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AH 93-W-300 (ah93w300-il)

AH 93-W-300 - Althaus AH 93-W-300 airfoil for use on wind turbines (W)


Airfoil ah93w300-il
Details Dat file Parser  
(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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Selig format dat file

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Polars for AH 93-W-300 (ah93w300-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah93w300-il50,00094.2 at α=-2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w300-il50,00055.4 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w300-il100,000917.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w300-il100,000527.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w300-il200,000942.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w300-il200,000541 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w300-il500,000961.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w300-il500,000558.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w300-il1,000,000980.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w300-il1,000,000574.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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