
Wing High Lift Devices
Rakovský, Kristián ; Weis, Martin (referee) ; Horák, Marek (advisor)
This bachelor’s thesis deals with wing high lift devices. Thesis states the purpose of high lift devices, their division, a brief overview of their history and a detailed description of particular devices with mentioning their advantages, disadvantages and usage in aviation. A part of the thesis also contains a short statistic, which compares wing high lift devices of high capacity transport aircraft.
Influence of the Francis turbine stay vane trailing edge shape on generation of Karman vortex street
Novotný, Vojtěch ; Skoták, Aleš (referee) ; Rudolf, Pavel (advisor)
In the flow past bluff bodies for a certain range of velocity a periodical vortex shedding emerges which is known as von Kármán vortex street. This phenomenon causes the periodical alteration of pressure field which affects the body. Should the vortex shedding frequency be similar to the body natural frequency, the amplitude of vibration significantly increases which can lead to fatigue cracking. In the case of water turbines, this phenomenon often affects the stay vanes. Both the vortex shedding frequency and the lift force amplitude can be influenced by the modification of the trailing edge geometry. The aim of this thesis is to use CFD computation in order to find the optimal geometry of the stay vane trailing edge for the specific Francis turbine unit.
Hight-lift Device of the Transport Aircraft Wings
Marek, Dominik ; Hammer, Jaromír (referee) ; Daněk, Vladimír (advisor)
This bachelor thesis brings a review of leading and trailing edge high-lift devices used on transport aircrafts. It briefly explains its function, calculates advantages and disadvantages of specific concepts, shows its influence on aerodynamic performance and observes current trends in air public transport.
High-lift system of the competition model aircraft
Vrba, Martin ; Koštial, Rostislav (referee) ; Koutník, Tomáš (advisor)
This Bachelor thesis is focused on compiling a summary of lift mechanization, at both the leading and the trailing edges used on plane models and unmanned means of transport. It briefly explains their principles and functions. It describes the method of calculation of the flight mode design of the competing aircraft according to the specifications of the Air Cargo Challenge competition.
High-lift system of the competition model aircraft
Vrba, Martin ; Koštial, Rostislav (referee) ; Koutník, Tomáš (advisor)
This Bachelor thesis is focused on compiling a summary of lift mechanization, at both the leading and the trailing edges used on plane models and unmanned means of transport. It briefly explains their principles and functions. It describes the method of calculation of the flight mode design of the competing aircraft according to the specifications of the Air Cargo Challenge competition.
Influence of the Francis turbine stay vane trailing edge shape on generation of Karman vortex street
Novotný, Vojtěch ; Skoták, Aleš (referee) ; Rudolf, Pavel (advisor)
In the flow past bluff bodies for a certain range of velocity a periodical vortex shedding emerges which is known as von Kármán vortex street. This phenomenon causes the periodical alteration of pressure field which affects the body. Should the vortex shedding frequency be similar to the body natural frequency, the amplitude of vibration significantly increases which can lead to fatigue cracking. In the case of water turbines, this phenomenon often affects the stay vanes. Both the vortex shedding frequency and the lift force amplitude can be influenced by the modification of the trailing edge geometry. The aim of this thesis is to use CFD computation in order to find the optimal geometry of the stay vane trailing edge for the specific Francis turbine unit.
Influence of the trailing edge on hydraulic machine parameters
Pospíšil, Dan ; Skoták, Aleš (referee) ; Rudolf, Pavel (advisor)
Master's thesis deals with possibility of simplifying calculation hydraulic machines by converting the three-dimensional geometry in the plane. The aim is to create modifications of a trailng edge and determine their effect of the hydraulic parameterso of the machine.
Wing High Lift Devices
Rakovský, Kristián ; Weis, Martin (referee) ; Horák, Marek (advisor)
This bachelor’s thesis deals with wing high lift devices. Thesis states the purpose of high lift devices, their division, a brief overview of their history and a detailed description of particular devices with mentioning their advantages, disadvantages and usage in aviation. A part of the thesis also contains a short statistic, which compares wing high lift devices of high capacity transport aircraft.
Hight-lift Device of the Transport Aircraft Wings
Marek, Dominik ; Hammer, Jaromír (referee) ; Daněk, Vladimír (advisor)
This bachelor thesis brings a review of leading and trailing edge high-lift devices used on transport aircrafts. It briefly explains its function, calculates advantages and disadvantages of specific concepts, shows its influence on aerodynamic performance and observes current trends in air public transport.
On Wakes in an Asymmetric Supersonic Flow Past Trailing Edges of a Profile Blade Cascade
Šafařík, Pavel ; Šimurda, David
Paper is concerned with results of research on the asymmetric supersonic flow past trailing edge. Distributions of the exit flow angle are compared to theoretical and reference value.

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