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GOE 650 AIRFOIL (goe650-il)

GOE 650 AIRFOIL - Gottingen 650 airfoil


Airfoil goe650-il
Details Dat file Parser  
(goe650-il) GOE 650 AIRFOIL
Gottingen 650 airfoil
Max thickness 13.4% at 19.5% chord.
Max camber 4.4% at 49.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 650 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0112400 0.0250700
 0.0232000 0.0356700
 0.0473600 0.0523900
 0.0717600 0.0641200
 0.0963200 0.0728600
 0.1456900 0.0853600
 0.1952900 0.0933600
 0.2948800 0.1013900
 0.3948000 0.1029400
 0.4950500 0.0980000
 0.5955300 0.0885700
 0.6963300 0.0726600
 0.7973400 0.0527700
 0.8985400 0.0288800
 0.9492199 0.0154400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0134800 -.0193200
 0.0263200 -.0261700
 0.0517600 -.0348900
 0.0770000 -.0396100
 0.1021100 -.0418400
 0.1521400 -.0423200
 0.2020400 -.0403000
 0.3016100 -.0317700
 0.4010200 -.0202500
 0.5004700 -.0092300
 0.6000400 -.0007000
 0.6997800 0.0043400
 0.7997500 0.0048900
 0.8999000 0.0019500
 0.9499800 0.0004700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 650 AIRFOIL (goe650-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe650-il50,000931.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe650-il50,000534.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe650-il100,000956 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe650-il100,000553.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe650-il200,000979 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe650-il200,000570.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe650-il500,0009101.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe650-il500,000583.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe650-il1,000,0009109.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe650-il1,000,000596.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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