E3S Web Conf.
Volume 44, 201810th Conference on Interdisciplinary Problems in Environmental Protection and Engineering EKO-DOK 2018
|Number of page(s)||8|
|Published online||03 July 2018|
RANS Simulations of Flow Past an DU-91-W2-250 Airfoil at High Reynolds Number
Institute of Theoretical and Applied Mechanics, Warsaw University of Technology, Warsaw, 00-665, Poland
2 DTU Wind Energy, Technical University of Denmark, Lyngby, 2800 Kgs, Denmark
* Corresponding author : email@example.com
This paper presents numerical results of the DU-91-W2-250 airfoil. Reynolds-averaged Navier–Stokes (RANS) simulations of the 2D profile are performed employing the Transient SST turbulence model. The airfoil was investigated for the Reynolds number of 6 106. Lift and drag coefficients are compared with the experimental data from LM Low Speed Wind Tunnel (LSWT). The results of lift and drag coefficients obtained using the SST Transient model are in a good agreement in comparison with the experiment in the angle of attack range from -10° to 10°. The static pressure distributions calculated by the SST Transition model are also in good agreement with the experiment.
© The Authors, published by EDP Sciences, 2018
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