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GOE 604 AIRFOIL (goe604-il)

GOE 604 AIRFOIL - Gottingen 604 airfoil


Airfoil goe604-il
Details Dat file Parser  
(goe604-il) GOE 604 AIRFOIL
Gottingen 604 airfoil
Max thickness 17.8% at 29.3% chord.
Max camber 5.4% at 29.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 604 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0108300 0.0330500
 0.0225200 0.0491400
 0.0463500 0.0723400
 0.0704300 0.0905600
 0.0947400 0.1042800
 0.1438300 0.1222600
 0.1932000 0.1347600
 0.2927900 0.1427900
 0.3930900 0.1368500
 0.4938700 0.1214400
 0.5949000 0.1010400
 0.6960300 0.0786500
 0.7972600 0.0542600
 0.8986200 0.0273800
 0.9493200 0.0134400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0132800 -.0154200
 0.0261000 -.0216800
 0.0514600 -.0289000
 0.0767000 -.0336300
 0.1018600 -.0368600
 0.1519600 -.0388300
 0.2019600 -.0388000
 0.3017800 -.0352600
 0.4015300 -.0302200
 0.5012700 -.0251900
 0.6010200 -.0201500
 0.7007599 -.0151100
 0.8005100 -.0100700
 0.9002500 -.0050400
 0.9501300 -.0025200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 604 AIRFOIL (goe604-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe604-il50,00093.7 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe604-il50,000520.6 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe604-il100,000929.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe604-il100,000542.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe604-il200,000959.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe604-il200,000561.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe604-il500,000987.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe604-il500,000585.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe604-il1,000,0009113 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe604-il1,000,0005108.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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