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GOE 365 AIRFOIL (goe365-il)

GOE 365 AIRFOIL - Gottingen 365 airfoil


Airfoil goe365-il
Details Dat file Parser  
(goe365-il) GOE 365 AIRFOIL
Gottingen 365 airfoil
Max thickness 11.7% at 29.9% chord.
Max camber 5.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 365 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122200 0.0266300
 0.0245900 0.0387600
 0.0493900 0.0580200
 0.0742600 0.0702800
 0.0991500 0.0805400
 0.1490200 0.0935600
 0.1989300 0.1015900
 0.2988500 0.1096400
 0.3988500 0.1091900
 0.4989200 0.1027400
 0.5990500 0.0902900
 0.6992500 0.0713400
 0.7994700 0.0503900
 0.8997200 0.0269500
 0.9498500 0.0144700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126000 -.0093700
 0.0251100 -.0102400
 0.0501000 -.0099700
 0.0751000 -.0097100
 0.1001000 -.0094500
 0.1500900 -.0089200
 0.2000900 -.0084000
 0.3000800 -.0073500
 0.4000700 -.0063000
 0.5000600 -.0052500
 0.6000400 -.0042000
 0.7000300 -.0031500
 0.8000200 -.0021000
 0.9000100 -.0010500
 0.9500100 -.0005200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 365 AIRFOIL (goe365-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe365-il50,000927.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe365-il50,000534.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe365-il100,000955.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe365-il100,000555.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe365-il200,000979.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe365-il200,000573.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe365-il500,0009107.2 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe365-il500,000590.6 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe365-il1,000,0009120.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe365-il1,000,000599.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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