In this survey paper transitional turbulence modeling is approached from the point of view
relevant to small unmanned aerial vehicles (span≈ 1 m), of which the flow is characterized …

The turbine of an aircraft engine involves a multi-disciplinary coupling problem that interacts
among the flow field, temperature field and solid structure. This study focuses on conducting …

Algebraic transitional extensions for the accurate computation of laminar separation bubbles
are developed for use with k− ω models. The transitional model, based on integral boundary …

2 ρ∞| u∞| 2) us= velocity component projected onto s direction (ms− 1) f tr= Transition
function us= velocity component projected onto s direction (ms− 1) H= boundary-layer …

The elsA CFD software developed at ONERA is both a software package capitalizing the
innovative results of research over time and a multipurpose tool for applied CFD and for …

The flow within low pressure turbines (LPTs) at high altitudes is essentially complex,
involving formation of separation bubbles and separation-induced transition. These …

L'objectif de cette thèse est de faire progresser la modélisation de la transition de couche
limite sur des aubes de turbines basse-pression fortement chargées. Cette modélisation …

This paper presents an extension of the γ-R θ t~ transition model of Menter et al.(2006) that
aims to take into account the effect of a specific type of surface roughness on the transition …

Flow past a high-lift low-pressure turbine (LPT) blade in a cascade could be quite complex
as phenomena like separation and transition are often involved. For a highly loadedT106A …

Le but de cette thèse est de proposer des modèles qui améliorent la précision des
prévisions RANS des bulbes de décollement laminaire. Dans un premier temps, des …