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GOE 645 AIRFOIL (goe645-il)

GOE 645 AIRFOIL - Gottingen 645 airfoil


Airfoil goe645-il
Details Dat file Parser  
(goe645-il) GOE 645 AIRFOIL
Gottingen 645 airfoil
Max thickness 15.4% at 19.4% chord.
Max camber 4.8% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 645 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111200 0.0285400
 0.0229300 0.0426100
 0.0469300 0.0632800
 0.0711700 0.0789500
 0.0956800 0.0891400
 0.1448600 0.1060300
 0.1944000 0.1154300
 0.2940700 0.1222600
 0.3943000 0.1176200
 0.4948600 0.1060000
 0.5956400 0.0898900
 0.6966200 0.0697900
 0.7976600 0.0481900
 0.8987600 0.0255900
 0.9493400 0.0135400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0132900 -.0163600
 0.0261000 -.0227300
 0.0514800 -.0305000
 0.0767400 -.0357800
 0.1018500 -.0380600
 0.1519500 -.0401300
 0.2018800 -.0387100
 0.3014500 -.0298800
 0.4010000 -.0205500
 0.5006400 -.0132200
 0.6003600 -.0073800
 0.7007000 -.0044300
 0.8001100 -.0021900
 0.9000400 -.0008500
 0.9500200 -.0004200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 645 AIRFOIL (goe645-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe645-il50,00099.5 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe645-il50,000528.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe645-il100,000943.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe645-il100,000548.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe645-il200,000966.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe645-il200,000565.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe645-il500,000993.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe645-il500,000584.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe645-il1,000,0009110.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe645-il1,000,000588.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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