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GOE 602 MOD. AIRFOIL (goe602m-il)

GOE 602 MOD. AIRFOIL - Gottingen 602 MOD airfoil


Airfoil goe602m-il
Details Dat file Parser  
(goe602m-il) GOE 602 MOD. AIRFOIL
Gottingen 602 MOD airfoil
Max thickness 9.6% at 30% chord.
Max camber 3.8% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 602 MOD. AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0153100
 0.0250000 0.0241200
 0.0500000 0.0382500
 0.0750000 0.0473800
 0.1000000 0.0550000
 0.1500000 0.0667500
 0.2000000 0.0745000
 0.3000000 0.0825000
 0.4000000 0.0830000
 0.5000000 0.0785000
 0.6000000 0.0700000
 0.7000000 0.0580000
 0.8000000 0.0425000
 0.9000000 0.0230000
 0.9500000 0.0122500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0098900
 0.0250000 -.0128800
 0.0500000 -.0162500
 0.0750000 -.0181300
 0.1000000 -.0187000
 0.1500000 -.0192500
 0.2000000 -.0190000
 0.3000000 -.0135000
 0.4000000 -.0081500
 0.5000000 -.0025000
 0.6000000 0.0025000
 0.7000000 0.0040000
 0.8000000 0.0050000
 0.9000000 0.0035000
 0.9500000 0.0017500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 602 MOD. AIRFOIL (goe602m-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe602m-il50,000939.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602m-il50,000540.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602m-il100,000959.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602m-il100,000559.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602m-il200,000980 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602m-il200,000576.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602m-il500,0009105.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602m-il500,000595.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602m-il1,000,0009122.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602m-il1,000,0005108.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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