Observatorio de I+D+i UPM

Descripción
Optimal aerodynamic shape design aims to find the minimum of a functional that de- scribes an aerodynamic characteristic, by controlling the PDE modelling the dynamics of the flow that surrounds an aircraft, by using surface deformation techniques. As a solution to the enormous computational resources required for classical shape optimization of func- tionals of aerodynamic interest, probably the best strategy is to apply methods inspired in control theory. One of the key ingredients relies on the usage of the adjoint methodology in order to simplify the computation of gradients. In this paper we will restrict our attention to optimal shape design in two dimensional systems governed by the steady Euler equations for flows whose steady-state solutions present discontinuities in the flow variables (an isolated shock wave)
Internacional	Si
JCR del ISI	Si
Título de la revista	AIAA JOURNAL
ISSN	0001-1452
Factor de impacto JCR	1,025
Información de impacto
Volumen	47
DOI
Número de revista	3
Desde la página	552
Hasta la página	562
Mes	MARZO
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Esta actividad pertenece a memorias de investigación

• Co-autor: Antonio Baeza (Madrid Institute for Advanced Studies in Mathematics)
• Co-autor: Enrique Zuazua (Basque Center for Applied Mathematics)
• Autor: Carlos Manuel Castro Barbero (UPM)
• Co-autor: Francisco Palacios (Madrid Institute for Advanced Studies in Mathematics)

• Creador: Grupo de Investigación: Cálculo estructural aplicado a la Ing. Civil
• Departamento: Matemática e Informática Aplicadas a la Ingeniería Civil