Memorias de investigación
Ponencias en congresos:
Adaptation of the computational grid to a moving wing-fuselage
Año:2014
Áreas de investigación
  • Ingeniería aeronaútica
Datos
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
Participantes
Grupos de investigación, Departamentos, Centros e Institutos de I+D+i relacionados
  • Creador: Departamento: Matemática Aplicada a la Ingeniería Aeroespacial