ABGRALL, Remi; CONGEDO, Pietro Marco; GALERA, Stéphane; GERACI, Gianluca

Metadatos

Licencia de uso del documento

ABGRALL, Remi
Parallel tools for Numerical Algorithms and Resolution of essentially Hyperbolic problems [BACCHUS]
Institut de Mathématiques de Bordeaux [IMB]

CONGEDO, Pietro Marco
Parallel tools for Numerical Algorithms and Resolution of essentially Hyperbolic problems [BACCHUS]
Institut de Mathématiques de Bordeaux [IMB]

GALERA, Stéphane
Parallel tools for Numerical Algorithms and Resolution of essentially Hyperbolic problems [BACCHUS]

Idioma

Communication dans un congrès

Este ítem está publicado en

4TH EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES, 2011-07-04, Saint Petersburg. 2011-07-04

Resumen en inglés

In this work we present semi-intrusive and non-intrusive techniques for uncertainties quantiﬁcation (UQ) in the context of the solution of partial diﬀerential equations, with a speciﬁc application to aerodynamics problems. These methods has been applied successfully to a supersonic nozzle ﬂow and the analysis of an inviscid transonic ﬂow over a RAE 2822 airfoil. In this case, we consider three uncertainties, on the Mach number, the angle of attack and the heat coeﬃcient ratio and the numerical results are compared with experimental data.< Leer menos

URI

https://oskar-bordeaux.fr/handle/20.500.12278/189990

Proyecto europeo

Adaptive Schemes for Deterministic and Stochastic Flow Problems

Orígen

Importado de Hal

Centros de investigación

Institut de Mathématiques de Bordeaux (IMB) - UMR 5251