NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa)
NACA0012H for VAWT from Sandia report SAND80-2114 - Modified Naca 0012 airfoil for Sandia VAWT tests
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(naca0012h-sa) NACA0012H for VAWT from Sandia report SAND80-2114 Modified Naca 0012 airfoil for Sandia VAWT tests Max thickness 12.2% at 22.5% chord. Max camber 0% at 0% chord Source Sandia National Laboratories Source dat file The dat file is in Selig format |
NACA0012H for VAWT from Sandia report SAND80-2114 1.00000 0.00126 0.95000 0.00807 0.90000 0.01448 0.85000 0.02053 0.80000 0.02623 0.75000 0.03160 0.70000 0.03664 0.65000 0.04133 0.60000 0.04563 0.55000 0.04952 0.50000 0.05294 0.44900 0.05588 0.39900 0.05808 0.34900 0.05951 0.29900 0.06002 0.27500 0.06048 0.25000 0.06084 0.22500 0.06100 0.20000 0.06087 0.17500 0.06033 0.15000 0.05924 0.12500 0.05740 0.10000 0.05454 0.08000 0.05121 0.06000 0.04655 0.05000 0.04351 0.04000 0.03982 0.03000 0.03522 0.02000 0.02925 0.01000 0.02074 0.00500 0.01438 0.00000 0.00000 0.00500 -0.01438 0.01000 -0.02074 0.02000 -0.02925 0.03000 -0.03522 0.04000 -0.03982 0.05000 -0.04351 0.06000 -0.04655 0.08000 -0.05121 0.10000 -0.05454 0.12500 -0.05740 0.15000 -0.05924 0.17500 -0.06033 0.20000 -0.06087 0.22500 -0.06100 0.25000 -0.06084 0.27500 -0.06048 0.29900 -0.06002 0.34900 -0.05951 0.39900 -0.05808 0.44900 -0.05588 0.50000 -0.05294 0.55000 -0.04952 0.60000 -0.04563 0.65000 -0.04133 0.70000 -0.03664 0.75000 -0.03160 0.80000 -0.02623 0.85000 -0.02053 0.90000 -0.01448 0.95000 -0.00807 1.00000 -0.00126 |
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Polars for NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| naca0012h-sa | 50,000 | 9 | 20.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 50,000 | 5 | 22.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 100,000 | 9 | 28.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 100,000 | 5 | 33.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 200,000 | 9 | 41.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 200,000 | 5 | 46.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 500,000 | 9 | 63.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 500,000 | 5 | 66.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0012h-sa | 1,000,000 | 9 | 82 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0012h-sa | 1,000,000 | 5 | 81.9 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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