Propeller wing aerodynamic interference for small UAVs during VSTOL

dc.contributor.author	Adair, Desmond
dc.contributor.author	Alimaganbetov, Mergen
dc.date.accessioned	2017-01-09T05:25:15Z
dc.date.available	2017-01-09T05:25:15Z
dc.date.issued	2016
dc.description.abstract	The goal of the present investigation is to gain a better understanding, using numerical simulation, of the aerodynamic interference between propeller and wing during different flight phases of a VSTOL unmanned-aerial-vehicle (UAV). The proposed UAV investigated here, tilts part of the wings together with the propellers and nacelles, with each of the propellers located inboard between wing-tip and fuselage.	ru_RU
dc.identifier.citation	Adair, D., & Alimaganbetov, M. (2016). Propeller wing aerodynamic interference for small UAVs during VSTOL. In IACAS 2016 - 56th Israel Annual Conference on Aerospace Sciences. Israel Annual Conference on Aerospace Sciences.	ru_RU
dc.identifier.uri	http://nur.nu.edu.kz/handle/123456789/2216
dc.language.iso	en	ru_RU
dc.publisher	Israel Annual Conference on Aerospace Sciences	ru_RU
dc.rights	Attribution-NonCommercial-ShareAlike 3.0 United States	*
dc.rights.uri	http://creativecommons.org/licenses/by-nc-sa/3.0/us/	*
dc.subject	Aerodynamics	ru_RU
dc.subject	Aerospace Engineering	ru_RU
dc.subject	Computation theory	ru_RU
dc.subject	Computational Fluid Dynamics	ru_RU
dc.subject	Flight simulators	ru_RU
dc.subject	Numerical methods	ru_RU
dc.title	Propeller wing aerodynamic interference for small UAVs during VSTOL	ru_RU
dc.type	Article	ru_RU

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