Scipediacontent: Scipediacontent moved page Draft Content 930171361 to Gorol et al 2018a

2021-02-12T15:01:01Z

Scipediacontent moved page Draft Content 930171361 to Gorol et al 2018a

Scipediacontent: Created page with " == Abstract == A challenging issue associated with fixed-wing Unmanned Aerial Vehicles (UAVs) is that these vehicles are often not appropriate for operating effectively in l..."

2021-02-12T15:00:57Z

Created page with " == Abstract == A challenging issue associated with fixed-wing Unmanned Aerial Vehicles (UAVs) is that these vehicles are often not appropriate for operating effectively in l..."

New page

== Abstract ==

A challenging issue associated with fixed-wing Unmanned Aerial Vehicles (UAVs) is that these vehicles are often not appropriate for operating effectively in limited airspace. This problem emerges especially in urban environment where the usage of a runway is not possible, and UAVs usually have to fly at a relatively low speed and altitude. The development of a vertical take-off and landing (VTOL) fixed-wing plane is a promising trend which hopefully will solve this issue. This paper presents the design process of an unmanned vertical take-off and landing aircraft including prototyping of the airframe construction and mathematical modeling as well as computational fluid dynamics (CFD) simulations. The designed system is to be a hybrid platform, for which different operating modes correspond to the vertical flight, transition, and spatial flight in the airframe system. The paper discusses an iterative design process of the platform with emphasis on CAD design and aerodynamic analysis for particular flight modes. The operating prototype is presented and future plans for platform improvement are discussed.

Document type: Article

== Full document ==
<pdf>Media:Draft_Content_930171361-beopen503-3670-document.pdf</pdf>

== Original document ==

The different versions of the original document can be found in:

* [http://downloads.hindawi.com/journals/jat/2018/7040531.pdf http://downloads.hindawi.com/journals/jat/2018/7040531.pdf] under the license https://creativecommons.org/licenses/by

* [http://dx.doi.org/10.1155/2018/7040531 http://dx.doi.org/10.1155/2018/7040531] under the license cc-by

* [http://downloads.hindawi.com/journals/jat/2018/7040531.pdf http://downloads.hindawi.com/journals/jat/2018/7040531.pdf],
: [http://downloads.hindawi.com/journals/jat/2018/7040531.xml http://downloads.hindawi.com/journals/jat/2018/7040531.xml],
: [http://dx.doi.org/10.1155/2018/7040531 http://dx.doi.org/10.1155/2018/7040531] under the license http://creativecommons.org/licenses/by/4.0

* [http://dx.doi.org/10.1155/2018/7040531 http://dx.doi.org/10.1155/2018/7040531],
: [https://doaj.org/toc/0197-6729 https://doaj.org/toc/0197-6729],
: [https://doaj.org/toc/2042-3195 https://doaj.org/toc/2042-3195] under the license http://creativecommons.org/licenses/by/4.0/

* [https://www.hindawi.com/journals/jat/2018/7040531 https://www.hindawi.com/journals/jat/2018/7040531],
: [http://downloads.hindawi.com/journals/jat/2018/7040531.pdf http://downloads.hindawi.com/journals/jat/2018/7040531.pdf],
: [https://www.mendeley.com/catalogue/a3e923d2-aa27-3d3c-9567-2c50a89d2a96 https://www.mendeley.com/catalogue/a3e923d2-aa27-3d3c-9567-2c50a89d2a96],
: [https://academic.microsoft.com/#/detail/2894872308 https://academic.microsoft.com/#/detail/2894872308]

← Older revision	Revision as of 15:01, 12 February 2021
(No difference)

Gorol et al 2018a - Revision history

Scipediacontent: Scipediacontent moved page Draft Content 930171361 to Gorol et al 2018a

Scipediacontent: Created page with " == Abstract == A challenging issue associated with fixed-wing Unmanned Aerial Vehicles (UAVs) is that these vehicles are often not appropriate for operating effectively in l..."