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GOE 385 AIRFOIL (goe385-il)

GOE 385 AIRFOIL - Gottingen 385 airfoil


Airfoil goe385-il
Details Dat file Parser  
(goe385-il) GOE 385 AIRFOIL
Gottingen 385 airfoil
Max thickness 9.9% at 29.9% chord.
Max camber 4.1% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 385 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123300 0.0198000
 0.0247400 0.0303100
 0.0496200 0.0445000
 0.0745200 0.0561300
 0.0994500 0.0643500
 0.1493500 0.0773700
 0.1992700 0.0851000
 0.2992300 0.0908400
 0.3992400 0.0895900
 0.4993000 0.0820400
 0.5994100 0.0694900
 0.6995300 0.0556500
 0.7996700 0.0385000
 0.8998200 0.0213500
 0.9499000 0.0112700
 1.0000000 0.0021000

 0.0000000 0.0000000
 0.0125800 -.0093900
 0.0250900 -.0103900
 0.0500900 -.0101700
 0.0750800 -.0099600
 0.1000800 -.0097500
 0.1500800 -.0093200
 0.2000800 -.0089000
 0.3000700 -.0080500
 0.4000600 -.0072000
 0.5000500 -.0063500
 0.6000500 -.0055000
 0.7000400 -.0046500
 0.8000300 -.0038000
 0.9000300 -.0029500
 0.9500200 -.0025200
 1.0000000 -.0021000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 385 AIRFOIL (goe385-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe385-il50,000929.8 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe385-il50,000537.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe385-il100,000951.8 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe385-il100,000556.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe385-il200,000973 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe385-il200,000572.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe385-il500,000997.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe385-il500,000593.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe385-il1,000,0009115.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe385-il1,000,0005108.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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