RANS simulations of flow past an DU-91-W2-250 airfoil at high Reynolds number

Research output: Research - peer-reviewConference article – Annual report year: 2018

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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.
Original languageEnglish
Article number00150
JournalE3S Web of Conferences
Volume44
Number of pages8
ISSN2267-1242
DOIs
StatePublished - 2018
CitationsWeb of Science® Times Cited: No match on DOI
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