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FX 63-145 AIRFOIL (fx63145-il)

FX 63-145 AIRFOIL - Wortmann FX 63-145 airfoil


Airfoil fx63145-il
Details Dat file Parser  
(fx63145-il) FX 63-145 AIRFOIL
Wortmann FX 63-145 airfoil
Max thickness 14.5% at 30.9% chord.
Max camber 4% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 63-145 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0065000
 0.0042200 0.0160000
 0.0096000 0.0240000
 0.0170200 0.0320000
 0.0265000 0.0405000
 0.0380200 0.0490000
 0.0515800 0.0569900
 0.0669400 0.0669800
 0.0842200 0.0729200
 0.1033000 0.0813100
 0.1240300 0.0864700
 0.1464300 0.0934200
 0.1703700 0.0975800
 0.1955800 0.1029100
 0.2222100 0.1057500
 0.2499800 0.1092600
 0.2789100 0.1105000
 0.3085100 0.1120700
 0.3393300 0.1115400
 0.3705600 0.1110300
 0.4024300 0.1086000
 0.4346900 0.1059900
 0.4673300 0.1017500
 0.4999700 0.0975200
 0.5327400 0.0923600
 0.5652500 0.0874100
 0.5975000 0.0819100
 0.6293800 0.0765200
 0.6607400 0.0709500
 0.6913300 0.0656500
 0.7211500 0.0601400
 0.7499501 0.0549800
 0.7777300 0.0497700
 0.8043500 0.0448800
 0.8297000 0.0400700
 0.8535000 0.0355300
 0.8759000 0.0310400
 0.8964400 0.0268600
 0.9157100 0.0228500
 0.9329900 0.0191400
 0.9484800 0.0156400
 0.9619200 0.0123700
 0.9734400 0.0093100
 0.9829100 0.0065000
 0.9903400 0.0041100
 0.9957100 0.0021900
 0.9989100 0.0009000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0020000
 0.0042200 -.0040000
 0.0096000 -.0070000
 0.0170200 -.0097000
 0.0265000 -.0131100
 0.0380200 -.0150000
 0.0515800 -.0184700
 0.0669400 -.0206000
 0.0842200 -.0239000
 0.1033000 -.0252300
 0.1240300 -.0284100
 0.1464300 -.0293200
 0.1703700 -.0316700
 0.1955800 -.0320700
 0.2222100 -.0335400
 0.2499800 -.0332400
 0.2789100 -.0337100
 0.3085100 -.0326400
 0.3393300 -.0321100
 0.3705600 -.0302400
 0.4024300 -.0287600
 0.4346900 -.0261300
 0.4673300 -.0237500
 0.4999700 -.0203500
 0.5327400 -.0171000
 0.5652500 -.0129500
 0.5975000 -.0090600
 0.6293800 -.0048400
 0.6607400 -.0012600
 0.6913300 0.0022400
 0.7211500 0.0050100
 0.7499501 0.0076000
 0.7777300 0.0094600
 0.8043500 0.0110700
 0.8297000 0.0120200
 0.8535000 0.0126500
 0.8759000 0.0126700
 0.8964400 0.0124300
 0.9157100 0.0117000
 0.9329900 0.0107200
 0.9484800 0.0094100
 0.9619200 0.0078500
 0.9734400 0.0060400
 0.9829100 0.0041200
 0.9903400 0.0023800
 0.9957100 0.0009700
 0.9989100 0.0001100
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 63-145 AIRFOIL (fx63145-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx63145-il50,000913.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63145-il50,000533.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63145-il100,000956.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63145-il100,000556.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63145-il200,000975.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63145-il200,000559.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63145-il500,000975.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63145-il500,000572.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx63145-il1,000,000986.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx63145-il1,000,000581.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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