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GOE 613 AIRFOIL (goe613-il)

GOE 613 AIRFOIL - Gottingen 613 airfoil


Airfoil goe613-il
Details Dat file Parser  
(goe613-il) GOE 613 AIRFOIL
Gottingen 613 airfoil
Max thickness 10.3% at 30% chord.
Max camber 4.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 613 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0181900
 0.0250000 0.0293900
 0.0500000 0.0457700
 0.0750000 0.0576600
 0.1000000 0.0665500
 0.1500000 0.0793200
 0.2000000 0.0866000
 0.3000000 0.0921500
 0.4000000 0.0912000
 0.5000000 0.0852500
 0.6000000 0.0763000
 0.7000000 0.0623500
 0.8000000 0.0454000
 0.9000000 0.0244500
 0.9500000 0.0132200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0118100
 0.0250000 -.0141100
 0.0500000 -.0142300
 0.0750000 -.0143400
 0.1000000 -.0139500
 0.1500000 -.0131700
 0.2000000 -.0124000
 0.3000000 -.0108500
 0.4000000 -.0093000
 0.5000000 -.0077500
 0.6000000 -.0062000
 0.7000000 -.0046500
 0.8000000 -.0031000
 0.9000000 -.0015500
 0.9500000 -.0007800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 613 AIRFOIL (goe613-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe613-il50,000930.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe613-il50,000537 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe613-il100,000953.3 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe613-il100,000552.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe613-il200,000972.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe613-il200,000567.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe613-il500,000993.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe613-il500,000588.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe613-il1,000,0009112 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe613-il1,000,0005106 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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