Статья

Turbulent Flow Simulation of the NREL S809 Airfoil

Ouahiba GuerriCentre de Développement des Energies Renouvelables, Cidex 01, BP 102, Bouzaréah, CP16340, Alger, AlgeriaKhadidja BouhadefUniversité des Sciences et Techniques Houari Boumediène, BP 32, El Alia, Bab Ezzouar, CP 16111, AlgeriaAmeziane HarhadLouisiana State University, Department of Mathematics, P.O. Box 22205, Baton Rouge, La 70894, USA

2006en

ABI

Аннотация

Numerical computations are carried out for the NREL S809 airfoil. The flow is modelled using an unsteady incompressible Reynolds Averaged Navier-Stokes solver. Two turbulence models (SST k/ω of Menter and RNG k/ε) are applied to close the RANS equations. All computations are performed assuming fully turbulent flow. The flow field is analyzed at various angles of attack from 0 to 20 degrees. Lift and drag forces are obtained from the computations by integrating the pressure and shear stress over the blade surface. The performance of the two turbulence models is compared and the influence of the free stream turbulence intensity is checked. The results confirm the satisfactory performance of the SST k/ω model of Menter for modelling turbulent flow around airfoils.

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Идентификаторы

DOI: 10.1260/030952406779295471

Цитирования и источники

Цитирований: 2Использованных источников: 0

Показатели — AkademScholar