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Preliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Engine

dc.contributor.advisorPax Dolz Del Castellar, Rafael
dc.contributor.authorFernández Torres, Christopher Fernando
dc.date.accessioned2024-07-02T09:33:38Z
dc.date.available2024-07-02T09:33:38Z
dc.date.issued2024-06
dc.identifier.citationFernández Torres, C. F. (2024). Preliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Engine [Trabajo Fin de Estudios, Universidad Europea de Madrid]. Repositorio de Trabajos Fin de Estudios TITULAes
dc.identifier.urihttps://hdl.handle.net/20.500.12880/8418
dc.description.abstractThis project presents the peliminary design of a variable area propelling nozzle for an afterburning military aircraft engine. The study begins with an engine cycle analysis using a Python script to interate through various flight speeds and altitudes, simulating engine performance with and without afterburners.es
dc.language.isoenges
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacionales
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/es
dc.titlePreliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Enginees
dc.typeTFGes
dc.description.affiliationUniversidad Europea de Madrides
dc.description.degreeGrado en Ingeniería Aeroespacial en Aeronaveses
dc.rights.accessRightsopenAccesses
dc.subject.keywordDiseño peliminares
dc.subject.keywordTobera de área variablees
dc.subject.keywordPostcombustiones
dc.subject.keywordCiclo de motores
dc.subject.keywordAnálisis multifísicoes
dc.description.methodologypresencial


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