2005
DOI: 10.1080/14685240500209981
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Vortex method for simulation of a 3D round jet in a cross-stream

Abstract: In this paper, the three-dimensional (3D) flow of a jet in a crossflow was investigated. This is a numerical study based on a vortex particle method. In order to account for the lower length scales, a crude LES turbulence model was implemented together with a regridding procedure. The numerical simulation was done with an injection ratio R inj = W jet /U ∞ = 4.0. The code was run until an averaged steady state of the jet was reached. The resulting vortex structures were shown to be consistent with previously p… Show more

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Cited by 8 publications
(11 citation statements)
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“…Those particles are emitted at the trailing edge of the obstacle according to the Kutta-Joukowski condition and then advected in a Lagrangian frame thanks to the Navier-Stokes equations for an incompressible flow. The details of the method are presented in [11,17].…”
Section: Comparison With Numerical Resultsmentioning
confidence: 99%
“…Those particles are emitted at the trailing edge of the obstacle according to the Kutta-Joukowski condition and then advected in a Lagrangian frame thanks to the Navier-Stokes equations for an incompressible flow. The details of the method are presented in [11,17].…”
Section: Comparison With Numerical Resultsmentioning
confidence: 99%
“…Both power and thrust coefficients (C P and C T ) predictions and wake characterisation are presented and discussed. To this purpose, three-dimensional software, initially issuing from [23,24] is being developed in order to assess the disturbances generated in the sea. This is an unsteady Lagrangian frame software designed to compute the evolution of the wake emitted by the turbine.…”
Section: Introductionmentioning
confidence: 99%
“…Le code de simulation numérique de l'écoulement autour d'une hydrolienne est basé sur une méthode Lagrangienne particulaire et présenté en détail dans (PINON et al, 2005 ;PINON et al, 2012). Les équations de Navier-Stokes sont formulées en vitesse / vorticité ( , ) u ω pour un fluide Newtonien incompressible : 2.1 Composante potentielle de la vitesse L'hydrolienne (les 3 pales et la partie centrale) est prise en compte par une méthode intégrale de frontière (cf.…”
Section: Méthode Numérique Utiliséeunclassified