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1 to 10 of 374 Results
May 23, 2025
Appelbaum, Jason; Gibis, Tobias; Pirozzoli, Sergio; Wenzel, Christoph, 2025, "Data for: The onset of outer-layer self-similarity in turbulent boundary layers", https://doi.org/10.18419/DARUS-4165, DaRUS, V1
Averaged data from a direct numerical simulation of a zero pressure gradient turbulent boundary layer. Files in 'zt_avg_txt.tar.gz' are in plaintext, column format and contain 1D data profiles of the spanwise & temporal (z,t) averaged flow field. 1x streamwise (x) profile and >200x wall-normal (y) profiles are included. Several base variables and p...
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.
Jan 28, 2025
Gagnon, Louis; Lutz, Thorsten, 2024, "Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations", https://doi.org/10.18419/DARUS-3859, DaRUS, V4
Note for access: The data is available to anyone interested, but in order to monitor access, we ask that interested users request access by logging in by using the account of their academic institution, selecting the files they want, and clicking "Request Access" If you do not have access through your institution, please contact us by clicking "Con...
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
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