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Gzip Archive - 28.3 MB - MD5: b3da93dd7f3daf21e73fa07cf052aeb5
1D [x] and [y] profiles of [z,t] averaged flow field. Data files are in plaintext format.
WebM Video - 78.9 MB - MD5: d1373aef10a99384f31f284c8173038b
Video of the lift, drag and moment coefficient plots from segment 0 to 192 of blade 022 and computed using 3D URANS CFD (one-third model), compared with the 2D coefficients, and shown along with each airfoil shape; see the technical note (technical-note-3Dpolars_C.pdf) for more information
WebM Video - 12.1 MB - MD5: c12235fc00e631cc3d12fab78741bce0
video of the lift, drag and moment coefficient plots from segment 0 to 192 of blade 008 and computed using 2D RANS CFD
Bzip Archive - 687.4 KB - MD5: b82ce4aaad70277039408c70f82410b0
Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist, BlCrvAC, BlSwpA and thickness to chord ratio] and airfoil coordinates; for the 193 cross-sectional segments of blade 008 of the southern wind turbine at the WINSENT test site.
WebM Video - 12.1 MB - MD5: f4feec5696d4674185ec96fb0feb7564
video of the lift, drag and moment coefficient plots from segment 0 to 192 of blade 022 and computed using 2D RANS CFD
Bzip Archive - 685.9 KB - MD5: 1585a54c41c5e059211c5f95511cdd0c
Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist, BlCrvAC, BlSwpA and thickness to chord ratio] and airfoil coordinates; for the 193 cross-sectional segments of blade 022 of the southern wind turbine at the WINSENT test site.
WebM Video - 12.1 MB - MD5: 768f2c2a7e829f57f8caa391802cc69b
video of the lift, drag and moment coefficient plots from segment 0 to 192 of blade 025 and computed using 2D RANS CFD
Bzip Archive - 692.8 KB - MD5: 348fc1abad9364098e4679658cd601a9
Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist, BlCrvAC, BlSwpA and thickness to chord ratio] and airfoil coordinates; for the 193 cross-sectional segments of blade 025 of the southern wind turbine at the WINSENT test site.
Adobe PDF - 601.7 KB - MD5: db765ef5f2bb4eedc6453747d1c885a0
This document describes the method used to obtain the airfoil tables (polars) for lift, drag, and moment using 2D RANS CFD on 193 segments for each of the 3 blades.
model/iges - 10.4 KB - MD5: 292e1c96d3e6287c3b9980d3c2eed118
WINSENT Wind turbine geometry, approximate, but close to reality: Laser-scan generated CAD iges file of the wind turbine tower, version_2 (small dimension corrections). The tower is rotated away from the z-axis by 3.46° along the y-axis to account for the rotor shaft angle, aligning with the blade located at the bottommost position. The blade's spa...
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