AH 93-W-145 (ah93w145-il)
AH 93-W-145 - Althaus AH 93-W-145 airfoil for use on wind turbines (W)
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(ah93w145-il) AH 93-W-145 Althaus AH 93-W-145 airfoil for use on wind turbines (W) Max thickness 14.5% at 33.9% chord. Max camber 3.9% at 37.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AH 93-W-145 1.00000 0.00033 0.99893 0.00067 0.99572 0.00172 0.99039 0.00330 0.98296 0.00533 0.97347 0.00775 0.96194 0.01054 0.94844 0.01364 0.93301 0.01699 0.91573 0.02056 0.89668 0.02435 0.87592 0.02838 0.85355 0.03269 0.82967 0.03730 0.80438 0.04225 0.77779 0.04751 0.75000 0.05305 0.72114 0.05880 0.69134 0.06472 0.66072 0.07075 0.62941 0.07682 0.59755 0.08286 0.56526 0.08882 0.53270 0.09454 0.50000 0.09979 0.46730 0.10427 0.43474 0.10771 0.40245 0.10996 0.37059 0.11094 0.33928 0.11066 0.30866 0.10919 0.27886 0.10668 0.25000 0.10325 0.22221 0.09904 0.19562 0.09414 0.17033 0.08864 0.14645 0.08263 0.12408 0.07617 0.10332 0.06933 0.08427 0.06218 0.06699 0.05480 0.05156 0.04727 0.03806 0.03970 0.02653 0.03216 0.01704 0.02478 0.00961 0.01774 0.00428 0.01121 0.00107 0.00533 0.00000 0.00000 0.00107 -0.00496 0.00428 -0.00964 0.00961 -0.01394 0.01704 -0.01787 0.02653 -0.02138 0.03806 -0.02442 0.05156 -0.02702 0.06699 -0.02921 0.08427 -0.03101 0.10332 -0.03246 0.12408 -0.03356 0.14645 -0.03436 0.17033 -0.03489 0.19562 -0.03521 0.22221 -0.03535 0.25000 -0.03531 0.27886 -0.03510 0.30866 -0.03473 0.33928 -0.03417 0.37059 -0.03342 0.40245 -0.03249 0.43474 -0.03137 0.46730 -0.03007 0.50000 -0.02860 0.53270 -0.02698 0.56526 -0.02523 0.59755 -0.02336 0.62941 -0.02140 0.66072 -0.01937 0.69134 -0.01728 0.72114 -0.01516 0.75000 -0.01303 0.77779 -0.01090 0.80438 -0.00882 0.82967 -0.00685 0.85355 -0.00506 0.87592 -0.00348 0.89668 -0.00215 0.91573 -0.00114 0.93301 -0.00048 0.94844 -0.00016 0.96194 -0.00012 0.97347 -0.00030 0.98296 -0.00064 0.99039 -0.00102 0.99572 -0.00135 0.99893 -0.00157 1.00000 -0.00162 |
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Polars for AH 93-W-145 (ah93w145-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah93w145-il | 50,000 | 9 | 6.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w145-il | 50,000 | 5 | 18.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w145-il | 100,000 | 9 | 41.9 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w145-il | 100,000 | 5 | 49.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w145-il | 200,000 | 9 | 79.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w145-il | 200,000 | 5 | 80.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w145-il | 500,000 | 9 | 120.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w145-il | 500,000 | 5 | 116.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w145-il | 1,000,000 | 9 | 151.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w145-il | 1,000,000 | 5 | 139.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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