AH 94-W-301 (ah94w301-il)
AH 94-W-301 - Althaus AH 94-W-301 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
|
(ah94w301-il) AH 94-W-301 Althaus AH 94-W-301 airfoil for use on wind turbines (W) Max thickness 30.1% at 30.9% chord. Max camber 1.3% at 80.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AH 94-W-301 1.00000 0.00546 0.99893 0.00599 0.99572 0.00761 0.99039 0.00993 0.98296 0.01272 0.97347 0.01568 0.96194 0.01886 0.94844 0.02231 0.93301 0.02604 0.91573 0.03007 0.89668 0.03448 0.87592 0.03927 0.85355 0.04448 0.82967 0.05011 0.80438 0.05616 0.77779 0.06261 0.75000 0.06945 0.72114 0.07660 0.69134 0.08396 0.66072 0.09145 0.62941 0.09897 0.59755 0.10641 0.56526 0.11366 0.53270 0.12058 0.50000 0.12700 0.46730 0.13273 0.43474 0.13756 0.40245 0.14127 0.37059 0.14371 0.33928 0.14476 0.30866 0.14438 0.27886 0.14251 0.25000 0.13920 0.22221 0.13458 0.19562 0.12877 0.17033 0.12193 0.14645 0.11422 0.12408 0.10579 0.10332 0.09674 0.08427 0.08721 0.06699 0.07734 0.05156 0.06723 0.03806 0.05700 0.02653 0.04678 0.01704 0.03674 0.00961 0.02701 0.00428 0.01774 0.00107 0.00886 0.00000 0.00000 0.00107 -0.01093 0.00428 -0.02602 0.00961 -0.04160 0.01704 -0.05601 0.02653 -0.06939 0.03806 -0.08188 0.05156 -0.09360 0.06699 -0.10454 0.08427 -0.11471 0.10332 -0.12404 0.12408 -0.13243 0.14645 -0.13978 0.17033 -0.14598 0.19562 -0.15093 0.22221 -0.15453 0.25000 -0.15673 0.27886 -0.15743 0.30866 -0.15662 0.33928 -0.15428 0.37059 -0.15045 0.40245 -0.14519 0.43474 -0.13865 0.46730 -0.13097 0.50000 -0.12242 0.53270 -0.11321 0.56526 -0.10361 0.59755 -0.09383 0.62941 -0.08410 0.66072 -0.07460 0.69134 -0.06548 0.72114 -0.05686 0.75000 -0.04881 0.77779 -0.04142 0.80438 -0.03475 0.82967 -0.02887 0.85355 -0.02383 0.87592 -0.01965 0.89668 -0.01630 0.91573 -0.01376 0.93301 -0.01200 0.94844 -0.01094 0.96194 -0.01041 0.97347 -0.01022 0.98296 -0.01022 0.99039 -0.01024 0.99572 -0.01032 0.99893 -0.01037 1.00000 -0.01038 |
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for AH 94-W-301 (ah94w301-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah94w301-il | 50,000 | 9 | 3.3 at α=-3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah94w301-il | 50,000 | 5 | 4.2 at α=13.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah94w301-il | 100,000 | 9 | 6.6 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah94w301-il | 100,000 | 5 | 23.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah94w301-il | 200,000 | 9 | 41.7 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah94w301-il | 200,000 | 5 | 49.2 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah94w301-il | 500,000 | 9 | 77.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah94w301-il | 500,000 | 5 | 76.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah94w301-il | 1,000,000 | 9 | 103 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah94w301-il | 1,000,000 | 5 | 99 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||