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GOE 493 AIRFOIL (goe493-il)

GOE 493 AIRFOIL - Gottingen 493 airfoil


Airfoil goe493-il
Details Dat file Parser  
(goe493-il) GOE 493 AIRFOIL
Gottingen 493 airfoil
Max thickness 14.9% at 29.3% chord.
Max camber 3.4% at 49.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 493 AIRFOIL
       17.       17.

 0.0000100 0.0000000
 0.0110100 0.0212800
 0.0228800 0.0301100
 0.0469200 0.0438100
 0.0711600 0.0545200
 0.0955100 0.0637300
 0.1444900 0.0781900
 0.1936800 0.0896500
 0.2928000 0.1021400
 0.3925200 0.1061700
 0.4928000 0.1022400
 0.5935300 0.0918400
 0.6946499 0.0759700
 0.7961500 0.0546300
 0.8979700 0.0288100
 0.9489500 0.0149000
 1.0000000 0.0000000

 0.0000100 0.0000000
 0.0136000 -.0155400
 0.0266000 -.0226200
 0.0522500 -.0318200
 0.0776500 -.0375300
 0.1029100 -.0412400
 0.1532300 -.0457000
 0.2033700 -.0476600
 0.3033300 -.0471200
 0.4029700 -.0420900
 0.5024100 -.0340800
 0.6017700 -.0250800
 0.7011700 -.0165700
 0.8006000 -.0085600
 0.9002100 -.0030300
 0.9500000 -.0013300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 493 AIRFOIL (goe493-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe493-il50,000924.2 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe493-il50,000524.4 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe493-il100,000951.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe493-il100,000551.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe493-il200,000975.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe493-il200,000572.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe493-il500,0009105.9 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe493-il500,000595.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe493-il1,000,0009127.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe493-il1,000,000598.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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