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dc.contributor.advisor | Ballester Sarrias, Enrique | es_ES |
dc.contributor.author | Esteller Torres, Alberto | es_ES |
dc.date.accessioned | 2015-07-09T13:29:51Z | |
dc.date.available | 2015-07-09T13:29:51Z | |
dc.date.created | 2014-07-02 | |
dc.date.issued | 2015-07-09 | |
dc.identifier.uri | http://hdl.handle.net/10251/52895 | |
dc.description.abstract | The aim of this project is the study of the improvement of an ideal turbofan engine based on the commercial model Price Induction DGEN 380. These kinds of aircraft engines are basically focused in personal light jet aviation, whose operation specifications match with this engine’s performance. Generally, the common layout of these aircraft is a twin-engine powerplant, which ensures the required performance and fuel consumption efficiency. This performance is explained in the table above. | es_ES |
dc.format.extent | 49 | es_ES |
dc.language | Inglés | es_ES |
dc.publisher | Universitat Politècnica de València | es_ES |
dc.rights | Reserva de todos los derechos | es_ES |
dc.subject | Engine analysis | es_ES |
dc.subject | Thermodynamics | es_ES |
dc.subject | Noise emission | es_ES |
dc.subject | Turbofan design | es_ES |
dc.subject | Personal jet aviation | es_ES |
dc.subject.classification | INGENIERIA DE SISTEMAS Y AUTOMATICA | es_ES |
dc.subject.other | Grado en Ingeniería Aeroespacial-Grau en Enginyeria Aeroespacial | es_ES |
dc.title | Small turbofan for personal jet aviation design | es_ES |
dc.type | Proyecto/Trabajo fin de carrera/grado | es_ES |
dc.rights.accessRights | Cerrado | es_ES |
dc.contributor.affiliation | Universitat Politècnica de València. Escuela Técnica Superior de Ingeniería del Diseño - Escola Tècnica Superior d'Enginyeria del Disseny | es_ES |
dc.description.bibliographicCitation | Esteller Torres, A. (2014). Small turbofan for personal jet aviation design. Universitat Politècnica de València. http://hdl.handle.net/10251/52895 | es_ES |
dc.description.accrualMethod | Archivo delegado | es_ES |