Zobrazeno 1 - 10
of 80
pro vyhledávání: '"gyroplane"'
Autor:
Tomasz Łusiak
Publikováno v:
Advances in Sciences and Technology, Vol 16, Iss 6, Pp 23-35 (2022)
The paper presents the results of aerodynamic testing and analysis of a new wind-rotor aircraft. The measurements were carried out on a specialized wind tunnel test stand equipped with a dedicated aerodynamic weighing system. Measurements were carrie
Externí odkaz:
https://doaj.org/article/438f9da0f3da4c428bfb9258bf9c18db
Autor:
Jacek Czarnigowski
Publikováno v:
Advances in Sciences and Technology, 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
Externí odkaz:
https://doaj.org/article/a9f84bd5f09446118d7c73641ed8f23a
Autor:
Zbigniew Czyż, Paweł Karpiński
Publikováno v:
Aviation, Vol 23, Iss 4 (2020)
The paper presents some of the works related to the project of modern gyrocopter construction with the possibility of a short start, known as "jump-start". It also presents a methodology related to numerical calculations using Computational Fluid Dyn
Externí odkaz:
https://doaj.org/article/bbfd041a883a47d88533ef9954381769
Autor:
Figat, Marcin
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2017, Vol. 89, Issue 5, pp. 663-670.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2017-0047
Autor:
Enrico Petritoli, Fabio Leccese
Publikováno v:
Drones, Vol 5, Iss 2, p 53 (2021)
Starting from the Martian environment, we examine all the necessary requirements for a UAV and outline the architecture of a gyroplane optimized for scientific research and support for (future) Mars explorers, highlighting its advantages and critical
Externí odkaz:
https://doaj.org/article/b26fc6545e534ecab79ce8c0832d2ab1
Publikováno v:
Advances in Sciences and Technology, Vol 10, Iss 31, Pp 169-176 (2016)
The paper presents the analyzes of the pre-rotation engine loads in the Taurus autogyro manufactured by Aviation Artur Trendak from Poland. Based on the NACA-9 H-12 airfoil characteristics of the drag coefficient, on which the rotor blade was made, f
Externí odkaz:
https://doaj.org/article/6542f767e5e245b98139c6942e987655
Publikováno v:
Sensors, Vol 20, Iss 19, p 5537 (2020)
This paper presents the results of research on the airflow around a multirotor aircraft. The research consisted of the analysis of the velocity field using particle image velocimetry. Based on the tests carried out in a wind tunnel, the distribution
Externí odkaz:
https://doaj.org/article/ecd7fb1b5c834c25a7eb82183b6ffb2a
While new-generation gyroplanes are very stable during flight, the susceptibility to roll over briefly after touching down is still the issue due to incorrectly applied landing procedure. A tendency to dynamically roll over is also known from helicop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c6f465d0e9253d34652a99dc86fec0c2
https://doi.org/10.1007/s13272-022-00575-5
https://doi.org/10.1007/s13272-022-00575-5
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2011, Vol. 83, Issue 6, pp. 420-428.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/00022661111173298
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