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FX 62-K-153/20 AIRFOIL (fx62k153-il)

FX 62-K-153/20 AIRFOIL - Wortmann FX 62-K-153/20 airfoil


Airfoil fx62k153-il
Details Dat file Parser  
(fx62k153-il) FX 62-K-153/20 AIRFOIL
Wortmann FX 62-K-153/20 airfoil
Max thickness 15.3% at 40.2% chord.
Max camber 4.1% at 62.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 62-K-153/20 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0071100
 0.0042200 0.0132500
 0.0096000 0.0197400
 0.0170200 0.0264300
 0.0265000 0.0334400
 0.0380200 0.0404900
 0.0515800 0.0475500
 0.0669400 0.0545300
 0.0842200 0.0614200
 0.1033000 0.0681500
 0.1240300 0.0746700
 0.1464300 0.0809000
 0.1703700 0.0868800
 0.1955800 0.0922000
 0.2222100 0.0971200
 0.2499800 0.1015600
 0.2789100 0.1054600
 0.3086100 0.1087900
 0.3393300 0.1115100
 0.3705600 0.1133100
 0.4024300 0.1144800
 0.4346900 0.1149400
 0.4673300 0.1146300
 0.4999700 0.1135600
 0.5327400 0.1116700
 0.5652500 0.1089900
 0.5975000 0.1054800
 0.6293800 0.1011100
 0.6607400 0.0958400
 0.6913300 0.0896800
 0.7211500 0.0827800
 0.7499501 0.0754100
 0.7777300 0.0679000
 0.8043500 0.0605300
 0.8297000 0.0534300
 0.8535000 0.0466900
 0.8759000 0.0403400
 0.8964400 0.0344200
 0.9157100 0.0289000
 0.9329900 0.0238200
 0.9484800 0.0191500
 0.9619200 0.0148800
 0.9734400 0.0110000
 0.9829100 0.0075500
 0.9903400 0.0047100
 0.9957100 0.0024000
 0.9989100 0.0007300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0016600
 0.0042200 -.0047800
 0.0096000 -.0078500
 0.0170200 -.0108200
 0.0265000 -.0137100
 0.0380200 -.0164500
 0.0515800 -.0190300
 0.0669400 -.0214900
 0.0842200 -.0238500
 0.1033000 -.0261100
 0.1240300 -.0282600
 0.1464300 -.0302600
 0.1703700 -.0321200
 0.1955800 -.0338200
 0.2222100 -.0353300
 0.2499800 -.0366000
 0.2789100 -.0376300
 0.3086100 -.0383300
 0.3393300 -.0387000
 0.3705600 -.0386800
 0.4024300 -.0382500
 0.4346900 -.0373400
 0.4673300 -.0359200
 0.4999700 -.0339000
 0.5327400 -.0312600
 0.5652500 -.0279700
 0.5975000 -.0240400
 0.6293800 -.0194700
 0.6607400 -.0144300
 0.6913300 -.0091400
 0.7211500 -.0039900
 0.7499501 0.0006800
 0.7777300 0.0046000
 0.8043500 0.0077200
 0.8297000 0.0100400
 0.8535000 0.0116400
 0.8759000 0.0125500
 0.8964400 0.0128400
 0.9157100 0.0125700
 0.9329900 0.0118100
 0.9484800 0.0106000
 0.9619200 0.0090300
 0.9734400 0.0071900
 0.9829100 0.0052200
 0.9903400 0.0035000
 0.9957100 0.0018600
 0.9989100 0.0005100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for FX 62-K-153/20 AIRFOIL (fx62k153-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx62k153-il50,000926.9 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k153-il50,000523 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k153-il100,000945.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k153-il100,000544.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k153-il200,000977.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k153-il200,000579.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k153-il500,0009124.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k153-il500,0005122.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fx62k153-il1,000,0009161.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx62k153-il1,000,0005151.3 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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