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GOE 415 AIRFOIL (goe415-il)

GOE 415 AIRFOIL - Gottingen 415 airfoil


Airfoil goe415-il
Details Dat file Parser  
(goe415-il) GOE 415 AIRFOIL
Gottingen 415 airfoil
Max thickness 8.5% at 19.9% chord.
Max camber 3.7% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 415 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123300 0.0167300
 0.0247300 0.0270500
 0.0495700 0.0423000
 0.0744600 0.0527600
 0.0993900 0.0600100
 0.1492900 0.0706200
 0.1992300 0.0760200
 0.2992100 0.0781400
 0.3992500 0.0737500
 0.4993400 0.0651700
 0.5994400 0.0553800
 0.6995500 0.0439000
 0.7996800 0.0311200
 0.8998400 0.0156300
 0.9499100 0.0084400
 1.0000000 0.0005500

 0.0000000 0.0000000
 0.0125400 -.0047000
 0.0250500 -.0056000
 0.0500700 -.0071000
 0.0750800 -.0084000
 0.1000900 -.0091800
 0.1500900 -.0091800
 0.2000900 -.0086700
 0.3000500 -.0049500
 0.4000100 -.0012400
 0.4999800 0.0018700
 0.5999800 0.0023900
 0.6999700 0.0028000
 0.7999700 0.0028200
 0.8999900 0.0005300
 0.9500100 -.0005600
 1.0000000 -.0005500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 415 AIRFOIL (goe415-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe415-il50,000934 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe415-il50,000537.2 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe415-il100,000952 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe415-il100,000553.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe415-il200,000968.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe415-il200,000569.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe415-il500,000992.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe415-il500,000590.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe415-il1,000,0009109.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe415-il1,000,0005106.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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