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GOE 376 AIRFOIL (goe376-il)

GOE 376 AIRFOIL - Gottingen 376 airfoil


Airfoil goe376-il
Details Dat file Parser  
(goe376-il) GOE 376 AIRFOIL
Gottingen 376 airfoil
Max thickness 6.6% at 30% chord.
Max camber 5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 376 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124000 0.0180700
 0.0248400 0.0284400
 0.0497600 0.0425800
 0.0747000 0.0532300
 0.0996500 0.0608700
 0.1495900 0.0713500
 0.1995500 0.0774400
 0.2995300 0.0825100
 0.3995400 0.0798800
 0.4995800 0.0736500
 0.5996400 0.0637200
 0.6997100 0.0507900
 0.7997900 0.0363600
 0.8998900 0.0199300
 0.9499300 0.0114100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125500 -.0081300
 0.0250300 -.0058600
 0.0500100 -.0019100
 0.0749900 0.0014300
 0.0999700 0.0046700
 0.1499500 0.0094500
 0.1999300 0.0129400
 0.2999100 0.0165100
 0.3999000 0.0178800
 0.4999100 0.0166500
 0.5999200 0.0140200
 0.6999400 0.0112900
 0.7999600 0.0068600
 0.8999900 0.0024300
 0.9500000 -.0002800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 376 AIRFOIL (goe376-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe376-il50,000933.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe376-il50,000541.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe376-il100,000956.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe376-il100,000558.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe376-il200,000976.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe376-il200,000576.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe376-il500,0009105.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe376-il500,000596 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe376-il1,000,0009121.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe376-il1,000,000597.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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