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Simulation of an aircraft

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Simulation of an aircraft

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dc.contributor.advisor Ballester Sarrias, Enrique es_ES
dc.contributor.author Soriano Torres, Juan es_ES
dc.date.accessioned 2020-01-27T12:37:43Z
dc.date.available 2020-01-27T12:37:43Z
dc.date.created 2015-09-10
dc.date.issued 2020-01-27
dc.identifier.uri http://hdl.handle.net/10251/135692
dc.description.abstract [EN] This thesis calculates the aerodynamic coefficients and forces of the aircraft and refines the mesh. From the given fuselage to the point with the complete aircraft with wings and horizontal stabilizer, the program used to mesh is ICEM CFD and to compare forces and fluid dynamics interactions between air and body is used ANSYS Fluent®. One of the objectives of the project is also the improvement of the quality of the given mesh in order to obtain more accurate results. It is possible by changing distributions and moving vertexes to avoid big jumps in the different zones of the mesh. Related to ANSYS Fluent®, special attention is paid to the choice of the turbulence models according to the best results in the previous calculations and to the geometry and intended purpose. That is the reason for choosing the Shear Stress Transport k-omega. The comparison between the configuration without wings and without horizontal stabilizer with the complete configuration with those components confirms the expected difference in lift and drag. The complexity of the mesh gives still the possibility to improve its quality. es_ES
dc.format.extent 57 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 Aerodiamics coefficients es_ES
dc.subject ICEM CFD es_ES
dc.subject Horizontal stabilizer es_ES
dc.subject Aircraft 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 Simulation of an aircraft 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 Soriano Torres, J. (2015). Simulation of an aircraft. http://hdl.handle.net/10251/135692 es_ES
dc.description.accrualMethod Archivo delegado es_ES


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