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WORTMANN FX 2 AIRFOIL (fx2-il)

WORTMANN FX 2 AIRFOIL - Wortmann FX 2 airfoil


Airfoil fx2-il
Details Dat file Parser  
(fx2-il) WORTMANN FX 2 AIRFOIL
Wortmann FX 2 airfoil
Max thickness 20.4% at 43.5% chord.
Max camber 3.8% at 69.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 2 AIRFOIL
      24.0      24.0
 
 0.0000000 0.0000000
 0.0170400 0.0255600
 0.0380600 0.0404600
 0.0669900 0.0548100
 0.1033300 0.0698000
 0.1464400 0.0836600
 0.1956200 0.0965700
 0.2500000 0.1079700
 0.3086600 0.1173000
 0.3705900 0.1242400
 0.4347400 0.1286100
 0.5000000 0.1301500
 0.5652600 0.1284200
 0.6294100 0.1232500
 0.6913400 0.1140100
 0.7500000 0.0982500
 0.8043800 0.0767100
 0.8535600 0.0564400
 0.8966700 0.0386100
 0.9330100 0.0246500
 0.9616400 0.0143900
 0.9829600 0.0067800
 0.9957200 0.0021400
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0170400 -.0186900
 0.0380600 -.0287600
 0.0669900 -.0375200
 0.1033300 -.0467500
 0.1464400 -.0549200
 0.1956200 -.0622200
 0.2500000 -.0684000
 0.3086600 -.0729700
 0.3705900 -.0755300
 0.4347400 -.0758500
 0.5000000 -.0729900
 0.5652600 -.0653800
 0.6294100 -.0547000
 0.6913400 -.0385600
 0.7500000 -.0241600
 0.8043800 -.0133100
 0.8535600 -.0045900
 0.8966700 0.0000700
 0.9330100 0.0026500
 0.9616400 0.0027800
 0.9829600 0.0020400
 0.9957200 0.0005700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for WORTMANN FX 2 AIRFOIL (fx2-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx2-il50,000918 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx2-il50,000514.9 at α=12.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx2-il100,000923.7 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   fx2-il100,000522.7 at α=11°Mach=0 Ncrit=5Xfoil predictionDetails
   fx2-il200,000934.2 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx2-il200,000534.1 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   fx2-il500,000951.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx2-il500,000550.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx2-il1,000,0009107.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx2-il1,000,0005111 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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