Development of an unsteady potential model for a flapping wing mav

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dc.contributor.advisor Flores Arias, Óscar
dc.contributor.author Arranz Fernández, Gonzalo
dc.date.accessioned 2016-10-20T10:54:43Z
dc.date.available 2016-10-20T10:54:43Z
dc.date.issued 2015-09
dc.date.submitted 2015-10-05
dc.identifier.uri http://hdl.handle.net/10016/23759
dc.description.abstract The main objective of this project is the development of an unsteady potential code that allows to compute the aerodynamic forces of two wings with an arbitrary motion. The code must be able to reasonably predict aerodynamic forces with a low computational cost and in a fast way. In this fashion, the code will allow, in a future, to analyse di erent apping con gurations with di erent parameters, that would be impossible to analyse using high order NS based methods.
dc.format.mimetype application/pdf
dc.language.iso eng
dc.rights Atribución-NoComercial-SinDerivadas 3.0 España
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject.other Unsteady potential code
dc.subject.other Aerodynamic
dc.subject.other Micro Air Vehicles (MAV)
dc.subject.other Flapping analysis
dc.subject.other Fluid mechanics
dc.title Development of an unsteady potential model for a flapping wing mav
dc.type bachelorThesis
dc.subject.eciencia Aeronáutica
dc.rights.accessRights openAccess
dc.description.degree Ingeniería Aeroespacial
dc.contributor.departamento Universidad Carlos III de Madrid. Departamento de. Bioingeniería e Ingeniería Aeroespacial
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