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dc.contributor.authorStaňa, Ján
dc.contributor.authorŠkultéty, Filip
dc.date.accessioned2021-06-22T07:22:05Z
dc.date.available2021-06-22T07:22:05Z
dc.date.issued2021
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/459
dc.description.abstractThe 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.en_US
dc.language.isosken_US
dc.publisherUniversity of Zilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectairplaneen_US
dc.subjectconstructionen_US
dc.subjectmodelen_US
dc.subjectunmanned aerial vehicleen_US
dc.subjectL-39en_US
dc.titleDesign of the reference model of the aero l-39 aircraften_US
dc.typeConference paperen_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2021.2.40


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Except where otherwise noted, this item's license is described as http://creativecommons.org/licenses/by/4.0/