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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.
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