Zobrazeno 1 - 10
of 122
pro vyhledávání: '"High lift devices"'
Publikováno v:
Aerospace, Vol 11, Iss 6, p 468 (2024)
In the last decades, electromechanical actuators started to be introduced in transport aircraft for primary and secondary flight control surfaces. Some innovative architectures have been proposed in the literature to use these actuators for high-lift
Externí odkaz:
https://doaj.org/article/25867ed9097246999200b49f4dc652fb
Autor:
Yuri Krashanitsa, Dmytro Zhyriakov
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 1, Pp 55-66 (2023)
The subject matter of this article is the aerodynamic profile of the wing with high-lift devices in the aircraft transport category. When high-lift devices are released, the aerodynamic flow of the wing changes significantly, this changes the stress-
Externí odkaz:
https://doaj.org/article/3267493c6d7f41e2898d5b964150b9f4
Akademický článek
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Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow, 2020, Vol. 31, Issue 2, pp. 618-628.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/HFF-09-2019-0687
Autor:
Muhammad Usman Shahid, Muhammad Tariq Javaid, Sheharyar Nasir, Umar Sajjad, Faizan Haider, S. Saddam ulHassan, Shuaib Salamat
Publikováno v:
Pakistan Journal of Engineering & Technology, Vol 5, Iss 2 (2022)
High lift devices play a vital role in dictating the accelerated performance of an aircraft for different flight phases such as takeoff, landing, and aerobatic maneuvers. The aerodynamic design of high lift devices for any particular aircraft is an i
Externí odkaz:
https://doaj.org/article/893e5e8631d64f6f86bb6368620511f9
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow, 2019, Vol. 30, Issue 8, pp. 3985-4011.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/HFF-07-2019-0570
Autor:
Yu. S. Mikhailov
Publikováno v:
Научный вестник МГТУ ГА, Vol 23, Iss 6, Pp 101-120 (2020)
The use of Fowler flaps and slotted slats in sweptwing aircraft is the standard solution to increase wing lift at take off and landing. In the literature this solution is known as a classical option of high-lift system of commercial subsonic aircraft
Externí odkaz:
https://doaj.org/article/4ac61c076abd424abdbab4410fc10612
Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 37, Iss 1, Pp 167-176 (2019)
By using the finite volume method and k-ω SST turbulence model to solve the Reynolds Average Navier-Stokes equation and using the slipping wall to simulate the relative movement of the ground, the ground effect on the aerodynamic characteristic of m
Externí odkaz:
https://doaj.org/article/44ad1f99d5dd4b37a790ea949c437dc0
Publikováno v:
Applied Sciences, Vol 12, Iss 3, p 1063 (2022)
Optimization design was widely used in the high-lift device design process, and the aeroacoustic reduction characteristic is an important objective of the optimization. The aerodynamic and aeroacoustic study on the baseline wing and flap configuratio
Externí odkaz:
https://doaj.org/article/e6f1f8f033654e98b7005e04de835d7e
Akademický článek
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