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GOE 269 AIRFOIL (goe269-il)

GOE 269 AIRFOIL - Gottingen 269 airfoil


Airfoil goe269-il
Details Dat file Parser  
(goe269-il) GOE 269 AIRFOIL
Gottingen 269 airfoil
Max thickness 6.6% at 29.9% chord.
Max camber 5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 269 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122700 0.0192500
 0.0246600 0.0287900
 0.0495100 0.0420000
 0.0744100 0.0515000
 0.0993100 0.0585000
 0.1491800 0.0691000
 0.1990900 0.0764700
 0.2990200 0.0824600
 0.3990400 0.0809500
 0.4991000 0.0752400
 0.5992300 0.0643300
 0.6993901 0.0512200
 0.7995700 0.0365100
 0.8997700 0.0197100
 0.9498600 0.0118000
 1.0000000 0.0029000

 0.0000000 0.0000000
 0.0126700 -.0116000
 0.0251700 -.0135000
 0.0501300 -.0113000
 0.0750700 -.0060100
 0.1000200 -.0017000
 0.1499300 0.0057500
 0.1998600 0.0113800
 0.2998000 0.0165700
 0.3997700 0.0195600
 0.4997600 0.0203500
 0.5997800 0.0182400
 0.6998300 0.0143300
 0.7999000 0.0085200
 0.8999700 0.0022100
 0.9500000 -.0002900
 1.0000000 -.0029000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 269 AIRFOIL (goe269-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe269-il50,000936.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe269-il50,000543.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe269-il100,000959.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe269-il100,000561.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe269-il200,000980.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe269-il200,000579.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe269-il500,0009107.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe269-il500,0005102.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe269-il1,000,0009127.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe269-il1,000,0005115.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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