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Fage & Collins 2 (fg2-il)

Fage & Collins 2 - Fage & Collins 2 airfoil


Airfoil fg2-il
Details Dat file Parser  
(fg2-il) Fage & Collins 2
Fage & Collins 2 airfoil
Max thickness 8.2% at 30% chord.
Max camber 3.3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Fage & Collins 2
1.0000     0.0050
0.9500     0.0185
0.9000     0.0265
0.8000     0.0410
0.7000     0.0530
0.6000     0.0630
0.5000     0.0720
0.4000     0.0790
0.3000     0.0816
0.2000     0.0785
0.1500     0.0720
0.1000     0.0625
0.0750     0.0560
0.0500     0.0465
0.0250     0.0337
0.0125     0.0245
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     0.0050
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Lednicer format dat file
Selig format dat file

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Polars for Fage & Collins 2 (fg2-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fg2-il50,000933.2 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fg2-il50,000537.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fg2-il100,000951.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fg2-il100,000553.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fg2-il200,000969.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fg2-il200,000569.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fg2-il500,000993.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fg2-il500,000590.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fg2-il1,000,0009111.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fg2-il1,000,0005105.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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