A Parallelized Coupled Navier-Stokes/Vortex-Panel Solver

Author:

Schmitz Sven1,Chattot Jean-Jacques1

Affiliation:

1. Department of Mechanical and Aeronautical Engineering, University of California Davis, One Shields Ave, Davis, CA 95616-5294

Abstract

A Navier-Stokes solver, CFX V5.6, is coupled with an in-house developed Vortex-Panel method for the numerical analysis of wind turbines. The Navier-Stokes zone is confined to the near-field around one wind turbine blade, the Vortex-Panel method models the entire vortex sheet of a two-bladed rotor and accounts for the far-field. This coupling methodology reduces both numerical diffusion and computational cost. The parallelized coupled solver (PCS) is applied to the NREL Phase VI rotor configuration under no-yaw conditions. Fully turbulent flow is assumed using the k - ϵ and k - ω turbulence models. Results obtained are very encouraging for fully attached flow. For separated and partially stalled flow, results are in good agreement with experimental data. Discrepancies observed between the turbulence models are attributed to different prediction of the onset of separation. This is revealed by two-dimensional (2D) results of the S809 airfoil.

Publisher

ASME International

Subject

Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment

Reference31 articles.

1. Fingersh, L. J., Simms, D., Hand, M., Jager, D., Cotrell, J., Robinson, M., Schreck, S., Larwood, S., 2001, “Wind Tunnel Testing of NREL’s Unsteady Aerodynamics Experiment,” AIAA-2001-0035, pp. 194–200.

2. Simms, D., Schreck, S., Hand, M., Fingersh, L. J., 2001, “NREL Unsteady Aerodynamics Experiment in the NASA-Ames Wind Tunnel: A Comparison of Predictions to Measurements,” NREL/TP-500-29494.

3. Evaluation of 3D effects from 3D CFD computations;Sorensen

4. Navier-Stokes Predictions of the NREL Phase VI Rotor in the NASA Ames 80ft×120ft Wind Tunnel;Sorensen;Wind Energy

5. Sorensen, N. N., Michelsen, J. A., Schreck, S., 2002, “Application of CFD to Wind Turbine Aerodynamics,” GRACM 2002, Patra.

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