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GOE 484 AIRFOIL (goe484-il)

GOE 484 AIRFOIL - Gottingen 484 airfoil


Airfoil goe484-il
Details Dat file Parser  
(goe484-il) GOE 484 AIRFOIL
Gottingen 484 airfoil
Max thickness 6.3% at 30% chord.
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 484 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0171500
 0.0250000 0.0233000
 0.0500000 0.0321000
 0.0750000 0.0399000
 0.1000000 0.0467000
 0.1500000 0.0578000
 0.2000000 0.0654000
 0.3000000 0.0751000
 0.4000000 0.0793000
 0.5000000 0.0765000
 0.6000000 0.0697000
 0.7000000 0.0598000
 0.8000000 0.0441000
 0.9000000 0.0248000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0115500
 0.0250000 -.0122000
 0.0500000 -.0115000
 0.0750000 -.0096000
 0.1000000 -.0068000
 0.1500000 -.0002000
 0.2000000 0.0054000
 0.3000000 0.0126000
 0.4000000 0.0188000
 0.5000000 0.0225000
 0.6000000 0.0242000
 0.7000000 0.0219000
 0.8000000 0.0171000
 0.9000000 0.0088000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 484 AIRFOIL (goe484-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe484-il50,000945 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe484-il50,000544.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe484-il100,000967.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe484-il100,000565.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe484-il200,000993.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe484-il200,000586.4 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe484-il500,0009128 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe484-il500,000593.4 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe484-il1,000,0009136.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe484-il1,000,000592.7 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
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