AH 93-W-215 (ah93w215-il)
AH 93-W-215 - Althaus AH 93-W-215 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
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(ah93w215-il) AH 93-W-215 Althaus AH 93-W-215 airfoil for use on wind turbines (W) Max thickness 21.2% at 33.9% chord. Max camber 3.1% at 40.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AH 93-W-215 1.00000 -0.00087 0.99893 -0.00031 0.99572 0.00140 0.99039 0.00394 0.98296 0.00713 0.97347 0.01042 0.96194 0.01376 0.94844 0.01732 0.93301 0.02116 0.91573 0.02529 0.89668 0.02974 0.87592 0.03453 0.85355 0.03970 0.82967 0.04524 0.80438 0.05112 0.77779 0.05738 0.75000 0.06404 0.72114 0.07108 0.69134 0.07846 0.66072 0.08613 0.62941 0.09396 0.59755 0.10178 0.56526 0.10935 0.53270 0.11640 0.50000 0.12261 0.46730 0.12778 0.43474 0.13174 0.40245 0.13444 0.37059 0.13589 0.33928 0.13613 0.30866 0.13520 0.27886 0.13315 0.25000 0.13001 0.22221 0.12584 0.19562 0.12069 0.17033 0.11463 0.14645 0.10774 0.12408 0.10011 0.10332 0.09182 0.08427 0.08299 0.06699 0.07370 0.05156 0.06409 0.03806 0.05429 0.02653 0.04447 0.01704 0.03471 0.00961 0.02520 0.00428 0.01618 0.00107 0.00785 0.00000 0.00000 0.00107 -0.00781 0.00428 -0.01556 0.00961 -0.02312 0.01704 -0.03032 0.02653 -0.03706 0.03806 -0.04326 0.05156 -0.04891 0.06699 -0.05399 0.08427 -0.05851 0.10332 -0.06248 0.12408 -0.06591 0.14645 -0.06882 0.17033 -0.07125 0.19562 -0.07321 0.22221 -0.07473 0.25000 -0.07581 0.27886 -0.07641 0.30866 -0.07651 0.33928 -0.07607 0.37059 -0.07504 0.40245 -0.07341 0.43474 -0.07118 0.46730 -0.06839 0.50000 -0.06508 0.53270 -0.06137 0.56526 -0.05734 0.59755 -0.05308 0.62941 -0.04868 0.66072 -0.04420 0.69134 -0.03967 0.72114 -0.03516 0.75000 -0.03069 0.77779 -0.02633 0.80438 -0.02215 0.82967 -0.01823 0.85355 -0.01465 0.87592 -0.01146 0.89668 -0.00871 0.91573 -0.00646 0.93301 -0.00472 0.94844 -0.00345 0.96194 -0.00267 0.97347 -0.00231 0.98296 -0.00203 0.99039 -0.00182 0.99572 -0.00136 0.99893 -0.00098 1.00000 -0.00087 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for AH 93-W-215 (ah93w215-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah93w215-il | 50,000 | 9 | 2.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w215-il | 50,000 | 5 | 6.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w215-il | 100,000 | 9 | 6.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w215-il | 100,000 | 5 | 27.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w215-il | 200,000 | 9 | 57.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w215-il | 200,000 | 5 | 58.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w215-il | 500,000 | 9 | 93.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w215-il | 500,000 | 5 | 79.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w215-il | 1,000,000 | 9 | 111.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w215-il | 1,000,000 | 5 | 97.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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