Aerodynamic simulation of a blimp kind unmanned aerial vehicle for stable environmental conditions

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dc.contributor.authorLópez-Leyva, Josué Aarón
dc.contributor.authorAguilera, L.A.
dc.contributor.authorPonce Camacho, Miguel Ángel
dc.contributor.authorBásaca-Preciado, Luis C.
dc.contributor.authorRamos García, Raúl
dc.contributor.authorRamos García, V.M.
dc.date.accessioned2019-10-24T17:12:15Z
dc.date.available2019-10-24T17:12:15Z
dc.date.created2017-11-06
dc.date.issued2018-03
dc.description.abstractAn Unmanned Aerial Vehicle blimp kind prototype for stable environmental conditions is shown in this paper. The lift, drag, weight, and thrust parameters are analyzed on the basis of the Archimedes principle, Bernoulli and continuity equations, and fluid simulations for different conditions (low-speed wind and absence of turbulence). The calculated push force (lift) is the minimum value to produce sustentation considering the overall mass of the aircraft. On the other hand, the drag parameter was analyzed using the fluid simulation to visualize the drag force.es_ES
dc.description.sponsorshipInternational Journal of Mechanical Engineering and Robotics Researches_ES
dc.description.urldoi: 10.18178/ijmerr.7.2.197-201es_ES
dc.format.page197-201es_ES
dc.identifier.indexacionScopuses_ES
dc.identifier.issn2278-0149
dc.identifier.urihttps://repositorio.cetys.mx/handle/60000/112
dc.language.isoen_USes_ES
dc.relation.ispartofseries7;2
dc.rightsAtribución-NoComercial-CompartirIgual 2.5 México*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/2.5/mx/*
dc.subjectLiftes_ES
dc.subjectDrages_ES
dc.subjectFluid simulationes_ES
dc.subjectUnmanned aerial vehiclees_ES
dc.titleAerodynamic simulation of a blimp kind unmanned aerial vehicle for stable environmental conditionses_ES
dc.title.alternativeInternational journal of mechanical engineering and robotics researches_ES
dc.typeArticlees_ES

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