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GOE 655 AIRFOIL (goe655-il)

GOE 655 AIRFOIL - Gottingen 655 airfoil


Airfoil goe655-il
Details Dat file Parser  
(goe655-il) GOE 655 AIRFOIL
Gottingen 655 airfoil
Max thickness 13.9% at 30% chord.
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 655 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0269800
 0.0250000 0.0404600
 0.0500000 0.0604300
 0.0750000 0.0748900
 0.1000000 0.0853500
 0.1500000 0.0987700
 0.2000000 0.1077000
 0.3000000 0.1125500
 0.4000000 0.1089000
 0.5000000 0.0997500
 0.6000000 0.0861000
 0.7000000 0.0684500
 0.8000000 0.0488000
 0.9000000 0.0256500
 0.9500000 0.0130800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0140200
 0.0250000 -.0190400
 0.0500000 -.0240800
 0.0750000 -.0271100
 0.1000000 -.0291500
 0.1500000 -.0307200
 0.2000000 -.0303000
 0.3000000 -.0264500
 0.4000000 -.0211000
 0.5000000 -.0157500
 0.6000000 -.0114000
 0.7000000 -.0075500
 0.8000000 -.0042000
 0.9000000 -.0018500
 0.9500000 -.0009300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 655 AIRFOIL (goe655-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe655-il50,000916.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe655-il50,000532.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe655-il100,000945.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe655-il100,000549 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe655-il200,000964.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe655-il200,000564.9 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe655-il500,000991.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe655-il500,000589.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe655-il1,000,0009115.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe655-il1,000,0005109 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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