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FX 61-163 AIRFOIL (fx61163-il)

FX 61-163 AIRFOIL - Wortmann FX 61-163 airfoil


Airfoil fx61163-il
Details Dat file Parser  
(fx61163-il) FX 61-163 AIRFOIL
Wortmann FX 61-163 airfoil
Max thickness 16.4% at 37.1% chord.
Max camber 2.6% at 33.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 61-163 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0056600
 0.0042200 0.0123400
 0.0096000 0.0192500
 0.0170200 0.0264100
 0.0265000 0.0340200
 0.0380200 0.0417500
 0.0515800 0.0492900
 0.0669400 0.0568700
 0.0842200 0.0641200
 0.1033000 0.0710900
 0.1240300 0.0776000
 0.1464300 0.0837100
 0.1703700 0.0892400
 0.1955800 0.0942200
 0.2222100 0.0984400
 0.2499800 0.1019400
 0.2789100 0.1045500
 0.3086100 0.1063500
 0.3393300 0.1072300
 0.3705600 0.1072800
 0.4024300 0.1063900
 0.4346900 0.1045700
 0.4673300 0.1016800
 0.4999700 0.0978000
 0.5327400 0.0930300
 0.5652500 0.0877200
 0.5975000 0.0820800
 0.6293800 0.0763700
 0.6607400 0.0706400
 0.6913300 0.0649700
 0.7211500 0.0593500
 0.7499501 0.0538800
 0.7777300 0.0485600
 0.8043500 0.0434700
 0.8297000 0.0386100
 0.8535000 0.0340300
 0.8759000 0.0296800
 0.8964400 0.0256000
 0.9157100 0.0217600
 0.9329900 0.0181700
 0.9484800 0.0148100
 0.9619200 0.0116700
 0.9734400 0.0087500
 0.9829100 0.0061000
 0.9903400 0.0039000
 0.9957100 0.0020600
 0.9989100 0.0006900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0024800
 0.0042200 -.0056000
 0.0096000 -.0090700
 0.0170200 -.0127200
 0.0265000 -.0165600
 0.0380200 -.0202700
 0.0515800 -.0241200
 0.0669400 -.0278600
 0.0842200 -.0316000
 0.1033000 -.0351800
 0.1240300 -.0387000
 0.1464300 -.0419900
 0.1703700 -.0451100
 0.1955800 -.0479200
 0.2222100 -.0504400
 0.2499800 -.0525200
 0.2789100 -.0542100
 0.3086100 -.0553700
 0.3393300 -.0560900
 0.3705600 -.0562500
 0.4024300 -.0558500
 0.4346900 -.0547400
 0.4673300 -.0529300
 0.4999700 -.0503900
 0.5327400 -.0471900
 0.5652500 -.0432400
 0.5975000 -.0384500
 0.6293800 -.0328800
 0.6607400 -.0268500
 0.6913300 -.0207900
 0.7211500 -.0151700
 0.7499501 -.0101400
 0.7777300 -.0057600
 0.8043500 -.0020100
 0.8297000 0.0011000
 0.8535000 0.0035800
 0.8759000 0.0054200
 0.8964400 0.0066700
 0.9157100 0.0073400
 0.9329900 0.0074900
 0.9484800 0.0071500
 0.9619200 0.0063700
 0.9734400 0.0052600
 0.9829100 0.0039200
 0.9903400 0.0027300
 0.9957100 0.0015000
 0.9989100 0.0004400
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 61-163 AIRFOIL (fx61163-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx61163-il50,00096.1 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61163-il50,000519.4 at α=11.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61163-il100,000947.7 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61163-il100,000550 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61163-il200,000970.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61163-il200,000572.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61163-il500,0009103.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61163-il500,000598.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61163-il1,000,0005115.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61163-il1,000,0000127.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
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