Comparison of efficient uncertainty quantification techniques on a transonic airfoil, using rans computations and adjoint method

Autor: Bennehard, Quentin, Peter, Jacques, Carini, Marco

Publikováno v: EUROGEN 2023-15th ECCOMAS Thematic Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control
EUROGEN 2023-15th ECCOMAS Thematic Conference on Evolutionary and Deterministic Methods for Design, Optimization and Control, Jun 2023, Chania, Greece

International audience; This paper presents a comparison among efficient techniques for uncertainty quantification on the RAE2822 airfoil whose shape is affected by uncertain geometrical parameters. Transonic conditions are considered with focus on e

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______3379::d8930505a53dd06d3c3027a81222e201
https://hal.science/hal-04153874

URANS Computations of Shock-Induced Oscillations Over 2D Rigid Airfoils: Influence of Test Section Geometry.

Autor: Mylène Thiery, Eric Coustols

Publikováno v: Flow, Turbulence & Combustion; Jun2005, Vol. 74 Issue 4, p331-354, 24p

Physique et modélisation d'interactions instationnaires onde de choc/couche limite autour de profils d'aile transsoniques par simulation numérique

Autor: Grossi, Fernando

L’interaction onde de choc/couche limite en écoulement transsonique autour de profils aérodynamiques est étudiée numériquement utilisant différentes classes de modélisation de la turbulence. Les approches utilisées sont celles de modèles U

Externí odkaz: http://www.theses.fr/2014INPT0015/document