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GOE 510 AIRFOIL (goe510-il)

GOE 510 AIRFOIL - Gottingen 510 airfoil


Airfoil goe510-il
Details Dat file Parser  
(goe510-il) GOE 510 AIRFOIL
Gottingen 510 airfoil
Max thickness 13.7% at 19.7% chord.
Max camber 5.8% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 510 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122400 0.0218800
 0.0242300 0.0350300
 0.0487100 0.0585700
 0.0733600 0.0746100
 0.0980900 0.0866600
 0.1477100 0.1042500
 0.1974600 0.1153400
 0.2972500 0.1250400
 0.3972900 0.1232400
 0.4974500 0.1159400
 0.5977400 0.1026500
 0.6981199 0.0853600
 0.7986100 0.0630700
 0.8992100 0.0357800
 0.9495800 0.0188900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0130400 -.0209900
 0.0255800 -.0264400
 0.0506200 -.0283900
 0.0756300 -.0288400
 0.1006300 -.0287900
 0.1505800 -.0261900
 0.2004800 -.0215900
 0.3002400 -.0108900
 0.4001400 -.0062000
 0.5002000 -.0090000
 0.6002900 -.0132900
 0.7003300 -.0150900
 0.8002800 -.0128900
 0.9001700 -.0077000
 0.9500800 -.0036000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 510 AIRFOIL (goe510-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe510-il50,00098.4 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe510-il50,000529.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe510-il100,000948.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe510-il100,000548.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe510-il200,000965.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe510-il200,000561.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe510-il500,000984.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe510-il500,000582.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe510-il1,000,0009106.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe510-il1,000,000599.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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