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GOE 464 AIRFOIL (goe464-il)

GOE 464 AIRFOIL - Gottingen 464 airfoil


Airfoil goe464-il
Details Dat file Parser  
(goe464-il) GOE 464 AIRFOIL
Gottingen 464 airfoil
Max thickness 7.7% at 7.4% chord.
Max camber 9.9% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 464 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0335900
 0.0246600 0.0486700
 0.0495300 0.0678500
 0.0744300 0.0815200
 0.0993600 0.0917000
 0.1492600 0.1060400
 0.1991900 0.1153900
 0.2991500 0.1220900
 0.3991700 0.1187900
 0.4992400 0.1089900
 0.5993400 0.0937000
 0.6994700 0.0759000
 0.7996399 0.0516000
 0.8998100 0.0268000
 0.9499000 0.0141500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125200 -.0061100
 0.0250400 -.0063200
 0.0500400 -.0051500
 0.0749700 0.0045200
 0.0998400 0.0227000
 0.1494400 0.0454700
 0.1995600 0.0629000
 0.2994700 0.0761000
 0.3994500 0.0788000
 0.4994900 0.0735000
 0.5995500 0.0637000
 0.6996500 0.0499000
 0.7997700 0.0331000
 0.8999000 0.0148000
 0.9499600 0.0056500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 464 AIRFOIL (goe464-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe464-il50,000919.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe464-il50,000537.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe464-il100,000979.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe464-il100,000556 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe464-il200,0009151.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe464-il200,000572.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe464-il500,0009164.9 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe464-il500,000597 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe464-il1,000,0009118.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe464-il1,000,0005117.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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