Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Ksenia Siadkowska"'
Publikováno v:
Applied Computer Science, Vol 18, Iss 1, Pp 5-19 (2022)
This paper investigates the strenght of a conceptual main rotor blade dedicated to an unmanned helicopter. The blade is made of smart materials in order to optimize the efficiency of the aircraft by increasing its aerodynamic performance. This purpos
Externí odkaz:
https://doaj.org/article/f622efbfee4d4f8c972ae4d61b628bbc
Autor:
Karol Ścisłowski, Krzysztof Skiba, Mirosław Wendeker, Rafał Kliza, Ksenia Siadkowska, Tomasz Lusiak, Andrej Novák
Publikováno v:
Communications, Vol 24, Iss 2, Pp B148-B157 (2022)
This paper presents an analysis of the strength of a prototype test rig for testing rotors of unmanned aerial vehicles. Digital design software was used for the design work that covered the creation of a virtual model of the test rig and strength ana
Externí odkaz:
https://doaj.org/article/f6f1c046b186408e87c4975c0f2d5768
Publikováno v:
Advances in Science and Technology Research Journal. 16:54-66
Autor:
Ksenia Siadkowska
Publikováno v:
2nd International PhD Student’s Conference at the University of Life Sciences in Lublin, Poland: ENVIRONMENT – PLANT – ANIMAL – PRODUCT.
Autor:
Ksenia Siadkowska
Publikováno v:
Advances in Science and Technology Research Journal, Vol 14, Iss 4, Pp 104-114 (2020)
The recommended optimal twist angles were determined for particular sections of the prototype rotor blade dedicated to an unmanned helicopter with a maximum take-off weight of 150 kg. The main rotor diameter is 2m. The main rotor blade was tested in
Autor:
Zbigniew Czyż, Ksenia Siadkowska
Publikováno v:
Combustion Engines, Vol 178, Iss 3, Pp 4-8 (2019)
Selecting appropriate materials is presently a complex task as material databases cover tens of thousands of different types of mate-rials. Product designing proceeds in numerous stages and in most of them there are open questions with not only one c
Publikováno v:
Combustion Engines, Vol 177, Iss 2, Pp 151-155 (2019)
The paper presents the research results of the injector construction with the modified injection nozzle. The injector is designed for a prototype opposed-piston aircraft diesel engine. The measurements were based on the Mie scattering technique. The
Publikováno v:
Combustion Engines, Vol 185, Iss 2, Pp 39-43 (2021)
This paper presents an analysis of selected propulsion units dedicated to test stands for unmanned aircraft systems. It focuses on engines suitable for aircraft with a maximum take-off mass up to 150 kg. The study includes an analysis of propulsion u
Autor:
Ksenia Siadkowska
Publikováno v:
CENTRAL EUROPEAN SYMPOSIUM ON THERMOPHYSICS 2021 (CEST 2021).
Publikováno v:
CENTRAL EUROPEAN SYMPOSIUM ON THERMOPHYSICS 2021 (CEST 2021).