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GOE 648 AIRFOIL (goe648-il)

GOE 648 AIRFOIL - Gottingen 648 airfoil


Airfoil goe648-il
Details Dat file Parser  
(goe648-il) GOE 648 AIRFOIL
Gottingen 648 airfoil
Max thickness 15.2% at 29.4% chord.
Max camber 3.9% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 648 AIRFOIL
       18.       17.

 0.0000000 0.0000000
 0.0055500 0.0236700
 0.0106800 0.0330900
 0.0224000 0.0473200
 0.0464000 0.0655500
 0.0706400 0.0793800
 0.0950700 0.0897300
 0.1443100 0.1034400
 0.1938900 0.1111600
 0.2937000 0.1146500
 0.3938600 0.1116600
 0.4943500 0.1026900
 0.5950900 0.0892300
 0.6960300 0.0722800
 0.7971800 0.0513400
 0.8984600 0.0279200
 0.9491900 0.0147100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0133700 -.0157600
 0.0262200 -.0220600
 0.0516100 -.0291600
 0.0768000 -.0327800
 0.1019500 -.0353900
 0.1521000 -.0381300
 0.2021400 -.0388800
 0.3020300 -.0368900
 0.4018100 -.0329000
 0.5014800 -.0269200
 0.6011000 -.0199400
 0.7007400 -.0134600
 0.8003800 -.0069800
 0.9001600 -.0029900
 0.9501000 -.0017400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 648 AIRFOIL (goe648-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe648-il50,000922.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe648-il50,000530.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe648-il100,000943.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe648-il100,000544.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe648-il200,000957.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe648-il200,000557.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe648-il500,000979.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe648-il500,000580.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe648-il1,000,0009104.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe648-il1,000,0005101.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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