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    Polymorfné konštrukcie ako súčasť riadenia letúnov
    (University of Žilina, 2025) Schwarz, Michal; Škultéty, Filip
    Goal of this work is to find out whether morphing wing configurations are a viable option for flight controls such as elevators, flaps, ailerons etc. This work is divided into 3 sections. First section is about general research of conventional wing constructions, materials used in aircraft and mechanisms used to actuate flight controls. Second section looks into construction of morphing wings, viable materials for these constructions, mechanism used to actuate them and finally designing a functioning morphing wing based on previous research. In final third part we are going to compare morphing configuration against conventional solutions used on aircraft today in CFD simulations as well as in a wind tunnel and compare the results gained by these simulations.
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    Design of the reference model of the aero l-39 aircraft
    (University of Zilina, 2021) Staňa, Ján; Škultéty, Filip
    The object of the research of the paper is to design a reference model of an unmanned aircraft according to the model of the training jet Aero L 39. The work contains an analysis of the methods, procedures and typology used in the creation of reference models. Subsequently, the design of an unmanned vehicle was created using computer modelling, which was subjected to aerodynamic simulations and strength analysis. Aerodynamic performance was investigated on the airframe of the aircraft and strength analyses were determined on specific structural elements. After successful program tests, a functional model of the aircraft was built. The prerequisite was mainly aerodynamic analyses, which should determine with sufficient accuracy the basic structure of the model's flight. The result of solving the problem is a functional model of the aircraft, which is suitable for flight tests using appropriate hardware.