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AH 93-W-215 (ah93w215-il)

AH 93-W-215 - Althaus AH 93-W-215 airfoil for use on wind turbines (W)


Airfoil ah93w215-il
Details Dat file Parser  
(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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Selig format dat file

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Polars for AH 93-W-215 (ah93w215-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah93w215-il50,00092.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w215-il50,00056.4 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w215-il100,00096.2 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w215-il100,000527.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w215-il200,000957.6 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w215-il200,000558.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w215-il500,000993.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w215-il500,000579.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w215-il1,000,0009111.4 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w215-il1,000,000597.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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