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AH 93-W-145 (ah93w145-il)

AH 93-W-145 - Althaus AH 93-W-145 airfoil for use on wind turbines (W)


Airfoil ah93w145-il
Details Dat file Parser  
(ah93w145-il) AH 93-W-145
Althaus AH 93-W-145 airfoil for use on wind turbines (W)
Max thickness 14.5% at 33.9% chord.
Max camber 3.9% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
AH 93-W-145
1.00000     0.00033
0.99893     0.00067
0.99572     0.00172
0.99039     0.00330
0.98296     0.00533
0.97347     0.00775
0.96194     0.01054
0.94844     0.01364
0.93301     0.01699
0.91573     0.02056
0.89668     0.02435
0.87592     0.02838
0.85355     0.03269
0.82967     0.03730
0.80438     0.04225
0.77779     0.04751
0.75000     0.05305
0.72114     0.05880
0.69134     0.06472
0.66072     0.07075
0.62941     0.07682
0.59755     0.08286
0.56526     0.08882
0.53270     0.09454
0.50000     0.09979
0.46730     0.10427
0.43474     0.10771
0.40245     0.10996
0.37059     0.11094
0.33928     0.11066
0.30866     0.10919
0.27886     0.10668
0.25000     0.10325
0.22221     0.09904
0.19562     0.09414
0.17033     0.08864
0.14645     0.08263
0.12408     0.07617
0.10332     0.06933
0.08427     0.06218
0.06699     0.05480
0.05156     0.04727
0.03806     0.03970
0.02653     0.03216
0.01704     0.02478
0.00961     0.01774
0.00428     0.01121
0.00107     0.00533
0.00000     0.00000
0.00107     -0.00496
0.00428     -0.00964
0.00961     -0.01394
0.01704     -0.01787
0.02653     -0.02138
0.03806     -0.02442
0.05156     -0.02702
0.06699     -0.02921
0.08427     -0.03101
0.10332     -0.03246
0.12408     -0.03356
0.14645     -0.03436
0.17033     -0.03489
0.19562     -0.03521
0.22221     -0.03535
0.25000     -0.03531
0.27886     -0.03510
0.30866     -0.03473
0.33928     -0.03417
0.37059     -0.03342
0.40245     -0.03249
0.43474     -0.03137
0.46730     -0.03007
0.50000     -0.02860
0.53270     -0.02698
0.56526     -0.02523
0.59755     -0.02336
0.62941     -0.02140
0.66072     -0.01937
0.69134     -0.01728
0.72114     -0.01516
0.75000     -0.01303
0.77779     -0.01090
0.80438     -0.00882
0.82967     -0.00685
0.85355     -0.00506
0.87592     -0.00348
0.89668     -0.00215
0.91573     -0.00114
0.93301     -0.00048
0.94844     -0.00016
0.96194     -0.00012
0.97347     -0.00030
0.98296     -0.00064
0.99039     -0.00102
0.99572     -0.00135
0.99893     -0.00157
1.00000     -0.00162
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Selig format dat file

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Polars for AH 93-W-145 (ah93w145-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah93w145-il50,00096.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w145-il50,000518.7 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w145-il100,000941.9 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w145-il100,000549.3 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w145-il200,000979.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w145-il200,000580.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w145-il500,0009120.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w145-il500,0005116.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93w145-il1,000,0009151.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93w145-il1,000,0005139.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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