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FX 63-143 AIRFOIL (fx63143-il)

FX 63-143 AIRFOIL - Wortmann FX 63-143 airfoil


Airfoil fx63143-il
Details Dat file Parser  
(fx63143-il) FX 63-143 AIRFOIL
Wortmann FX 63-143 airfoil
Max thickness 14.3% at 33.9% chord.
Max camber 3.1% at 30.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 63-143 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0055000
 0.0042200 0.0118900
 0.0096000 0.0180000
 0.0170200 0.0250300
 0.0265000 0.0322000
 0.0380200 0.0396300
 0.0515800 0.0459900
 0.0669400 0.0543900
 0.0842200 0.0607200
 0.1033000 0.0684900
 0.1240300 0.0743700
 0.1464300 0.0811100
 0.1703700 0.0860700
 0.1955800 0.0914100
 0.2222100 0.0950100
 0.2499800 0.0985800
 0.2789100 0.1005200
 0.3086100 0.1021200
 0.3393300 0.1021700
 0.3705600 0.1016600
 0.4024300 0.0997100
 0.4346900 0.0971600
 0.4673300 0.0934700
 0.4999700 0.0893000
 0.5327400 0.0844200
 0.5662500 0.0794300
 0.5975000 0.0740600
 0.6293800 0.0686600
 0.6607400 0.0631100
 0.6913300 0.0577300
 0.7211500 0.0523100
 0.7499501 0.0472000
 0.7777300 0.0421700
 0.8043500 0.0374700
 0.8297000 0.0329800
 0.8535000 0.0288100
 0.8759000 0.0249100
 0.8964400 0.0213200
 0.9157100 0.0180100
 0.9329900 0.0149700
 0.9484800 0.0121700
 0.9619200 0.0095500
 0.9734400 0.0070800
 0.9829100 0.0048200
 0.9903400 0.0028800
 0.9957100 0.0013600
 0.9989100 0.0003900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0030000
 0.0042200 -.0051500
 0.0096000 -.0098100
 0.0170200 -.0115900
 0.0265000 -.0157600
 0.0380200 -.0176200
 0.0515800 -.0212300
 0.0669400 -.0229500
 0.0842200 -.0261400
 0.1033000 -.0278500
 0.1240300 -.0307100
 0.1464300 -.0322900
 0.1703700 -.0347500
 0.1955800 -.0368000
 0.2222100 -.0379200
 0.2499800 -.0387600
 0.2789100 -.0400500
 0.3086100 -.0403800
 0.3393300 -.0410200
 0.3705600 -.0408100
 0.4024300 -.0408300
 0.4346900 -.0401300
 0.4673300 -.0396200
 0.4999700 -.0385000
 0.5327400 -.0375100
 0.5662500 -.0360100
 0.5975000 -.0346100
 0.6293800 -.0327900
 0.6607400 -.0310200
 0.6913300 -.0288700
 0.7211500 -.0267300
 0.7499501 -.0241800
 0.7777300 -.0215800
 0.8043500 -.0186800
 0.8297000 -.0156800
 0.8535000 -.0124200
 0.8759000 -.0090800
 0.8964400 -.0056700
 0.9157100 -.0026400
 0.9329900 -.0001800
 0.9484800 0.0015000
 0.9619200 0.0024400
 0.9734400 0.0026700
 0.9829100 0.0023500
 0.9903400 0.0017000
 0.9957100 0.0008900
 0.9989100 0.0003000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 63-143 AIRFOIL (fx63143-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63143-il50,000910.7 at α=-1°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63143-il50,000524 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63143-il100,000946.5 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63143-il100,000549.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63143-il200,000972.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63143-il200,000565.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63143-il500,000971 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63143-il500,000564.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63143-il1,000,000979.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63143-il1,000,000578.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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