Zobrazeno 1 - 10
of 708
pro vyhledávání: '"Flying wing"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2024, Vol. 96, Issue 9, pp. 1268-1278.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-05-2024-0128
Autor:
FANG Xinrui, YU Xiongqing
Publikováno v:
Hangkong gongcheng jinzhan, Vol 15, Iss 1, Pp 30-37 (2024)
Flying wing is a preferred configuration for unmanned combat air vehicle（UCAV），in which its airframe is highly integrated with intake and exhaust of propulsion system. To implement rapid geometric model of flying wing UCAV concept，a parametri
Externí odkaz:
https://doaj.org/article/54d9603a536d4a96a7ab21e295658ded
Autor:
Oktaf Agni Dhewa, Fatchul Arifin, Ardy Seto Priyambodo, Anggun Winursito, Yasir Mohd. Mustafa
Publikováno v:
International Islamic University Malaysia Engineering Journal, Vol 25, Iss 2 (2024)
The stability of an Unmanned Aerial Vehicle (UAV) attitude is crucial in aviation to mitigate the risk of accidents and ensure mission success. This study aims to optimize and adaptively control the flight attitude stability of a flying wing-type UAV
Externí odkaz:
https://doaj.org/article/79a72f08e21f456298ddd7782646053b
Autor:
Milenković-Babić Miodrag D., Ivković Dušan A., Ostojić Branislav G., Dovatov Biljana Z., Trifković Milenko S., Antonić Vuk D.
Publikováno v:
FME Transactions, Vol 52, Iss 4, Pp 556-562 (2024)
The main aim of this paper is to present a method for the conceptual design of a flying wing unmanned aerial vehicle using open-source software for rapid airfoil comparison and design and parametric geometry design and analysis. After adopting the fi
Externí odkaz:
https://doaj.org/article/ab716ad757a54c5aa23cb9946a25bc3e
Publikováno v:
气体物理, Vol 8, Iss 6, Pp 65-74 (2023)
The performance requirements of modern fighters meet multiple targets such as high speed, high mobility, stealth, lightweight and so on. The aircraft with a tailless flying wing configuration has the advantages of high aerodynamic efficiency, good mo
Externí odkaz:
https://doaj.org/article/8b158630c24943fa9658097daba2f86f
Publikováno v:
Aerospace, Vol 11, Iss 7, p 586 (2024)
The airfoil is the foundation of an aircraft, and its characteristics have a significant impact on those of the aircraft. Conventional airfoil design mainly focuses on improving aerodynamic performance, while flying wing airfoil designs should also c
Externí odkaz:
https://doaj.org/article/a5825bbd8c074ef49cc67fb11240b997
Akademický článek
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Akademický článek
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Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 40, Iss 5, Pp 990-996 (2022)
The flying-wing layout vectored thrust UAV often uses multiple sets of aerodynamic rudder surfaces and vector nozzles to jointly generate the required control force and torque, which belongs to a typical overdrive system. Multiple sets of rudder surf
Externí odkaz:
https://doaj.org/article/c56dd5751e9048d69fe1fa2936db4ea4
Autor:
Fabian Wiesemüller, Severin Meyer, Yijie Hu, Dominik Bachmann, Annapaola Parrilli, Gustav Nyström, Mirko Kovač
Publikováno v:
Advanced Intelligent Systems, Vol 5, Iss 7, Pp n/a-n/a (2023)
Aerial robots can autonomously collect temporal and spatial high‐resolution environmental data. This data can be utilized to develop mathematical ecology models to understand the impact of climate change on the habitat. In case of drone malfunction
Externí odkaz:
https://doaj.org/article/d248c1db524f419097bce5c65615a052