Zobrazeno 1 - 10
of 51
pro vyhledávání: '"Jacek Czarnigowski"'
Publikováno v:
Applied Computer Science, Vol 11, Iss 3 (2015)
The article presents a simulation study of air flow around the airfoil equipped with an additional rotary element, using the Magnus effect to change the air flow around it. For this purpose, a two-dimensional computational model for the airfoil witho
Externí odkaz:
https://doaj.org/article/379d032543f546079f7b83f7d2d7937b
Autor:
Michał Trendak, Jacek Czarnigowski
Publikováno v:
2nd International PhD Student’s Conference at the University of Life Sciences in Lublin, Poland: ENVIRONMENT – PLANT – ANIMAL – PRODUCT.
Autor:
Jacek Czarnigowski, Michał Trendak
Publikováno v:
Combustion Engines.
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
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:
International Journal of Engine Research. 22:2884-2899
The paper presents the results of the experimental research on the combustion process inside the cylinder of a large piston radial aircraft engine with dual or single spark plug ignition. The tests were carried out on the ASz-62IR-16X radial engine e
Autor:
Jacek Czarnigowski
Publikováno v:
Advances in Science and Technology Research Journal, Vol 14, Iss 3, Pp 107-117 (2020)
The paper presents the results of experimental investigations of total tensile stresses in a gyroplane’s rotor during flight. The research aimed to determine which flight maneuvers induce the greatest stress in the rotor blade and the hub bar. The
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
Autor:
Piotr Jakliński, Jacek Czarnigowski
Publikováno v:
Combustion Engines, Vol 177, Iss 2, Pp 60-65 (2019)
Aircraft piston engines are built with compromise on performance and safety. The desire to achieve the highest power-to-weight ratio leads to the search for solutions that optimize the combustion process. On the other hand, the need for maximum relia
Publikováno v:
Combustion Engines, Vol 177, Iss 2, Pp 12-18 (2019)
Ultralight aviation is based on piston engines requiring both performance and reliability. An important aspect is also the require-ments for the installation of such an engine on an airframe, especially its heat emission. This is firstly because of t
Publikováno v:
International Journal of Engine Research. :146808742211037
The paper presents the results of the experimental research on the combustion process inside the cylinder of a large piston radial aircraft engine with dual spark plug ignition. The tests were carried out on the ASz-62IR-16X radial engine equipped wi