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GOE 573 AIRFOIL (goe573-il)

GOE 573 AIRFOIL - Gottingen 573 airfoil


Airfoil goe573-il
Details Dat file Parser  
(goe573-il) GOE 573 AIRFOIL
Gottingen 573 airfoil
Max thickness 14.1% at 29.9% chord.
Max camber 6.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 573 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123900 0.0245600
 0.0248300 0.0371100
 0.0497400 0.0572200
 0.0746700 0.0738400
 0.0996100 0.0874500
 0.1495100 0.1087700
 0.1994500 0.1224000
 0.2993900 0.1353500
 0.3994100 0.1313000
 0.4994700 0.1182500
 0.5995500 0.0997000
 0.6996500 0.0786500
 0.7997500 0.0556000
 0.8998600 0.0315500
 0.9499199 0.0187700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125500 -.0104400
 0.0250600 -.0123900
 0.0500600 -.0122700
 0.0750500 -.0116600
 0.1000500 -.0105500
 0.1500400 -.0083200
 0.2000300 -.0076000
 0.3000300 -.0056500
 0.4000200 -.0042000
 0.5000200 -.0047500
 0.6000300 -.0058000
 0.7000300 -.0068500
 0.8000400 -.0079000
 0.9000400 -.0079500
 0.9500400 -.0047500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 573 AIRFOIL (goe573-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe573-il50,000911.6 at α=-4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe573-il50,000524.6 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe573-il100,000934.4 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe573-il100,000547.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe573-il200,000964.7 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe573-il200,000569.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe573-il500,000999.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe573-il500,0005100 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe573-il1,000,0009130.2 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe573-il1,000,0005127.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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