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GOE 167 (V.KARMAN PROP.2) AIRFOIL (goe167-il)

GOE 167 (V.KARMAN PROP.2) AIRFOIL - Gottingen 167 (V.Karman PROP.2) airfoil


Airfoil goe167-il
Details Dat file Parser  
(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL
Gottingen 167 (V.Karman PROP.2) airfoil
Max thickness 10.1% at 29.9% chord.
Max camber 4.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 167 (V.KARMAN PROP.2) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123600 0.0182000
 0.0247800 0.0283900
 0.0496800 0.0412800
 0.0746000 0.0521700
 0.0995200 0.0620700
 0.1494100 0.0766500
 0.1993400 0.0853300
 0.2992600 0.0958000
 0.3992700 0.0944700
 0.4993500 0.0838500
 0.5994600 0.0704200
 0.6995700 0.0553900
 0.7997000 0.0391600
 0.8998300 0.0223300
 0.9499000 0.0130100
 1.0000000 0.0045000

 0.0000000 0.0000000
 0.0125800 -.0110000
 0.0250900 -.0120100
 0.0500900 -.0113100
 0.0750800 -.0103200
 0.1000700 -.0087300
 0.1500600 -.0073400
 0.2000500 -.0063600
 0.3000400 -.0050900
 0.4000300 -.0038200
 0.5000200 -.0030500
 0.6000200 -.0027800
 0.7000200 -.0025100
 0.8000200 -.0023400
 0.9000200 -.0025700
 0.9500300 -.0039800
 1.0000000 -.0045000
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Lednicer format dat file
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Polars for GOE 167 (V.KARMAN PROP.2) AIRFOIL (goe167-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe167-il50,000926.6 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe167-il50,000534 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe167-il100,000958 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe167-il100,000558.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe167-il200,000980.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe167-il200,000578.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe167-il500,0009106.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe167-il500,000597.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe167-il1,000,0009124.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe167-il1,000,0005108.6 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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