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GOE 647 AIRFOIL (goe647-il)

GOE 647 AIRFOIL - Gottingen 647 airfoil


Airfoil goe647-il
Details Dat file Parser  
(goe647-il) GOE 647 AIRFOIL
Gottingen 647 airfoil
Max thickness 16.2% at 19.5% chord.
Max camber 5.3% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 647 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111500 0.0314800
 0.0229800 0.0469900
 0.0470100 0.0695200
 0.0713000 0.0860700
 0.0957400 0.0991200
 0.1449400 0.1177300
 0.1945000 0.1278600
 0.2942800 0.1331500
 0.3944800 0.1284600
 0.4949800 0.1167800
 0.5957200 0.0996200
 0.6966100 0.0789500
 0.7976400 0.0548000
 0.8987700 0.0286500
 0.9493600 0.0148200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0132100 -.0164300
 0.0259400 -.0218800
 0.0512000 -.0278000
 0.0763400 -.0312200
 0.1014300 -.0331400
 0.1515300 -.0354800
 0.2014800 -.0343400
 0.3012300 -.0285500
 0.4009100 -.0212600
 0.5006000 -.0139700
 0.6004000 -.0091800
 0.7002300 -.0053900
 0.8001300 -.0030900
 0.9000599 -.0013000
 0.9500500 -.0011500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 647 AIRFOIL (goe647-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe647-il50,000913.1 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe647-il50,000528.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe647-il100,000941.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe647-il100,000544.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe647-il200,000959 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe647-il200,000558.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe647-il500,000981.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe647-il500,000581.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe647-il1,000,0009105.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe647-il1,000,0005104.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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