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GOE 381 AIRFOIL (goe381-il)

GOE 381 AIRFOIL - Gottingen 381 airfoil


Airfoil goe381-il
Details Dat file Parser  
(goe381-il) GOE 381 AIRFOIL
Gottingen 381 airfoil
Max thickness 6.4% at 30% chord.
Max camber 5.8% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 381 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124300 0.0162600
 0.0248800 0.0271100
 0.0498000 0.0434300
 0.0747400 0.0571400
 0.0997000 0.0653600
 0.1496500 0.0773900
 0.1996100 0.0837200
 0.2995900 0.0894800
 0.3995900 0.0883400
 0.4996300 0.0807000
 0.5996800 0.0703600
 0.6997400 0.0570200
 0.7998200 0.0398800
 0.8999100 0.0203400
 0.9499500 0.0103700
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0125200 -.0053400
 0.0250200 -.0038800
 0.0500000 0.0002300
 0.0749700 0.0057400
 0.0999500 0.0115600
 0.1499100 0.0195900
 0.1999000 0.0225200
 0.2998800 0.0256800
 0.3998800 0.0261400
 0.4998900 0.0239000
 0.5999100 0.0195600
 0.6999300 0.0143200
 0.7999600 0.0096800
 0.8999800 0.0041400
 0.9499900 0.0016700
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 381 AIRFOIL (goe381-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe381-il50,000937.6 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe381-il50,000543 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe381-il100,000958.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe381-il100,000561.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe381-il200,000980 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe381-il200,000576.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe381-il500,0009100.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe381-il500,000592 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe381-il1,000,0009111.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe381-il1,000,000593.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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