AH 93-W-480B (ah93w480b-il)
AH 93-W-480B - Althaus AH 93-W-480B airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
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(ah93w480b-il) AH 93-W-480B Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord. Max camber 3.6% at 44.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AH 93-W-480B 1.00000 0.10990 0.99991 0.11047 0.99702 0.12519 0.99467 0.12550 0.99156 0.12944 0.98761 0.13418 0.98269 0.13963 0.97663 0.14571 0.96914 0.15226 0.95951 0.15889 0.94687 0.16510 0.93154 0.17089 0.91484 0.17700 0.89683 0.18345 0.87746 0.19016 0.85671 0.19707 0.83458 0.20414 0.81108 0.21128 0.78621 0.21845 0.75996 0.22556 0.73234 0.23254 0.70337 0.23930 0.67306 0.24577 0.64142 0.25186 0.60848 0.25746 0.57424 0.26246 0.53872 0.26671 0.50195 0.27004 0.46398 0.27217 0.42498 0.27280 0.38522 0.27162 0.34517 0.26832 0.30548 0.26269 0.26697 0.25468 0.23044 0.24443 0.19655 0.23228 0.16567 0.21864 0.13802 0.20391 0.11372 0.18849 0.09264 0.17274 0.07435 0.15692 0.05859 0.14126 0.04523 0.12592 0.03415 0.11107 0.02516 0.09682 0.01805 0.08330 0.01257 0.07058 0.00847 0.05874 0.00553 0.04785 0.00351 0.03796 0.00215 0.02907 0.00123 0.02112 0.00058 0.01403 0.00000 0.00042 0.00025 -0.00830 0.00032 -0.00946 0.00046 -0.01129 0.00072 -0.01406 0.00115 -0.01781 0.00184 -0.02259 0.00290 -0.02834 0.00444 -0.03498 0.00664 -0.04245 0.00965 -0.05073 0.01369 -0.05980 0.01898 -0.06963 0.02574 -0.08018 0.03423 -0.09134 0.04471 -0.10303 0.05744 -0.11510 0.07270 -0.12735 0.09072 -0.13953 0.11163 -0.15130 0.13530 -0.16225 0.16140 -0.17205 0.18948 -0.18053 0.21906 -0.18760 0.24970 -0.19329 0.28104 -0.19769 0.31278 -0.20095 0.34472 -0.20324 0.37672 -0.20471 0.40869 -0.20549 0.44056 -0.20568 0.47226 -0.20535 0.50371 -0.20453 0.53483 -0.20331 0.56557 -0.20172 0.59584 -0.19982 0.62560 -0.19766 0.65477 -0.19529 0.68330 -0.19274 0.71111 -0.19006 0.73816 -0.18728 0.76437 -0.18444 0.78970 -0.18158 0.81408 -0.17873 0.83744 -0.17591 0.85975 -0.17316 0.88092 -0.17050 0.90093 -0.16796 0.91970 -0.16555 0.93728 -0.16339 0.95313 -0.16089 0.96562 -0.15681 0.97473 -0.15180 0.98164 -0.14685 0.98703 -0.14232 0.99125 -0.13834 0.99451 -0.13504 0.99695 -0.13215 0.99966 -0.12444 1.00000 -0.12402 |
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Polars for AH 93-W-480B (ah93w480b-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah93w480b-il | 50,000 | 9 | 7.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 50,000 | 5 | 11.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 100,000 | 9 | 18.3 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 100,000 | 5 | 20.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 200,000 | 9 | 21.4 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 200,000 | 5 | 22.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 500,000 | 9 | 24.9 at α=14.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 500,000 | 5 | 23.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah93w480b-il | 1,000,000 | 9 | 28 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah93w480b-il | 1,000,000 | 5 | 26.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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