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FX 67-K-150/17 AIRFOIL (fx67k150-il)

FX 67-K-150/17 AIRFOIL - Wortmann FX 67-K-150/17 airfoil


Airfoil fx67k150-il
Details Dat file Parser  
(fx67k150-il) FX 67-K-150/17 AIRFOIL
Wortmann FX 67-K-150/17 airfoil
Max thickness 15% at 40.2% chord.
Max camber 4.8% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 67-K-150/17 AIRFOIL
       44.       44.

 0.0000000 0.0000000
 0.0010700 0.0046200
 0.0042800 0.0098900
 0.0096100 0.0162600
 0.0170400 0.0231000
 0.0265300 0.0299200
 0.0380600 0.0375200
 0.0515600 0.0453600
 0.0669900 0.0532700
 0.0842700 0.0611000
 0.1033200 0.0688200
 0.1240800 0.0762900
 0.1464500 0.0834800
 0.1703300 0.0902700
 0.1956200 0.0966300
 0.2222100 0.1024600
 0.2500000 0.1077100
 0.2788600 0.1123000
 0.3086600 0.1161900
 0.3392800 0.1192800
 0.3705900 0.1215200
 0.4024500 0.1228500
 0.4347400 0.1231800
 0.4673000 0.1223900
 0.5000000 0.1204100
 0.5327000 0.1171600
 0.5652600 0.1126900
 0.5975500 0.1070200
 0.6294100 0.1002500
 0.6607200 0.0924900
 0.6913400 0.0839500
 0.7211400 0.0749000
 0.7500000 0.0657000
 0.7777900 0.0567000
 0.8043801 0.0482700
 0.8296700 0.0406500
 0.8535500 0.0339400
 0.8759201 0.0280900
 0.9157300 0.0185600
 0.9484400 0.0113000
 0.9734700 0.0059900
 0.9903900 0.0023300
 0.9989300 0.0002600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0014500
 0.0042800 -.0037500
 0.0096100 -.0060700
 0.0170400 -.0080400
 0.0265300 -.0101500
 0.0380600 -.0122400
 0.0515600 -.0142200
 0.0669900 -.0161100
 0.0842700 -.0178800
 0.1033200 -.0195500
 0.1240800 -.0210700
 0.1464500 -.0224600
 0.1703300 -.0236800
 0.1956200 -.0247400
 0.2222100 -.0256200
 0.2500000 -.0263200
 0.2788600 -.0268400
 0.3086600 -.0271700
 0.3392800 -.0273000
 0.3705900 -.0272400
 0.4024500 -.0269800
 0.4347400 -.0265300
 0.4673000 -.0258800
 0.5000000 -.0250400
 0.5327000 -.0239900
 0.5652600 -.0227400
 0.5975500 -.0213000
 0.6294100 -.0196700
 0.6607200 -.0178400
 0.6913400 -.0157500
 0.7211400 -.0133900
 0.7500000 -.0108000
 0.7777900 -.0081300
 0.8043801 -.0055900
 0.8296700 -.0033400
 0.8535500 -.0014800
 0.8759201 -.0000600
 0.9157300 0.0015700
 0.9484400 0.0019300
 0.9734700 0.0014200
 0.9903900 0.0006000
 0.9989300 0.0000700
 1.0000000 0.0000000
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Polars for FX 67-K-150/17 AIRFOIL (fx67k150-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx67k150-il50,00095.8 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   fx67k150-il50,000514.3 at α=12°Mach=0 Ncrit=5Xfoil predictionDetails
   fx67k150-il100,000925 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx67k150-il100,000527.1 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   fx67k150-il200,000961.6 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx67k150-il200,000568.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx67k150-il500,0009126.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx67k150-il500,0005118.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx67k150-il1,000,0009157.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx67k150-il1,000,0005147.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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