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GOE 683 AIRFOIL (goe683-il)

GOE 683 AIRFOIL - Gottingen 683 airfoil


Airfoil goe683-il
Details Dat file Parser  
(goe683-il) GOE 683 AIRFOIL
Gottingen 683 airfoil
Max thickness 19.9% at 30% chord.
Max camber 3% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 683 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0300000
 0.0250000 0.0450000
 0.0500000 0.0650000
 0.0750000 0.0800000
 0.1000000 0.0910000
 0.1500000 0.1090000
 0.2000000 0.1205000
 0.3000000 0.1290000
 0.4000000 0.1240000
 0.5000000 0.1110000
 0.6000000 0.0920000
 0.7000000 0.0700000
 0.8000000 0.0460000
 0.9000000 0.0230000
 0.9500000 0.0120000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0250000
 0.0250000 -.0350000
 0.0500000 -.0465000
 0.0750000 -.0535000
 0.1000000 -.0595000
 0.1500000 -.0660000
 0.2000000 -.0690000
 0.3000000 -.0700000
 0.4000000 -.0680000
 0.5000000 -.0635000
 0.6000000 -.0575000
 0.7000000 -.0500000
 0.8000000 -.0410000
 0.9000000 -.0270000
 0.9500000 -.0160000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 683 AIRFOIL (goe683-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe683-il50,00097.9 at α=-0.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe683-il50,000521.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe683-il100,000931.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe683-il100,000541.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe683-il200,000958.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe683-il200,000559.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe683-il500,000985.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe683-il500,000570.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe683-il1,000,000998.2 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe683-il1,000,000581.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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