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FX S 02/1-158 AIRFOIL (fxs21158-il)

FX S 02/1-158 AIRFOIL - Wortmann FX S 02/1-158 airfoil


Airfoil fxs21158-il
Details Dat file Parser  
(fxs21158-il) FX S 02/1-158 AIRFOIL
Wortmann FX S 02/1-158 airfoil
Max thickness 15.8% at 30.9% chord.
Max camber 3.5% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX S 02/1-158 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0040000
 0.0042200 0.0105200
 0.0096000 0.0175000
 0.0170200 0.0245400
 0.0265000 0.0315800
 0.0380200 0.0400000
 0.0515800 0.0478900
 0.0669400 0.0565600
 0.0842200 0.0641000
 0.1033000 0.0724300
 0.1240300 0.0795700
 0.1464300 0.0871200
 0.1703700 0.0933800
 0.1955800 0.0996400
 0.2222100 0.1045300
 0.2499800 0.1089800
 0.2789100 0.1117300
 0.3086100 0.1135500
 0.3393300 0.1133900
 0.3705600 0.1120600
 0.4024300 0.1088800
 0.4346900 0.1048300
 0.4673300 0.0997300
 0.4999700 0.0945900
 0.5327400 0.0888000
 0.5652500 0.0830800
 0.5975000 0.0769500
 0.6293800 0.0709900
 0.6607400 0.0648700
 0.6913300 0.0590800
 0.7211500 0.0533200
 0.7499501 0.0478600
 0.7777300 0.0425000
 0.8043500 0.0375300
 0.8297000 0.0327200
 0.8535000 0.0282800
 0.8759000 0.0241000
 0.8964400 0.0203000
 0.9157100 0.0167800
 0.9329900 0.0136500
 0.9484800 0.0108100
 0.9619200 0.0083300
 0.9734400 0.0061800
 0.9829100 0.0043100
 0.9903400 0.0027500
 0.9957100 0.0014800
 0.9989100 0.0006000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0025000
 0.0042200 -.0068000
 0.0096000 -.0109500
 0.0170200 -.0140000
 0.0265000 -.0171400
 0.0380200 -.0200000
 0.0515800 -.0230900
 0.0669400 -.0256000
 0.0842200 -.0289000
 0.1033000 -.0312700
 0.1240300 -.0342600
 0.1464300 -.0363500
 0.1703700 -.0388600
 0.1955800 -.0405800
 0.2222100 -.0424500
 0.2499800 -.0434500
 0.2789100 -.0443100
 0.3086100 -.0442500
 0.3393300 -.0437500
 0.3705600 -.0421500
 0.4024300 -.0395000
 0.4346900 -.0355700
 0.4673300 -.0310000
 0.4999700 -.0260900
 0.5327400 -.0213700
 0.5652500 -.0167900
 0.5975000 -.0126400
 0.6293800 -.0088400
 0.6607400 -.0055600
 0.6913300 -.0027000
 0.7211500 -.0004100
 0.7499501 0.0015200
 0.7777300 0.0029300
 0.8043500 0.0040200
 0.8297000 0.0046900
 0.8535000 0.0051300
 0.8759000 0.0052100
 0.8964400 0.0050800
 0.9157100 0.0047300
 0.9329900 0.0042400
 0.9484800 0.0036300
 0.9619200 0.0029500
 0.9734400 0.0022000
 0.9829100 0.0014500
 0.9903400 0.0007600
 0.9957100 0.0002300
 0.9989100 0.0000500
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for FX S 02/1-158 AIRFOIL (fxs21158-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fxs21158-il50,00095.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs21158-il50,000518.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs21158-il100,000937.4 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs21158-il100,000547.3 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs21158-il200,000976.8 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs21158-il200,000572.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs21158-il500,000996.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs21158-il500,000587.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   fxs21158-il1,000,0009105.1 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fxs21158-il1,000,000576 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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