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FX 66-H-60 (fx66h60-il)

FX 66-H-60 - Wortmann FX 66-H-60 airfoil


Airfoil fx66h60-il
Details Dat file Parser  
(fx66h60-il) FX 66-H-60
Wortmann FX 66-H-60 airfoil
Max thickness 6% at 22.2% chord.
Max camber 1.7% at 17% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 66-H-60
1.00000     0.00000
0.99893     0.00012
0.99572     0.00037
0.99039     0.00071
0.98296     0.00112
0.97347     0.00155
0.96194     0.00200
0.94844     0.00241
0.93301     0.00273
0.91573     0.00296
0.89668     0.00319
0.87592     0.00354
0.85355     0.00410
0.82967     0.00489
0.80438     0.00592
0.77779     0.00717
0.75000     0.00862
0.72114     0.01028
0.69134     0.01215
0.66072     0.01421
0.62941     0.01644
0.59755     0.01882
0.56526     0.02132
0.53270     0.02393
0.50000     0.02662
0.46730     0.02934
0.43474     0.03207
0.40245     0.03476
0.37059     0.03733
0.33928     0.03973
0.30866     0.04191
0.27886     0.04377
0.25000     0.04522
0.22221     0.04615
0.19562     0.04647
0.17033     0.04608
0.14645     0.04487
0.12408     0.04278
0.10332     0.03982
0.08427     0.03615
0.06699     0.03198
0.05156     0.02751
0.03806     0.02290
0.02653     0.01829
0.01704     0.01384
0.00961     0.00970
0.00428     0.00597
0.00107     0.00272
0.00000     0.00000
0.00107     -0.00219
0.00428     -0.00393
0.00961     -0.00532
0.01704     -0.00646
0.02653     -0.00740
0.03806     -0.00820
0.05156     -0.00886
0.06699     -0.00945
0.08427     -0.00997
0.10332     -0.01049
0.12408     -0.01105
0.14645     -0.01168
0.17033     -0.01240
0.19562     -0.01319
0.22221     -0.01402
0.25000     -0.01488
0.27886     -0.01576
0.30866     -0.01662
0.33928     -0.01744
0.37059     -0.01821
0.40245     -0.01889
0.43474     -0.01947
0.46730     -0.01994
0.50000     -0.02029
0.53270     -0.02050
0.56526     -0.02056
0.59755     -0.02048
0.62941     -0.02024
0.66072     -0.01984
0.69134     -0.01929
0.72114     -0.01857
0.75000     -0.01768
0.77779     -0.01657
0.80438     -0.01518
0.82967     -0.01350
0.85355     -0.01161
0.87592     -0.00968
0.89668     -0.00785
0.91573     -0.00620
0.93301     -0.00477
0.94844     -0.00357
0.96194     -0.00258
0.97347     -0.00178
0.98296     -0.00115
0.99039     -0.00066
0.99572     -0.00032
0.99893     -0.00011
1.00000     0.00000
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Selig format dat file

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Polars for FX 66-H-60 (fx66h60-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx66h60-il50,000928.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il50,000529.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il100,000937.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il100,000540.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il200,000951.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il200,000551.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il500,000969.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il500,000567.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il1,000,000984.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il1,000,000576.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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