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GOE 575 AIRFOIL (goe575-il)

GOE 575 AIRFOIL - Gottingen 575 airfoil


Airfoil goe575-il
Details Dat file Parser  
(goe575-il) GOE 575 AIRFOIL
Gottingen 575 airfoil
Max thickness 13.3% at 29.8% chord.
Max camber 3.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 575 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120300 0.0282000
 0.0243300 0.0409000
 0.0490700 0.0563100
 0.0738800 0.0677200
 0.0987400 0.0766300
 0.1485400 0.0884500
 0.1984100 0.0962700
 0.2983100 0.1024200
 0.3983200 0.1015700
 0.4984100 0.0962200
 0.5985600 0.0873800
 0.6987500 0.0760300
 0.7989700 0.0626800
 0.8992900 0.0428400
 0.9495400 0.0281700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127800 -.0167900
 0.0253800 -.0230800
 0.0504500 -.0281700
 0.0755300 -.0322500
 0.1005600 -.0338400
 0.1505600 -.0340200
 0.2005400 -.0326900
 0.3005100 -.0310400
 0.4004900 -.0293900
 0.5004700 -.0282400
 0.6004600 -.0275900
 0.7004300 -.0259400
 0.8004000 -.0242900
 0.9003500 -.0211400
 0.9503200 -.0153100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 575 AIRFOIL (goe575-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe575-il50,000931.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe575-il50,000532.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe575-il100,000947.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe575-il100,000544.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe575-il200,000957.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe575-il200,000555.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe575-il500,000974.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe575-il500,000570.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe575-il1,000,000988.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe575-il1,000,000575.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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