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FX 60-157 AIRFOIL (fx60157-il)

FX 60-157 AIRFOIL - Wortmann FX 60-157 airfoil


Airfoil fx60157-il
Details Dat file Parser  
(fx60157-il) FX 60-157 AIRFOIL
Wortmann FX 60-157 airfoil
Max thickness 15.7% at 40.2% chord.
Max camber 2.7% at 75% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 60-157 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0084700
 0.0042200 0.0158200
 0.0096000 0.0218300
 0.0170200 0.0293000
 0.0265000 0.0361800
 0.0380200 0.0438000
 0.0515800 0.0506800
 0.0669400 0.0577500
 0.0842200 0.0639700
 0.1033000 0.0701900
 0.1240300 0.0755600
 0.1464300 0.0807500
 0.1703700 0.0850900
 0.1955800 0.0891700
 0.2222100 0.0924700
 0.2499800 0.0954500
 0.2789100 0.0976900
 0.3086100 0.0995500
 0.3393300 0.1007100
 0.3705600 0.1014800
 0.4024300 0.1015100
 0.4346900 0.1011600
 0.4673300 0.1001300
 0.4999700 0.0987500
 0.5327400 0.0967600
 0.5652500 0.0943800
 0.5975000 0.0913900
 0.6293800 0.0880100
 0.6607400 0.0840000
 0.6913300 0.0796100
 0.7211500 0.0747100
 0.7499501 0.0694700
 0.7777300 0.0638400
 0.8043500 0.0580300
 0.8297000 0.0520000
 0.8535000 0.0459300
 0.8759000 0.0398800
 0.8964400 0.0340400
 0.9157100 0.0284200
 0.9329900 0.0231600
 0.9484800 0.0182900
 0.9619200 0.0138900
 0.9734400 0.0099700
 0.9829100 0.0065800
 0.9903400 0.0038600
 0.9957100 0.0018400
 0.9989100 0.0005600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0022200
 0.0042200 -.0058500
 0.0096000 -.0103200
 0.0170200 -.0140300
 0.0265000 -.0182500
 0.0380200 -.0218300
 0.0515800 -.0257500
 0.0669400 -.0291800
 0.0842200 -.0329600
 0.1033000 -.0362100
 0.1240300 -.0396600
 0.1464300 -.0425700
 0.1703700 -.0455700
 0.1955800 -.0479700
 0.2222100 -.0503600
 0.2499800 -.0520600
 0.2789100 -.0536800
 0.3086100 -.0546200
 0.3393300 -.0553700
 0.3705600 -.0551400
 0.4024300 -.0552200
 0.4346900 -.0543800
 0.4673300 -.0532300
 0.4999700 -.0513900
 0.5327400 -.0491400
 0.5652500 -.0460100
 0.5975000 -.0422900
 0.6293800 -.0376900
 0.6607400 -.0324800
 0.6913300 -.0267200
 0.7211500 -.0209000
 0.7499501 -.0151400
 0.7777300 -.0099200
 0.8043500 -.0052700
 0.8297000 -.0013900
 0.8535000 0.0017700
 0.8759000 0.0041700
 0.8964400 0.0058800
 0.9157100 0.0069100
 0.9329900 0.0073300
 0.9484800 0.0071700
 0.9619200 0.0065200
 0.9734400 0.0054300
 0.9829100 0.0040700
 0.9903400 0.0026700
 0.9957100 0.0013700
 0.9989100 0.0004400
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX 60-157 AIRFOIL (fx60157-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx60157-il50,000928.8 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60157-il50,000528.6 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60157-il100,000946.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60157-il100,000541.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60157-il200,000956.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60157-il200,000557.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60157-il500,000981.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60157-il500,000570 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60157-il1,000,000995.8 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60157-il1,000,000572.8 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
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