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FX 68-H-120 (fx68h120-il)

FX 68-H-120 - Wortmann FX 68-H-120 airfoil


Airfoil fx68h120-il
Details Dat file Parser  
(fx68h120-il) FX 68-H-120
Wortmann FX 68-H-120 airfoil
Max thickness 11.8% at 25% chord.
Max camber 2.3% at 33.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 68-H-120
1.00000     0.00000
0.99893     0.00006
0.99572     0.00003
0.99039     0.00020
0.98296     0.00057
0.97347     0.00127
0.96194     0.00240
0.94844     0.00405
0.93301     0.00628
0.91573     0.00912
0.89668     0.01253
0.87592     0.01646
0.85355     0.02088
0.82967     0.02576
0.80438     0.03098
0.77779     0.03637
0.75000     0.04176
0.72114     0.04703
0.69134     0.05208
0.66072     0.05678
0.62941     0.06102
0.59755     0.06475
0.56526     0.06797
0.53270     0.07075
0.50000     0.07319
0.46730     0.07536
0.43474     0.07726
0.40245     0.07887
0.37059     0.08017
0.33928     0.08112
0.30866     0.08170
0.27886     0.08187
0.25000     0.08157
0.22221     0.08074
0.19562     0.07935
0.17033     0.07734
0.14645     0.07471
0.12408     0.07138
0.10332     0.06717
0.08427     0.06183
0.06699     0.05520
0.05156     0.04742
0.03806     0.03890
0.02653     0.03013
0.01704     0.02171
0.00961     0.01423
0.00428     0.00819
0.00107     0.00362
0.00000     0.00000
0.00107     -0.00338
0.00428     -0.00700
0.00961     -0.01096
0.01704     -0.01511
0.02653     -0.01927
0.03806     -0.02327
0.05156     -0.02698
0.06699     -0.03023
0.08427     -0.03283
0.10332     -0.03466
0.12408     -0.03578
0.14645     -0.03640
0.17033     -0.03672
0.19562     -0.03684
0.22221     -0.03676
0.25000     -0.03650
0.27886     -0.03609
0.30866     -0.03554
0.33928     -0.03486
0.37059     -0.03407
0.40245     -0.03317
0.43474     -0.03217
0.46730     -0.03110
0.50000     -0.02996
0.53270     -0.02877
0.56526     -0.02753
0.59755     -0.02625
0.62941     -0.02495
0.66072     -0.02361
0.69134     -0.02225
0.72114     -0.02086
0.75000     -0.01945
0.77779     -0.01802
0.80438     -0.01656
0.82967     -0.01509
0.85355     -0.01359
0.87592     -0.01207
0.89668     -0.01054
0.91573     -0.00900
0.93301     -0.00747
0.94844     -0.00598
0.96194     -0.00459
0.97347     -0.00335
0.98296     -0.00230
0.99039     -0.00144
0.99572     -0.00077
0.99893     -0.00030
1.00000     0.00000
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Lednicer format dat file
Selig format dat file

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Polars for FX 68-H-120 (fx68h120-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx68h120-il50,000928.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx68h120-il50,000529.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx68h120-il100,000940.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx68h120-il100,000541 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx68h120-il200,000954.5 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx68h120-il200,000554.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx68h120-il500,000974.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx68h120-il500,000573.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx68h120-il1,000,000991.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx68h120-il1,000,000588.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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