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WORTMANN FX 73-170 A (fx73170a-il)

WORTMANN FX 73-170 A - Wortmann FX 73-170 A airfoil


Airfoil fx73170a-il
Details Dat file Parser  
(fx73170a-il) WORTMANN FX 73-170 A
Wortmann FX 73-170 A airfoil
Max thickness 17.1% at 43.5% chord.
Max camber 5.6% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
WORTMANN FX 73-170 A
1.00000     0.00000
0.99893     0.00129
0.99572     0.00223
0.99039     0.00378
0.98296     0.00578
0.97347     0.00836
0.96194     0.01147
0.94844     0.01514
0.93301     0.01946
0.91573     0.02450
0.89668     0.03028
0.87592     0.03681
0.85355     0.04403
0.82967     0.05191
0.80438     0.06037
0.77779     0.06935
0.75000     0.07880
0.72114     0.08847
0.69134     0.09808
0.66072     0.10726
0.62941     0.11577
0.59755     0.12345
0.56526     0.13002
0.53270     0.13527
0.50000     0.13903
0.46730     0.14124
0.43474     0.14195
0.40245     0.14130
0.37059     0.13949
0.33928     0.13666
0.30866     0.13292
0.27886     0.12834
0.25000     0.12299
0.22221     0.11695
0.19562     0.11030
0.17033     0.10310
0.14645     0.09542
0.12408     0.08736
0.10332     0.07898
0.08427     0.07038
0.06699     0.06164
0.05156     0.05285
0.03806     0.04411
0.02653     0.03557
0.01704     0.02738
0.00961     0.01965
0.00428     0.01222
0.00107     0.00547
0.00000     0.00000
0.00107     -0.00415
0.00428     -0.00722
0.00961     -0.00990
0.01704     -0.01239
0.02653     -0.01462
0.03806     -0.01670
0.05156     -0.01860
0.06699     -0.02035
0.08427     -0.02196
0.10332     -0.02342
0.12408     -0.02473
0.14645     -0.02588
0.17033     -0.02689
0.19562     -0.02775
0.22221     -0.02846
0.25000     -0.02902
0.27886     -0.02943
0.30866     -0.02970
0.33928     -0.02981
0.37059     -0.02976
0.40245     -0.02955
0.43474     -0.02917
0.46730     -0.02860
0.50000     -0.02781
0.53270     -0.02677
0.56526     -0.02550
0.59755     -0.02403
0.62941     -0.02234
0.66072     -0.02040
0.69134     -0.01813
0.72114     -0.01546
0.75000     -0.01248
0.77779     -0.00938
0.80438     -0.00643
0.82967     -0.00385
0.85355     -0.00175
0.87592     -0.00018
0.89668     0.00089
0.91573     0.00154
0.93301     0.00181
0.94844     0.00177
0.96194     0.00147
0.97347     0.00098
0.98296     0.00040
0.99039     -0.00022
0.99572     -0.00060
0.99893     -0.00091
1.00000     0.00000
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Polars for WORTMANN FX 73-170 A (fx73170a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx73170a-il50,00094.8 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73170a-il50,000511.1 at α=16°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73170a-il100,000918.1 at α=14.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73170a-il100,000517.4 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73170a-il200,000931.2 at α=13°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73170a-il200,000551.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73170a-il500,0009117.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73170a-il500,0005110.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73170a-il1,000,0009151.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73170a-il1,000,0005144 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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