Propeller wing aerodynamic interference for small UAVs during VSTOL

dc.contributor.authorAdair, Desmond
dc.contributor.authorAlimaganbetov, Mergen
dc.date.accessioned2017-01-09T05:25:15Z
dc.date.available2017-01-09T05:25:15Z
dc.date.issued2016
dc.description.abstractThe 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.citationAdair, 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.urihttp://nur.nu.edu.kz/handle/123456789/2216
dc.language.isoenru_RU
dc.publisherIsrael Annual Conference on Aerospace Sciencesru_RU
dc.rightsAttribution-NonCommercial-ShareAlike 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/3.0/us/*
dc.subjectAerodynamicsru_RU
dc.subjectAerospace Engineeringru_RU
dc.subjectComputation theoryru_RU
dc.subjectComputational Fluid Dynamicsru_RU
dc.subjectFlight simulatorsru_RU
dc.subjectNumerical methodsru_RU
dc.titlePropeller wing aerodynamic interference for small UAVs during VSTOLru_RU
dc.typeArticleru_RU

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