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GOE 633 AIRFOIL (goe633-il)

GOE 633 AIRFOIL - Gottingen 633 airfoil


Airfoil goe633-il
Details Dat file Parser  
(goe633-il) GOE 633 AIRFOIL
Gottingen 633 airfoil
Max thickness 13.8% at 19.7% chord.
Max camber 4% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 633 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0117300 0.0248600
 0.0238300 0.0377400
 0.0482600 0.0560000
 0.0728500 0.0692600
 0.0975700 0.0785200
 0.1471300 0.0925600
 0.1968500 0.1016000
 0.2966800 0.1072000
 0.3967800 0.1038000
 0.4971400 0.0924100
 0.5976700 0.0750300
 0.6983200 0.0541500
 0.7989500 0.0337700
 0.8994900 0.0163800
 0.9497500 0.0079400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0131200 -.0200900
 0.0257800 -.0252000
 0.0509700 -.0314200
 0.0761100 -.0356400
 0.1011600 -.0373600
 0.1511900 -.0383100
 0.2011100 -.0357700
 0.3009000 -.0291700
 0.4007600 -.0245800
 0.5006700 -.0214800
 0.6006200 -.0198800
 0.7006100 -.0197800
 0.8005600 -.0181800
 0.9003600 -.0115900
 0.9501899 -.0060400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 633 AIRFOIL (goe633-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe633-il50,00099.7 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe633-il50,000526.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe633-il100,000943.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe633-il100,000548.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe633-il200,000967.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe633-il200,000566.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe633-il500,000994.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe633-il500,000590.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe633-il1,000,0009118.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe633-il1,000,0005102.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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