AH 93-W-300 (ah93w300-il)
AH 93-W-300 - Althaus AH 93-W-300 airfoil for use on wind turbines (W)
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(ah93w300-il) AH 93-W-300 Althaus AH 93-W-300 airfoil for use on wind turbines (W) Max thickness 30% at 27.9% chord. Max camber 1.6% at 72.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AH 93-W-300 1.00000 0.00040 0.99893 0.00084 0.99572 0.00223 0.99039 0.00448 0.98296 0.00714 0.97347 0.01034 0.96194 0.01391 0.94844 0.01794 0.93301 0.02247 0.91573 0.02749 0.89668 0.03301 0.87592 0.03898 0.85355 0.04538 0.82967 0.05214 0.80438 0.05924 0.77779 0.06663 0.75000 0.07425 0.72114 0.08204 0.69134 0.08989 0.66072 0.09773 0.62941 0.10545 0.59755 0.11293 0.56526 0.12007 0.53270 0.12678 0.50000 0.13295 0.46730 0.13847 0.43474 0.14328 0.40245 0.14732 0.37059 0.15048 0.33928 0.15265 0.30866 0.15373 0.27886 0.15369 0.25000 0.15250 0.22221 0.15019 0.19562 0.14673 0.17033 0.14219 0.14645 0.13663 0.12408 0.13010 0.10332 0.12264 0.08427 0.11428 0.06699 0.10511 0.05156 0.09522 0.03806 0.08466 0.02653 0.07336 0.01704 0.06094 0.00961 0.04688 0.00428 0.03126 0.00107 0.01517 0.00000 0.00000 0.00107 -0.01592 0.00428 -0.03035 0.00961 -0.04373 0.01704 -0.05600 0.02653 -0.06726 0.03806 -0.07773 0.05156 -0.08764 0.06699 -0.09707 0.08427 -0.10604 0.10332 -0.11440 0.12408 -0.12204 0.14645 -0.12885 0.17033 -0.13467 0.19562 -0.13938 0.22221 -0.14291 0.25000 -0.14519 0.27886 -0.14615 0.30866 -0.14578 0.33928 -0.14406 0.37059 -0.14101 0.40245 -0.13668 0.43474 -0.13120 0.46730 -0.12466 0.50000 -0.11723 0.53270 -0.10922 0.56526 -0.10085 0.59755 -0.09227 0.62941 -0.08368 0.66072 -0.07522 0.69134 -0.06704 0.72114 -0.05924 0.75000 -0.05190 0.77779 -0.04512 0.80438 -0.03890 0.82967 -0.03330 0.85355 -0.02835 0.87592 -0.02409 0.89668 -0.02052 0.91573 -0.01767 0.93301 -0.01551 0.94844 -0.01400 0.96194 -0.01310 0.97347 -0.01272 0.98296 -0.01278 0.99039 -0.01298 0.99572 -0.01337 0.99893 -0.01362 1.00000 -0.01369 |
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Polars for AH 93-W-300 (ah93w300-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah93w300-il | 50,000 | 9 | 4.2 at α=-2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w300-il | 50,000 | 5 | 5.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w300-il | 100,000 | 9 | 17.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w300-il | 100,000 | 5 | 27.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w300-il | 200,000 | 9 | 42.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w300-il | 200,000 | 5 | 41 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w300-il | 500,000 | 9 | 61.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w300-il | 500,000 | 5 | 58.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w300-il | 1,000,000 | 9 | 80.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w300-il | 1,000,000 | 5 | 74.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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