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GOE 403 AIRFOIL (goe403-il)

GOE 403 AIRFOIL - Gottingen 403 airfoil


Airfoil goe403-il
Details Dat file Parser  
(goe403-il) GOE 403 AIRFOIL
Gottingen 403 airfoil
Max thickness 6.7% at 29.9% chord.
Max camber 4.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 403 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123900 0.0106300
 0.0248100 0.0182600
 0.0496800 0.0300200
 0.0745800 0.0397800
 0.0995000 0.0480400
 0.1493700 0.0595700
 0.1992900 0.0675900
 0.2992100 0.0751400
 0.3992200 0.0741900
 0.4992800 0.0682400
 0.5993700 0.0597900
 0.6995000 0.0478400
 0.7996500 0.0329000
 0.8998100 0.0179500
 0.9499000 0.0094700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125800 -.0078700
 0.0251000 -.0097400
 0.0501000 -.0099700
 0.0750900 -.0087100
 0.1000700 -.0064500
 0.1500200 -.0019200
 0.1999800 0.0021000
 0.2999100 0.0086500
 0.3998700 0.0122000
 0.4998600 0.0137500
 0.5998700 0.0128000
 0.6998900 0.0103500
 0.7999200 0.0074000
 0.8999600 0.0039500
 0.9499800 0.0019700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 403 AIRFOIL (goe403-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe403-il50,000942.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe403-il50,000541.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe403-il100,000959.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe403-il100,000557.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe403-il200,000975.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe403-il200,000573 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe403-il500,000998.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe403-il500,000592.9 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe403-il1,000,0009116.1 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe403-il1,000,0005107.9 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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