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FX 38-153 AIRFOIL (fx38153-il)

FX 38-153 AIRFOIL - Wortmann FX 38-153 airfoil


Airfoil fx38153-il
Details Dat file Parser  
(fx38153-il) FX 38-153 AIRFOIL
Wortmann FX 38-153 airfoil
Max thickness 15.5% at 43.5% chord.
Max camber 2.1% at 80.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 38-153 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010200 0.0064500
 0.0042200 0.0134900
 0.0096000 0.0191400
 0.0170200 0.0263000
 0.0265000 0.0327000
 0.0380200 0.0397500
 0.0515800 0.0461100
 0.0669400 0.0526600
 0.0842200 0.0584600
 0.1033000 0.0642400
 0.1240300 0.0692900
 0.1464300 0.0742600
 0.1703400 0.0785300
 0.1955800 0.0826600
 0.2222100 0.0861100
 0.2499800 0.0893200
 0.2789100 0.0918200
 0.3086100 0.0940200
 0.3393300 0.0955100
 0.3705600 0.0967000
 0.4024300 0.0971800
 0.4346900 0.0973900
 0.4673300 0.0969500
 0.4999700 0.0961800
 0.5327400 0.0948200
 0.5652500 0.0931100
 0.5975000 0.0908300
 0.6293800 0.0882100
 0.6607400 0.0850300
 0.6913300 0.0814800
 0.7211500 0.0773200
 0.7499501 0.0727200
 0.7777300 0.0675900
 0.8043500 0.0620300
 0.8297000 0.0559600
 0.8535000 0.0495800
 0.8759000 0.0429100
 0.8964400 0.0362800
 0.9157100 0.0298800
 0.9329900 0.0239500
 0.9484800 0.0185600
 0.9619200 0.0138300
 0.9734400 0.0097000
 0.9829100 0.0062400
 0.9903400 0.0035400
 0.9957100 0.0015900
 0.9989100 0.0004200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010200 -.0024500
 0.0042200 -.0051900
 0.0096000 -.0091000
 0.0170200 -.0122800
 0.0265000 -.0162900
 0.0380200 -.0196200
 0.0515800 -.0234800
 0.0669400 -.0268700
 0.0842200 -.0306300
 0.1033000 -.0338600
 0.1240300 -.0373500
 0.1464300 -.0403400
 0.1703400 -.0434500
 0.1955800 -.0461000
 0.2222100 -.0487100
 0.2499800 -.0508800
 0.2789100 -.0530300
 0.3086100 -.0546600
 0.3393300 -.0561800
 0.3705600 -.0571200
 0.4024300 -.0578500
 0.4346900 -.0580300
 0.4673300 -.0579600
 0.4999700 -.0572700
 0.5327400 -.0562200
 0.5652500 -.0545800
 0.5975000 -.0525400
 0.6293800 -.0497900
 0.6607400 -.0464000
 0.6913300 -.0421400
 0.7211500 -.0371600
 0.7499501 -.0314100
 0.7777300 -.0253500
 0.8043500 -.0192600
 0.8297000 -.0135400
 0.8535000 -.0083600
 0.8759000 -.0040600
 0.8964400 -.0005900
 0.9157100 0.0020300
 0.9329900 0.0038100
 0.9484800 0.0047900
 0.9619200 0.0050300
 0.9734400 0.0046100
 0.9829100 0.0037100
 0.9903400 0.0025900
 0.9957100 0.0014200
 0.9989100 0.0005100
 1.0000000 0.0000000
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Polars for FX 38-153 AIRFOIL (fx38153-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx38153-il50,000931.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx38153-il50,000526.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   fx38153-il100,000946.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx38153-il100,000536.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx38153-il200,000946.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx38153-il200,000547.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx38153-il500,000963.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx38153-il500,000560.8 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
   fx38153-il1,000,000991.5 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx38153-il1,000,000564.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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