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GOE 407 AIRFOIL (goe407-il)

GOE 407 AIRFOIL - Gottingen 407 airfoil


Airfoil goe407-il
Details Dat file Parser  
(goe407-il) GOE 407 AIRFOIL
Gottingen 407 airfoil
Max thickness 9.5% at 29.9% chord.
Max camber 4.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 407 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123500 0.0218800
 0.0247800 0.0325700
 0.0496800 0.0474300
 0.0746100 0.0579000
 0.0995600 0.0660700
 0.1494700 0.0797000
 0.1994100 0.0880400
 0.2993600 0.0950100
 0.3993700 0.0946800
 0.4994000 0.0889500
 0.5994900 0.0768200
 0.6995800 0.0622900
 0.7997000 0.0452600
 0.8998200 0.0267300
 0.9498800 0.0141700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125900 -.0132200
 0.0251000 -.0142300
 0.0500900 -.0135600
 0.0750800 -.0112000
 0.1000600 -.0094300
 0.1500400 -.0053900
 0.2000200 -.0024600
 0.3000000 0.0004100
 0.3999900 0.0008800
 0.5000000 0.0001500
 0.6000100 -.0007800
 0.7000200 -.0028100
 0.8000300 -.0047400
 0.9000500 -.0067700
 0.9500500 -.0055300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 407 AIRFOIL (goe407-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe407-il50,000927.9 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe407-il50,000537.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe407-il100,000956.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe407-il100,000557.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe407-il200,000979.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe407-il200,000575.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe407-il500,0009106.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe407-il500,000595.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe407-il1,000,0009121.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe407-il1,000,0005114.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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