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GOE 476 AIRFOIL (goe476-il)

GOE 476 AIRFOIL - Gottingen 476 airfoil


Airfoil goe476-il
Details Dat file Parser  
(goe476-il) GOE 476 AIRFOIL
Gottingen 476 airfoil
Max thickness 14.5% at 29.5% chord.
Max camber 5.2% at 39.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 476 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0113900 0.0284400
 0.0233900 0.0414100
 0.0477200 0.0583600
 0.0722000 0.0718200
 0.0967900 0.0822700
 0.1461900 0.0977000
 0.1957800 0.1081400
 0.2952600 0.1215200
 0.3952300 0.1224100
 0.4955400 0.1143300
 0.5961700 0.0982500
 0.6969500 0.0781800
 0.7978700 0.0546200
 0.8988700 0.0290600
 0.9494100 0.0150300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0133800 -.0224800
 0.0261700 -.0299800
 0.0513800 -.0355000
 0.0764400 -.0370200
 0.1014500 -.0370400
 0.1513100 -.0336000
 0.2011600 -.0296500
 0.3008900 -.0227700
 0.4007000 -.0178700
 0.5005300 -.0134800
 0.6004300 -.0110800
 0.7003601 -.0091900
 0.8003399 -.0087900
 0.9002301 -.0058900
 0.9501300 -.0034400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 476 AIRFOIL (goe476-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe476-il50,00096.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe476-il50,000518.1 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe476-il100,000944.8 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe476-il100,000549.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe476-il200,000975.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe476-il200,000574.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe476-il500,0009108.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe476-il500,0005101.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe476-il1,000,0009132.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe476-il1,000,0005116.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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