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GOE 676 (= M 12) AIRFOIL (goe676-il)

GOE 676 (= M 12) AIRFOIL - Gottingen 676 (= M 12) airfoil


Airfoil goe676-il
Details Dat file Parser  
(goe676-il) GOE 676 (= M 12) AIRFOIL
Gottingen 676 (= M 12) airfoil
Max thickness 11.9% at 30% chord.
Max camber 2% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 676 (= M 12) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0186200
 0.0250000 0.0270400
 0.0500000 0.0395700
 0.0750000 0.0486100
 0.1000000 0.0551500
 0.1500000 0.0662200
 0.2000000 0.0738000
 0.3000000 0.0799500
 0.4000000 0.0791000
 0.5000000 0.0732500
 0.6000000 0.0629000
 0.7000000 0.0505500
 0.8000000 0.0352000
 0.9000000 0.0193500
 0.9500000 0.0109200
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0159800
 0.0250000 -.0214600
 0.0500000 -.0269300
 0.0750000 -.0298900
 0.1000000 -.0323500
 0.1500000 -.0347700
 0.2000000 -.0367000
 0.3000000 -.0390500
 0.4000000 -.0389000
 0.5000000 -.0367500
 0.6000000 -.0336000
 0.7000000 -.0284500
 0.8000000 -.0213000
 0.9000000 -.0111500
 0.9500000 -.0055800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 676 (= M 12) AIRFOIL (goe676-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe676-il50,000930.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe676-il50,000533.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe676-il100,000948.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe676-il100,000548.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe676-il200,000965.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe676-il200,000562.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe676-il500,000986.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe676-il500,000577.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe676-il1,000,000997.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe676-il1,000,000585.9 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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