Zobrazeno 1 - 10
of 4 577
pro vyhledávání: '"lift to drag ratio"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2024, Vol. 96, Issue 6, pp. 808-817.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-10-2023-0271
Publikováno v:
Heliyon, Vol 10, Iss 8, Pp e29377- (2024)
In recent times, machine learning algorithms have gained significant traction in addressing aerodynamic challenges. These algorithms prove invaluable for predicting the aerodynamic performance, specifically the Lift-to-Drag ratio of airfoil datasets,
Externí odkaz:
https://doaj.org/article/df6c5136ad384ce2aa25f35102e560cf
Publikováno v:
Sustainable Earth Review; Oct2023, Vol. 3 Issue 4, p46-61, 16p
Publikováno v:
International Journal of Technology, Vol 14, Iss 1, Pp 5-14 (2023)
Turbines are efficient power generators. Because wind energy is a clean fuel source, it is widely utilized in some regions. One of the major factors affecting wind turbine performance is the angle of attack of the blade. The aerodynamics and effic
Externí odkaz:
https://doaj.org/article/82258c5fd86b4ab1b041f5aad544cefb
Autor:
Emmanuel Yeboah Osei, Richard Opoku, Albert K. Sunnu, Muyiwa S. Adaramola, Ebenezer Adu Kyeremeh
Publikováno v:
Alexandria Engineering Journal, Vol 61, Iss 12, Pp 12301-12310 (2022)
In this study, the aerodynamic performance characteristics of three new EYO-Series low Reynolds number (Re) airfoils were tested at Re = 100,000 to 500,000, which are typical range of Re numbers encountered by airfoils of small wind turbine blades. T
Externí odkaz:
https://doaj.org/article/96f73747cee043ccb04a973348d95dd0
Akademický článek
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Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 94, Issue 4, pp. 633-645.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-04-2021-0121
Autor:
Durmus, Seyhun
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 94, Issue 3, pp. 473-479.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-07-2021-0218
Publikováno v:
Applied Mechanics; Dec2022, Vol. 3 Issue 4, p1176-1189, 14p
Autor:
Durmus, Seyhun
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 6, pp. 1097-1103.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2021-0038