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FX 63-110 AIRFOIL (fx63110-il)

FX 63-110 AIRFOIL - Wortmann FX 63-110 airfoil


Airfoil fx63110-il
Details Dat file Parser  
(fx63110-il) FX 63-110 AIRFOIL
Wortmann FX 63-110 airfoil
Max thickness 11% at 30.8% chord.
Max camber 4.3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 63-110 AIRFOIL
       18.       16.

 0.0000000 0.0000000
 0.0090000 0.0214700
 0.0260000 0.0343700
 0.0380000 0.0410400
 0.0670000 0.0532500
 0.1030000 0.0648400
 0.1460000 0.0748700
 0.1960000 0.0831800
 0.2500000 0.0894300
 0.3080000 0.0931500
 0.4020000 0.0936300
 0.5000000 0.0889300
 0.5970000 0.0788800
 0.6910000 0.0651600
 0.8040000 0.0447600
 0.8960000 0.0264100
 0.9480000 0.0151100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0090000 -.0087700
 0.0260000 -.0143700
 0.1030000 -.0202400
 0.1460000 -.0211700
 0.1960000 -.0212800
 0.2500000 -.0201300
 0.3080000 -.0168500
 0.4020000 -.0097300
 0.5000000 -.0020800
 0.5970000 0.0073200
 0.6910000 0.0146400
 0.8040000 0.0189400
 0.8960000 0.0159900
 0.9480000 0.0107900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for FX 63-110 AIRFOIL (fx63110-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63110-il50,000940 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63110-il50,000542.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63110-il100,000964.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63110-il100,000566.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63110-il200,000990.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63110-il200,000587.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63110-il500,0009118.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63110-il500,0005105.8 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63110-il1,000,0009136.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63110-il1,000,0005117.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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