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GOE 624 AIRFOIL (goe624-il)

GOE 624 AIRFOIL - Gottingen 624 airfoil


Airfoil goe624-il
Details Dat file Parser  
(goe624-il) GOE 624 AIRFOIL
Gottingen 624 airfoil
Max thickness 16% at 30% chord.
Max camber 5.2% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 624 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0320000
 0.0250000 0.0460000
 0.0500000 0.0660000
 0.0750000 0.0805000
 0.1000000 0.0925000
 0.1500000 0.1095000
 0.2000000 0.1210000
 0.3000000 0.1320000
 0.4000000 0.1300000
 0.5000000 0.1205000
 0.6000000 0.1040000
 0.7000000 0.0830000
 0.8000000 0.0580000
 0.9000000 0.0315000
 0.9500000 0.0180000
 1.0000000 0.0050000

 0.0000000 0.0000000
 0.0125000 -.0170000
 0.0250000 -.0225000
 0.0500000 -.0285000
 0.0750000 -.0310000
 0.1000000 -.0320000
 0.1500000 -.0325000
 0.2000000 -.0315000
 0.3000000 -.0280000
 0.4000000 -.0240000
 0.5000000 -.0200000
 0.6000000 -.0160000
 0.7000000 -.0120000
 0.8000000 -.0080000
 0.9000000 -.0040000
 0.9500000 -.0020000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 624 AIRFOIL (goe624-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe624-il50,00095.9 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe624-il50,000522.8 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe624-il100,000939.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe624-il100,000550.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe624-il200,000969.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe624-il200,000569.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe624-il500,000999.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe624-il500,000597.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe624-il1,000,0009126.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe624-il1,000,0005120.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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