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GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL (goe301-il)

GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL - Gottingen 301 (Friedrichshafen G 13) airfoil


Airfoil goe301-il
Details Dat file Parser  
(goe301-il) GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL
Gottingen 301 (Friedrichshafen G 13) airfoil
Max thickness 10% at 28.9% chord.
Max camber 6.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122200 0.0274200
 0.0246000 0.0395500
 0.0494200 0.0573000
 0.0742800 0.0710600
 0.0991800 0.0808100
 0.1490200 0.0958200
 0.1989300 0.1053300
 0.2886400 0.1137400
 0.3988500 0.1123700
 0.4989400 0.1043900
 0.5990800 0.0904100
 0.6992500 0.0734300
 0.7994400 0.0544500
 0.8996800 0.0309800
 0.9498200 0.0179900
 1.0000000 0.0015000

 0.0000000 0.0000000
 0.0126000 -.0100700
 0.0251200 -.0114400
 0.0500900 -.0086900
 0.0750500 -.0044300
 0.1000100 -.0011800
 0.1499600 0.0043300
 0.1999100 0.0090400
 0.2998500 0.0148600
 0.3998200 0.0173800
 0.4998200 0.0179000
 0.5998200 0.0174200
 0.6998500 0.0144400
 0.7998900 0.0104600
 0.8999400 0.0054800
 0.9499800 0.0016900
 1.0000000 -.0015000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL (goe301-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe301-il50,000919 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe301-il50,000538.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe301-il100,000955.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe301-il100,000561.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe301-il200,000981.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe301-il200,000581.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe301-il500,0009112.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe301-il500,0005108.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe301-il1,000,0009138.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe301-il1,000,0005128.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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