Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Gennady S. Panatov"'
Publikováno v:
Diagnostyka, Vol 23, Iss 2, Pp 1-8 (2022)
In the present research, an investigation of the influence of winglet sweep angle and winglet tip chord of the aircraft wing on the aerodynamics properties and how to make it better has been carried out, assuming Cant angle 60, winglet height = 3.5 m
Externí odkaz:
https://doaj.org/article/487d22e9ad194f449dd2768903834930
Publikováno v:
2022 5th International Conference on Engineering Technology and its Applications (IICETA).
In this paper, we study the effect of winglet Toe & Twist angle on the wing of the aircraft aerodynamics performances and how to improve it, we analyze the aerodynamics properties of the wing with winglets with Cant angle 60o and winglet span = 3.5 m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8eb72417035013adfcd30fea98b39a6d
https://doi.org/10.21203/rs.3.rs-664368/v1
https://doi.org/10.21203/rs.3.rs-664368/v1