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AH 94-W-301 (ah94w301-il)

AH 94-W-301 - Althaus AH 94-W-301 airfoil for use on wind turbines (W)


Airfoil ah94w301-il
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
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Selig format dat file

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Polars for AH 94-W-301 (ah94w301-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah94w301-il50,00093.3 at α=-3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il50,00054.2 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il100,00096.6 at α=0°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il100,000523.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il200,000941.7 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il200,000549.2 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il500,000977.5 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il500,000576.9 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il1,000,0009103 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il1,000,000599 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
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