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FX 61-147 AIRFOIL (fx61147-il)

FX 61-147 AIRFOIL - Wortmann FX 61-147 airfoil


Airfoil fx61147-il
Details Dat file Parser  
(fx61147-il) FX 61-147 AIRFOIL
Wortmann FX 61-147 airfoil
Max thickness 14.8% at 33.9% chord.
Max camber 3.2% at 33.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 61-147 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0068800
 0.0042200 0.0132200
 0.0096000 0.0199600
 0.0170200 0.0269800
 0.0265000 0.0344000
 0.0380200 0.0420400
 0.0515800 0.0496500
 0.0669400 0.0572100
 0.0842200 0.0645500
 0.1033000 0.0716500
 0.1240300 0.0783100
 0.1464300 0.0845300
 0.1700000 0.0900600
 0.1955800 0.0948900
 0.2222100 0.0988300
 0.2499800 0.1019400
 0.2789100 0.1041000
 0.3086100 0.1053700
 0.3393300 0.1056700
 0.3705600 0.1051100
 0.4024300 0.1036600
 0.4346900 0.1015100
 0.4673300 0.0987000
 0.4999700 0.0953900
 0.5327400 0.0916400
 0.5652500 0.0875400
 0.5975000 0.0831500
 0.6293800 0.0785500
 0.6607400 0.0737800
 0.6913300 0.0688800
 0.7211500 0.0638800
 0.7499501 0.0588200
 0.7777300 0.0537500
 0.8043500 0.0487100
 0.8297000 0.0437000
 0.8535000 0.0388000
 0.8759000 0.0340500
 0.8964400 0.0295300
 0.9157100 0.0252500
 0.9329900 0.0212100
 0.9484800 0.0174100
 0.9619200 0.0138200
 0.9734400 0.0104700
 0.9829100 0.0074100
 0.9903400 0.0048400
 0.9957100 0.0026600
 0.9989100 0.0009900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0016600
 0.0042200 -.0047500
 0.0096000 -.0078900
 0.0170200 -.0109900
 0.0265000 -.0140900
 0.0380200 -.0170800
 0.0515800 -.0200100
 0.0669400 -.0228800
 0.0842200 -.0257000
 0.1033000 -.0283900
 0.1240300 -.0309300
 0.1464300 -.0332700
 0.1700000 -.0354200
 0.1955800 -.0373000
 0.2222100 -.0389200
 0.2499800 -.0402300
 0.2789100 -.0412000
 0.3086100 -.0418000
 0.3393300 -.0419900
 0.3705600 -.0417400
 0.4024300 -.0410300
 0.4346900 -.0398000
 0.4673300 -.0380500
 0.4999700 -.0357400
 0.5327400 -.0328800
 0.5652500 -.0295000
 0.5975000 -.0255200
 0.6293800 -.0209600
 0.6607400 -.0159200
 0.6913300 -.0107000
 0.7211500 -.0056500
 0.7499501 -.0011500
 0.7777300 0.0026500
 0.8043500 0.0056800
 0.8297000 0.0079300
 0.8535000 0.0093900
 0.8759000 0.0101200
 0.8964400 0.0102500
 0.9157100 0.0099000
 0.9329900 0.0091700
 0.9484800 0.0081900
 0.9619200 0.0069800
 0.9734400 0.0055900
 0.9829100 0.0040900
 0.9903400 0.0027600
 0.9957100 0.0014800
 0.9989100 0.0004000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 61-147 AIRFOIL (fx61147-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx61147-il50,00098.4 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61147-il50,000528.7 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61147-il100,000950 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61147-il100,000552.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61147-il200,000970.8 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61147-il200,000571.9 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61147-il500,000999.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61147-il500,000598.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx61147-il1,000,0009123.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   fx61147-il1,000,0005119.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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