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GOE 515 AIRFOIL (goe515-il)

GOE 515 AIRFOIL - Gottingen 515 airfoil


Airfoil goe515-il
Details Dat file Parser  
(goe515-il) GOE 515 AIRFOIL
Gottingen 515 airfoil
Max thickness 8.5% at 30% chord.
Max camber 2.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 515 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0153200
 0.0250000 0.0226400
 0.0500000 0.0327700
 0.0750000 0.0404100
 0.1000000 0.0460500
 0.1500000 0.0548300
 0.2000000 0.0616000
 0.3000000 0.0681500
 0.4000000 0.0692000
 0.5000000 0.0662500
 0.6000000 0.0588000
 0.7000000 0.0478500
 0.8000000 0.0334000
 0.9000000 0.0174500
 0.9500000 0.0087300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0131800
 0.0250000 -.0178600
 0.0500000 -.0227300
 0.0750000 -.0245900
 0.1000000 -.0244500
 0.1500000 -.0231800
 0.2000000 -.0209000
 0.3000000 -.0163500
 0.4000000 -.0133000
 0.5000000 -.0107500
 0.6000000 -.0097000
 0.7000000 -.0081500
 0.8000000 -.0071000
 0.9000000 -.0045500
 0.9500000 -.0027800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 515 AIRFOIL (goe515-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe515-il50,000937.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe515-il50,000537.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe515-il100,000956.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe515-il100,000554.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe515-il200,000977.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe515-il200,000571 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe515-il500,0009103.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe515-il500,000588 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe515-il1,000,0009119 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe515-il1,000,000595.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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