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GOE 602 AIRFOIL (goe602-il)

GOE 602 AIRFOIL - Gottingen 602 airfoil


Airfoil goe602-il
Details Dat file Parser  
(goe602-il) GOE 602 AIRFOIL
Gottingen 602 airfoil
Max thickness 10% at 30% chord.
Max camber 3.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 602 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0158100
 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 -.0190000
 0.1500000 -.0197500
 0.2000000 -.0200000
 0.3000000 -.0170000
 0.4000000 -.0135000
 0.5000000 -.0100000
 0.6000000 -.0065000
 0.7000000 -.0030000
 0.8000000 -.0010000
 0.9000000 0.0005000
 0.9500000 0.0007500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 602 AIRFOIL (goe602-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe602-il50,000937.8 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602-il50,000539.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602-il100,000957.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602-il100,000557.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602-il200,000977.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602-il200,000574 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602-il500,0009102.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602-il500,000593.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe602-il1,000,0009119.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe602-il1,000,0005104.9 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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