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FX 63-120 AIRFOIL (fx63120-il)

FX 63-120 AIRFOIL - Wortmann FX 63-120 airfoil


Airfoil fx63120-il
Details Dat file Parser  
(fx63120-il) FX 63-120 AIRFOIL
Wortmann FX 63-120 airfoil
Max thickness 12% at 30.8% chord.
Max camber 5.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 63-120 AIRFOIL
       18.       18.

 0.0000000 0.0000000
 0.0090000 0.0240000
 0.0260000 0.0385000
 0.0380000 0.0460000
 0.0670000 0.0598000
 0.1030000 0.0728000
 0.1460000 0.0843000
 0.1960000 0.0938000
 0.2500000 0.1009000
 0.3080000 0.1053000
 0.4020000 0.1063000
 0.5000000 0.1014000
 0.5970000 0.0905000
 0.6910000 0.0752000
 0.8040000 0.0522000
 0.8960000 0.0311000
 0.9480000 0.0180000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0090000 -.0083000
 0.0260000 -.0130000
 0.0380000 -.0149000
 0.0670000 -.0174000
 0.1030000 -.0191000
 0.1460000 -.0198000
 0.1960000 -.0194000
 0.2500000 -.0178000
 0.3080000 -.0148000
 0.4020000 -.0057000
 0.5000000 0.0033000
 0.5970000 0.0129000
 0.6910000 0.0205000
 0.8040000 0.0242000
 0.8960000 0.0198000
 0.9480000 0.0133000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for FX 63-120 AIRFOIL (fx63120-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63120-il50,000936.7 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63120-il50,000540 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63120-il100,000964.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63120-il100,000567.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63120-il200,000993.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63120-il200,000590 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63120-il500,0009125.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63120-il500,0005114.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63120-il1,000,0009147.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63120-il1,000,0005129.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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