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FX 60-100 AIRFOIL (fx60100-il)

FX 60-100 AIRFOIL - Wortmann FX 60-100 airfoil


Airfoil fx60100-il
Details Dat file Parser  
(fx60100-il) FX 60-100 AIRFOIL
Wortmann FX 60-100 airfoil
Max thickness 10% at 27.9% chord.
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 60-100 AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010700 0.0057400
 0.0042800 0.0114400
 0.0096100 0.0177500
 0.0170400 0.0236800
 0.0265300 0.0294800
 0.0380600 0.0352300
 0.0515600 0.0405600
 0.0669900 0.0460900
 0.0842700 0.0508600
 0.1033200 0.0556900
 0.1240800 0.0598900
 0.1464500 0.0640400
 0.1703300 0.0675400
 0.1956200 0.0708100
 0.2222100 0.0733900
 0.2500000 0.0756500
 0.2788600 0.0772000
 0.3086600 0.0783800
 0.3392800 0.0788800
 0.3705900 0.0789800
 0.4024500 0.0784500
 0.4347400 0.0775000
 0.4673000 0.0759600
 0.5000000 0.0740900
 0.5327000 0.0717400
 0.5652600 0.0691100
 0.5975500 0.0660800
 0.6294100 0.0627500
 0.6607200 0.0590500
 0.6913400 0.0551100
 0.7211400 0.0508900
 0.7500000 0.0465200
 0.7777900 0.0420000
 0.8043801 0.0374700
 0.8296700 0.0329800
 0.8535500 0.0286400
 0.8759201 0.0244700
 0.8966800 0.0205300
 0.9157300 0.0168100
 0.9330100 0.0134200
 0.9484400 0.0103500
 0.9619400 0.0076600
 0.9734700 0.0053400
 0.9829600 0.0034100
 0.9903900 0.0019300
 0.9957200 0.0008600
 0.9989300 0.0002300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0020000
 0.0042800 -.0043600
 0.0096100 -.0069100
 0.0170400 -.0097000
 0.0265300 -.0124700
 0.0380600 -.0148100
 0.0515600 -.0173000
 0.0669900 -.0191300
 0.0842700 -.0211000
 0.1033200 -.0224600
 0.1240800 -.0237700
 0.1464500 -.0244700
 0.1703300 -.0250300
 0.1956200 -.0250000
 0.2222100 -.0247500
 0.2500000 -.0238900
 0.2788600 -.0227500
 0.3086600 -.0210000
 0.3392800 -.0189500
 0.3705900 -.0163700
 0.4024500 -.0135700
 0.4347400 -.0104500
 0.4673000 -.0073100
 0.5000000 -.0040500
 0.5327000 -.0009200
 0.5652600 0.0021700
 0.5975500 0.0049600
 0.6294100 0.0074800
 0.6607200 0.0095100
 0.6913400 0.0111800
 0.7211400 0.0124100
 0.7500000 0.0132900
 0.7777900 0.0137300
 0.8043801 0.0138100
 0.8296700 0.0134700
 0.8535500 0.0128000
 0.8759201 0.0118600
 0.8966800 0.0107200
 0.9157300 0.0094100
 0.9330100 0.0080200
 0.9484400 0.0065900
 0.9619400 0.0051500
 0.9734700 0.0037700
 0.9829600 0.0025100
 0.9903900 0.0015100
 0.9957200 0.0007000
 0.9989300 0.0001500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for FX 60-100 AIRFOIL (fx60100-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx60100-il50,000940.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100-il50,000542.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100-il100,000962.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100-il100,000561.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100-il200,000984.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100-il200,000577.7 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100-il500,0009109.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100-il500,000587.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   fx60100-il1,000,0009112.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx60100-il1,000,000596.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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