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dc.contributorFlores Le Roux, Roberto Maurice
dc.contributor.authorMoral Cejudo, Miguel Alejandro del
dc.date.accessioned2015-11-20T18:29:56Z
dc.date.available2015-11-20T18:29:56Z
dc.date.issued2015-04
dc.identifier.urihttp://hdl.handle.net/2117/79535
dc.description.abstractIn this study a Computational Fluid Dynamics (CFD) code to solve the two-dimensional subsonic flow around simple geometry airfoils is developed. The presented method departs from the Euler equations and through a finite-volume explicit time-marching method produces the solution of all the variables of the potential flow. Furthermore, some variations of the main code using different discretization schemes are used in order to compare their results. Also a simple meshing code was also designed and included in the main software in order to produce the structured grid the solver works with. The fundamentals of all of them are also presented in this study along with a detailed explanation of the software's functioning and a proper validation of the results. Finally, further code improvements are suggested
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Enginyeria mecànica
dc.subject.lcshComputational fluid dynamics
dc.subject.lcshFluid dynamics--Mathematical models
dc.titleStudy of numerical methods for the solution of compressible external flows
dc.typeMaster thesis (pre-Bologna period)
dc.subject.lemacDinámica de fluids computacional
dc.subject.lemacDinàmica de fluids -- Mètodes numèrics
dc.rights.accessOpen Access
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola Tècnica Superior d'Enginyeries Industrial i Aeronàutica de Terrassa
dc.audience.degreeENGINYERIA AERONÀUTICA (Pla 2004)


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