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3D Navier–Stokes computations of a stall‐regulated wind turbine

A. Le Pape, +1 more
- 01 Oct 2004 - 
- Vol. 7, Iss: 4, pp 309-324
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TLDR
In this article, several 2D and 3D Navier-Stokes computations performed with the compressible elsA solver on the wind turbine tested by NREL in the NASA Ames large wind tunnel are presented.
Abstract
Several 2D and 3D Navier–Stokes computations performed with the compressible elsA solver, developed at ONERA, on the wind turbine tested by NREL in the NASA Ames large wind tunnel are presented. After a brief description of the tools and methods used, the predictions of the S809 aerofoil performance are first discussed. Full 3D computations are then presented, analysed and compared with the experimental results. The successes and failures of the computations are highlighted and explained. The analysis focuses in particular on the 3D and unsteady effects. Copyright © 2004 John Wiley & Sons, Ltd.

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Journal ArticleDOI

State of the art in wind turbine aerodynamics and aeroelasticity

TL;DR: In this article, a comprehensive review of wind turbine aeroelasticity is given, starting with the simple aerodynamic Blade Element Momentum Method and ending with giving a review of the work done applying CFD on wind turbine rotors.
Journal ArticleDOI

The Onera elsA CFD software: input from research and feedback from industry

TL;DR: The Onera elsA CFD software is both a software package capitalizing the innovative results of research over time and a multi-purpose tool for applied CFD and multi-physics.
Journal ArticleDOI

Fluid---structure interaction modeling of wind turbines: simulating the full machine

TL;DR: In this article, the aerodynamics and fluid-structure interaction (FSI) simulation of wind turbines at full scale, and in the presence of the nacelle and tower, is presented.
Journal ArticleDOI

Finite element simulation of wind turbine aerodynamics: validation study using NREL Phase VI experiment

TL;DR: In this paper, a validation study using the NREL Phase VI wind turbine is presented, where aerodynamics simulations are performed using the finite element ALE-VMS formulation augmented with weakly enforced essential boundary conditions.
Journal ArticleDOI

Ale-vms and st-vms methods for computer modeling of wind-turbine rotor aerodynamics and fluid–structure interaction

TL;DR: The related techniques described include weak enforcement of the essential boundary conditions, Kirchhoff–Love shell modeling of the rotor-blade structure, NURBS-based isogeometric analysis, and full FSI coupling.
References
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Journal ArticleDOI

Two-equation eddy-viscosity turbulence models for engineering applications

TL;DR: In this paper, two new two-equation eddy-viscosity turbulence models are presented, which combine different elements of existing models that are considered superior to their alternatives.

Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes

TL;DR: In this paper, a new combination of a finite volume discretization in conjunction with carefully designed dissipative terms of third order, and a Runge Kutta time stepping scheme, is shown to yield an effective method for solving the Euler equations in arbitrary geometric domains.
Journal ArticleDOI

Reassessment of the scale-determining equation for advanced turbulence models

David C. Wilcox
- 01 Nov 1988 - 
TL;DR: In this paper, a two-equation turbulence model is proposed that is shown to be quite accurate for attached boundary layers in adverse pressure gradient, compressible boundary layers, and free shear flows.
Journal ArticleDOI

The application of preconditioning in viscous flows

TL;DR: A time-derivative preconditioning algorithm that is effective over a wide range of flow conditions from inviscid to very diffusive flows and from low speed to supersonic flows has been developed and convergence rates are shown to be accelerated by as much as two orders of magnitudes.
Proceedings ArticleDOI

Navier-Stokes predictions of the NREL phase VI rotor in the NASA Ames 80-by-120 wind tunnel

TL;DR: In this paper, the application of an incompressible Reynolds Averaged Navier-Stokes solver to cases from the NREL/NASA Ames wind tunnel test is described.
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