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GOE 625 AIRFOIL (goe625-il)

GOE 625 AIRFOIL - Gottingen 625 airfoil


Airfoil goe625-il
Details Dat file Parser  
(goe625-il) GOE 625 AIRFOIL
Gottingen 625 airfoil
Max thickness 20% at 30% chord.
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 625 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0356900
 0.0250000 0.0543800
 0.0500000 0.0807500
 0.0750000 0.0986300
 0.1000000 0.1140000
 0.1500000 0.1357500
 0.2000000 0.1490000
 0.3000000 0.1615000
 0.4000000 0.1575000
 0.5000000 0.1460000
 0.6000000 0.1285000
 0.7000000 0.1045000
 0.8000000 0.0750000
 0.9000000 0.0420000
 0.9500000 0.0247500
 1.0000000 0.0065000

 0.0000000 0.0000000
 0.0125000 -.0213100
 0.0250000 -.0301300
 0.0500000 -.0397500
 0.0750000 -.0433800
 0.1000000 -.0455000
 0.1500000 -.0452500
 0.2000000 -.0430000
 0.3000000 -.0385000
 0.4000000 -.0330000
 0.5000000 -.0275000
 0.6000000 -.0220000
 0.7000000 -.0165000
 0.8000000 -.0110000
 0.9000000 -.0055000
 0.9500000 -.0027500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 625 AIRFOIL (goe625-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe625-il50,00093.8 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il50,000518.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il100,000933.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il100,000542.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il200,000958.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il200,000557.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il500,000980.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il500,000577.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il1,000,0009101.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il1,000,000599.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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