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

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Licence d’utilisation du document

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]

Langue

Communication dans un congrès

Ce document a été publié dans

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

Résumé en anglais

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.< Réduire

URI

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

Projet Européen

Adaptive Schemes for Deterministic and Stochastic Flow Problems

Origine

Importé de hal

Unités de recherche

Institut de Mathématiques de Bordeaux (IMB) - UMR 5251