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Propeller wing aerodynamic interference for small UAVs during VSTOL

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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.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.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.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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