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Fage & Collins 3 (fg3-il)

Fage & Collins 3 - Fage & Collins 3 airfoil


Airfoil fg3-il
Details Dat file Parser  
(fg3-il) Fage & Collins 3
Fage & Collins 3 airfoil
Max thickness 10.1% at 30% chord.
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Fage & Collins 3
1.0000     0.0065
0.9500     0.0225
0.9000     0.0325
0.8000     0.0533
0.7000     0.0705
0.6000     0.0835
0.5000     0.0925
0.4000     0.0985
0.3000     0.1014
0.2000     0.0976
0.1500     0.0900
0.1000     0.0758
0.0750     0.0660
0.0500     0.0528
0.0250     0.0370
0.0125     0.0270
0.0000     0.0083
0.0125     0.0000
0.0250     0.0000
0.0500     0.0000
0.0750     0.0000
0.1000     0.0000
0.1500     0.0000
0.2000     0.0000
0.3000     0.0000
0.4000     0.0000
0.5000     0.0000
0.6000     0.0000
0.7000     0.0000
0.8000     0.0000
0.9000     0.0000
0.9500     0.0000
1.0000     0.0065
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Lednicer format dat file
Selig format dat file

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Polars for Fage & Collins 3 (fg3-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fg3-il50,000932.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fg3-il50,000535.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fg3-il100,000948.8 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fg3-il100,000549.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fg3-il200,000965.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fg3-il200,000565.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fg3-il500,000990.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fg3-il500,000589 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fg3-il1,000,0009111.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fg3-il1,000,0005108.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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