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GOE 417 AIRFOIL (goe417-il)

GOE 417 AIRFOIL - Gottingen 417 airfoil


Airfoil goe417-il
Details Dat file Parser  
(goe417-il) GOE 417 AIRFOIL
Gottingen 417 airfoil
Max thickness 6% at 20% chord.
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 417 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0195800
 0.0250000 0.0296600
 0.0500000 0.0443200
 0.0750000 0.0564900
 0.1000000 0.0646500
 0.1500000 0.0759700
 0.2000000 0.0833000
 0.3000000 0.0884500
 0.4000000 0.0876000
 0.5000000 0.0822500
 0.6000000 0.0729000
 0.7000000 0.0605500
 0.8000000 0.0437000
 0.9000000 0.0233500
 0.9500000 0.0116800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0059200
 0.0250000 -.0038400
 0.0500000 0.0008300
 0.0750000 0.0049900
 0.1000000 0.0091500
 0.1500000 0.0164800
 0.2000000 0.0233000
 0.3000000 0.0319500
 0.4000000 0.0351000
 0.5000000 0.0332500
 0.6000000 0.0294000
 0.7000000 0.0230500
 0.8000000 0.0157000
 0.9000000 0.0073500
 0.9500000 0.0036800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 417 AIRFOIL (goe417-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe417-il50,000938.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417-il50,000544.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417-il100,000962 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417-il100,000563.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417-il200,000982.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417-il200,000578.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417-il500,0009105.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417-il500,0005102.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe417-il1,000,0009127.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe417-il1,000,0005115.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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