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AH 82-150 F (ah82150f-il)

AH 82-150 F - Althaus AH 82-150 F airfoil


Airfoil ah82150f-il
Details Dat file Parser  
(ah82150f-il) AH 82-150 F
Althaus AH 82-150 F airfoil
Max thickness 15% at 43.5% chord.
Max camber 3.6% at 46.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
AH 82-150 F
1.00000     0.00000
0.99893     0.00042
0.99572     0.00133
0.99039     0.00262
0.98296     0.00438
0.97347     0.00666
0.96194     0.00952
0.94844     0.01301
0.93301     0.01716
0.91573     0.02201
0.89668     0.02754
0.87592     0.03374
0.85355     0.04057
0.82967     0.04796
0.80438     0.05588
0.77779     0.06429
0.75000     0.07299
0.72114     0.08150
0.69134     0.08914
0.66072     0.09545
0.62941     0.10036
0.59755     0.10413
0.56526     0.10703
0.53270     0.10917
0.50000     0.11058
0.46730     0.11128
0.43474     0.11128
0.40245     0.11062
0.37059     0.10929
0.33928     0.10731
0.30866     0.10466
0.27886     0.10134
0.25000     0.09734
0.22221     0.09268
0.19562     0.08740
0.17033     0.08156
0.14645     0.07523
0.12408     0.06853
0.10332     0.06156
0.08427     0.05443
0.06699     0.04721
0.05156     0.03997
0.03806     0.03276
0.02653     0.02570
0.01704     0.01901
0.00961     0.01300
0.00428     0.00789
0.00107     0.00366
0.00000     0.00000
0.00107     -0.00348
0.00428     -0.00700
0.00961     -0.01045
0.01704     -0.01363
0.02653     -0.01642
0.03806     -0.01891
0.05156     -0.02121
0.06699     -0.02342
0.08427     -0.02552
0.10332     -0.02752
0.12408     -0.02939
0.14645     -0.03112
0.17033     -0.03269
0.19562     -0.03409
0.22221     -0.03528
0.25000     -0.03628
0.27886     -0.03708
0.30866     -0.03770
0.33928     -0.03818
0.37059     -0.03850
0.40245     -0.03867
0.43474     -0.03869
0.46730     -0.03856
0.50000     -0.03827
0.53270     -0.03782
0.56526     -0.03719
0.59755     -0.03639
0.62941     -0.03541
0.66072     -0.03422
0.69134     -0.03279
0.72114     -0.03096
0.75000     -0.02854
0.77779     -0.02533
0.80438     -0.02138
0.82967     -0.01702
0.85355     -0.01273
0.87592     -0.00892
0.89668     -0.00577
0.91573     -0.00332
0.93301     -0.00151
0.94844     -0.00028
0.96194     0.00044
0.97347     0.00077
0.98296     0.00080
0.99039     0.00066
0.99572     0.00043
0.99893     0.00019
1.00000     0.00000
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Lednicer format dat file
Selig format dat file

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Polars for AH 82-150 F (ah82150f-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah82150f-il50,000917.6 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah82150f-il50,000519.4 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah82150f-il100,000934.6 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah82150f-il100,000533.5 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   ah82150f-il200,000958.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah82150f-il200,000553.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah82150f-il500,000995.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah82150f-il500,000599.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah82150f-il1,000,0009135.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah82150f-il1,000,0005133.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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