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GOE 13K AIRFOIL (goe13k-il)

GOE 13K AIRFOIL - Gottingen 13K airfoil


Airfoil goe13k-il
Details Dat file Parser  
(goe13k-il) GOE 13K AIRFOIL
Gottingen 13K airfoil
Max thickness 14.8% at 50% chord.
Max camber 5.5% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 13K AIRFOIL
       15.       15.

 0.0000000 0.0000000
 0.0250000 0.0383500
 0.0500000 0.0535900
 0.1000000 0.0738900
 0.1500000 0.0889900
 0.2000000 0.1008800
 0.3000000 0.1168700
 0.4000000 0.1241600
 0.5000000 0.1280500
 0.6000000 0.1260400
 0.7000000 0.1130300
 0.8000000 0.0893200
 0.9000000 0.0542100
 0.9500000 0.0321100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0255500
 0.0500000 -.0301000
 0.1000000 -.0319100
 0.1500000 -.0304200
 0.2000000 -.0289200
 0.3000000 -.0259300
 0.4000000 -.0229400
 0.5000000 -.0199500
 0.6000000 -.0169600
 0.7000000 -.0139700
 0.8000000 -.0109800
 0.9000000 -.0079900
 0.9500000 -.0065000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 13K AIRFOIL (goe13k-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe13k-il50,000925.6 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe13k-il50,000520.9 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe13k-il100,000934.8 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe13k-il100,000530.3 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe13k-il200,000945.8 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe13k-il200,000542.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe13k-il500,000992.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe13k-il500,000585.8 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe13k-il1,000,0009129 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe13k-il1,000,000593.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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