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Descripción
This paper proposes two approaches to automatically adapt the computa- tional grid at the presence of moving intersections between surface components, such as wing-fuselage assemblies. The ?rst method is based on the underlying CAD de?nition, which is represented by Non-Uniform Rational B-Splines (NURBS). The second method employs Radial Basis Functions (RBFs). Both methods have been tested to ?x the surface grid of an DLR F6 wing-body con?guration, where the wing geometry has been deformed at the intersection with the fuselage. The proposed strategies are suitable for both struc- tured and unstructured computational grids and can be deployed in an industrial context to adapt the computational grid upon deformations of surface components
Internacional	Si
Nombre congreso	ECCOMAS de 2014
Tipo de participación	960
Lugar del congreso	Barcelona
Revisores	Si
ISBN o ISSN	978-84-942844-7-2
DOI
Fecha inicio congreso	20/07/2014
Fecha fin congreso	25/07/2014
Desde la página	5536
Hasta la página	5546
Título de las actas	Proceedings of Conference on Modelling and Simulation (2014), Vol 5,

Esta actividad pertenece a memorias de investigación

• Autor: Mario J. Martín Burgos
• Autor: Marta Amalia Cordero Gracia (UPM)
• Autor: Mariola Gomez Lopez (UPM)

• Creador: Departamento: Matemática Aplicada a la Ingeniería Aeroespacial