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GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il)

GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL - Gottingen 303 (Friedrichshafen G03) airfoil


Airfoil goe303-il
Details Dat file Parser  
(goe303-il) GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL
Gottingen 303 (Friedrichshafen G03) airfoil
Max thickness 9.8% at 29.9% chord.
Max camber 5.9% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122400 0.0258300
 0.0246200 0.0372500
 0.0494600 0.0530100
 0.0743400 0.0647600
 0.0992400 0.0745200
 0.1490900 0.0887300
 0.1990100 0.0970400
 0.2989100 0.1059600
 0.3989100 0.1062900
 0.4989800 0.0993100
 0.5991000 0.0873400
 0.6992700 0.0716700
 0.7994600 0.0526900
 0.8997000 0.0292200
 0.9498300 0.0167400
 1.0000000 0.0022500

 0.0000000 0.0000000
 0.0126200 -.0105800
 0.0251300 -.0122400
 0.0501200 -.0119900
 0.0751000 -.0099300
 0.1000800 -.0074700
 0.1500300 -.0024600
 0.1999800 0.0021500
 0.2999200 0.0075700
 0.3998800 0.0113000
 0.4998700 0.0123200
 0.5998900 0.0111500
 0.6999100 0.0087700
 0.7999400 0.0057000
 0.8999900 0.0012200
 0.9500100 -.0011600
 1.0000000 -.0022500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe303-il50,000926.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe303-il50,000539.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe303-il100,000958.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe303-il100,000561.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe303-il200,000983.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe303-il200,000581.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe303-il500,0009114.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe303-il500,0005106.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe303-il1,000,0009137.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe303-il1,000,0005122.1 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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