Análisis de un perfil aerodinámico para generar sustentación en la atmósfera de Marte

dc.contributorHernández Beleño, Rubén Darío
dc.contributorMejía Ruda, Edilberto
dc.creatorJiménez García, Mauricio
dc.date.accessioned2020-06-11T15:01:08Z
dc.date.accessioned2022-09-28T21:24:58Z
dc.date.available2020-06-11T15:01:08Z
dc.date.available2022-09-28T21:24:58Z
dc.date.created2020-06-11T15:01:08Z
dc.date.issued2020-02-28
dc.identifierhttp://hdl.handle.net/10654/35775
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3744835
dc.description.abstractEste proyecto de investigación busca simular las condiciones de la atmósfera de Marte y ver como un perfil aerodinámico se comporta bajo dichas circunstancias, buscando abrir las puertas para el futuro diseño de aeronaves que permitan una exploración más eficiente y rápida de la superficie marciana. También, busca comprender la complejidad del flujo en la atmósfera de Marte, dada su baja densidad en comparación con la de la tierra, y el apoyo que da un bajo coeficiente de gravedad. Estos dos factores reducen la fuerza y eficiencia de elevación, lo que hace aún más complejo el vuelo en la atmósfera de Marte.
dc.languagespa
dc.languagespa
dc.publisherUniversidad Militar Nueva Granada
dc.publisherFacultad de Ingeniería
dc.publisherMaestría en Ingeniería Mecatrónica
dc.publisherIngeniería - Maestría en Ingeniería Mecatrónica
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dc.rightshttps://creativecommons.org/licenses/by-nc-nd/2.5/co/
dc.rightsinfo:eu-repo/semantics/openAccess
dc.rightsAtribución-NoComercial-SinDerivadas
dc.rightsDerechos Reservados - Universidad Militar Nueva Granada, 2020
dc.titleAnálisis de un perfil aerodinámico para generar sustentación en la atmósfera de Marte
dc.typeinfo:eu-repo/semantics/masterThesis


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