Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Karol Ścisłowski"'
Publikováno v:
Communications, Vol 26, Iss 1, Pp A1-A10 (2024)
The paper presents the results of gyrocopter fuselage experiment testing in a wind tunnel. The model subjected to testing was made in 1:8 scale by 3D printing. The tests included the measurement of forces and aerodynamic moments acting on the model,
Externí odkaz:
https://doaj.org/article/c4a6e6b6b35a42d387ad7b12cd3f4ace
Publikováno v:
Combustion Engines, Vol 191, Iss 4, Pp 23-28 (2022)
The researched object os a helicopter main rotor with blades of variable geometric twist characteristics. Variable torsion refers to systems of actuators made of shape memory alloys. The presented numerical analyses allow for evaluating both the dyna
Externí odkaz:
https://doaj.org/article/630d5d12f06642b392fcb472f388ef5c
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
Publikováno v:
Combustion Engines, Vol 187, Iss 4, Pp 83-89 (2021)
The article presents the results of analysis of operational parameters of piston engine CA 912 ULT which is a propulsion system of ultralight gyroplane Tercel produced by Aviation Artur Trendak. Research was conducted under normal operating condition
Externí odkaz:
https://doaj.org/article/022ac8445d9c411f8074f936aefe048e
Publikováno v:
Advances in Sciences and Technology, Vol 15, Iss 3, Pp 155-166 (2021)
In ultralight aviation, a very important engine parameter is the power-to-weight ratio. On the one hand, there is a tendency to minimize the size and weight of engines, and on the other hand, there is a demand to achieve the highest possible power by
Externí odkaz:
https://doaj.org/article/0a955489ff7d4f6fb8b3bc7c3c5e6fc6
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
Externí odkaz:
https://doaj.org/article/eba613663da3466fb99a22d4d79363e9
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
Autor:
Karol Ścisłowski
Publikováno v:
2nd International PhD Student’s Conference at the University of Life Sciences in Lublin, Poland: ENVIRONMENT – PLANT – ANIMAL – PRODUCT.
Publikováno v:
Advances in Science and Technology Research Journal, Vol 15, Iss 3, Pp 155-166 (2021)
In ultralight aviation, a very important engine parameter is the power-to-weight ratio. On the one hand, there is a tendency to minimize the size and weight of engines, and on the other hand, there is a demand to achieve the highest possible power by
Publikováno v:
Combustion Engines, Vol 187, Iss 4, Pp 83-89 (2021)
The article presents the results of analysis of operational parameters of piston engine CA 912 ULT which is a propulsion system of ultralight gyroplane Tercel produced by Aviation Artur Trendak. Research was conducted under normal operating condition