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GOE 14 AIRFOIL (goe14-il)

GOE 14 AIRFOIL - Gottingen 14 airfoil


Airfoil goe14-il
Details Dat file Parser  
(goe14-il) GOE 14 AIRFOIL
Gottingen 14 airfoil
Max thickness 9.9% at 29.8% chord.
Max camber 6.9% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 14 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119700 0.0297100
 0.0242000 0.0446300
 0.0488400 0.0648700
 0.0735800 0.0793100
 0.0984000 0.0897600
 0.1481200 0.1051400
 0.1979700 0.1137300
 0.2978800 0.1188200
 0.3979700 0.1136000
 0.4981700 0.1025900
 0.5984300 0.0878800
 0.6987800 0.0685700
 0.7991700 0.0465700
 0.8995800 0.0235600
 0.9497899 0.0119500
 1.0000000 0.0006500

 0.0000000 0.0000000
 0.0128100 -.0172700
 0.0253200 -.0180500
 0.0502300 -.0131000
 0.0750600 -.0031600
 0.0999100 0.0050800
 0.1497600 0.0131700
 0.1997400 0.0163100
 0.2996500 0.0198500
 0.3996900 0.0183800
 0.4997200 0.0159200
 0.5997600 0.0137100
 0.6998100 0.0104900
 0.7998800 0.0067800
 0.8999299 0.0029500
 0.9499800 0.0010600
 1.0000000 -.0006500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 14 AIRFOIL (goe14-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe14-il50,000917.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14-il50,000534.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14-il100,000946.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14-il100,000553.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14-il200,000970.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14-il200,000570 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14-il500,000998.6 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14-il500,000593.9 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   goe14-il1,000,0009122.5 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe14-il1,000,0005111.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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