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GOE 448 AIRFOIL (goe448-il)

GOE 448 AIRFOIL - Gottingen 448 airfoil


Airfoil goe448-il
Details Dat file Parser  
(goe448-il) GOE 448 AIRFOIL
Gottingen 448 airfoil
Max thickness 12.9% at 29.8% chord.
Max camber 10.5% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 448 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121100 0.0265800
 0.0243800 0.0425500
 0.0490300 0.0672100
 0.0737600 0.0855700
 0.0985300 0.1012300
 0.1482000 0.1240500
 0.1979400 0.1421700
 0.2976400 0.1626200
 0.3975500 0.1688600
 0.4976400 0.1629200
 0.5978800 0.1458700
 0.6982700 0.1194200
 0.7987600 0.0854800
 0.8993400 0.0457400
 0.9496500 0.0238700
 1.0000000 0.0013000

 0.0000000 0.0000000
 0.0126700 -.0119200
 0.0252200 -.0151300
 0.0502100 -.0146700
 0.0751100 -.0078100
 0.1000400 -.0027500
 0.1498800 0.0079700
 0.1997300 0.0188000
 0.2995100 0.0339400
 0.3994000 0.0414900
 0.4993600 0.0442400
 0.5994100 0.0403900
 0.6995300 0.0323400
 0.7996700 0.0227000
 0.8998200 0.0125500
 0.9499199 0.0053700
 1.0000000 -.0013000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 448 AIRFOIL (goe448-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe448-il50,00095.4 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   goe448-il50,000511.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe448-il100,000911.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe448-il100,000537 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe448-il200,0009162 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe448-il200,000574.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe448-il500,0009119.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe448-il500,0005102.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe448-il1,000,0009137.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe448-il1,000,0005123.6 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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