Featured Dataverses

In order to use this feature you must have at least one published or linked dataverse.

Publish Dataverse

Are you sure you want to publish your dataverse? Once you do so it must remain published.

Publish Dataverse

This dataverse cannot be published because the dataverse it is in has not been published.

Delete Dataverse

Are you sure you want to delete your dataverse? You cannot undelete this dataverse.

Advanced Search

1 to 10 of 362 Results
Shell Script - 6.4 KB - MD5: 53475befa44d4277d8e8c8928a7d8ac8
Script to download publicly available reference data
Python Source Code - 40.2 KB - MD5: 594f1952ca98700274b0109b46093152
Plot script for 1D [x] and [y] profiles
Python Source Code - 10.3 KB - MD5: 13b3891a9fb5a40e0759b55cbd740a5e
Helper tools for loading plaintext (.txt) 1D profiles in python
Gzip Archive - 28.3 MB - MD5: b3da93dd7f3daf21e73fa07cf052aeb5
1D [x] and [y] profiles of [z,t] averaged flow field. Data files are in plaintext format.
Bzip Archive - 825.2 KB - MD5: 26e3c21b4feaec6e97f2946549496e43
Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist, 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.; see the technical note (technical-note-3Dpolars_C.pdf) for more information
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
Adobe PDF - 1.2 MB - MD5: f19b810810f8e679c4be5e3aec2927e6
This document describes the method used to obtain the airfoil tables (polars) for lift, drag, and moment using 3D URANS CFD on 193 segments for blade 022 within a one-third turbine model simulation.
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
Add Data

Log in to create a dataverse or add a dataset.

Share Dataverse

Share this dataverse on your favorite social media networks.

Link Dataverse
Reset Modifications

Are you sure you want to reset the selected metadata fields? If you do this, any customizations (hidden, required, optional) you have done will no longer appear.