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GOE 457 AIRFOIL (goe457-il)

GOE 457 AIRFOIL - Gottingen 457 airfoil


Airfoil goe457-il
Details Dat file Parser  
(goe457-il) GOE 457 AIRFOIL
Gottingen 457 airfoil
Max thickness 7.8% at 19.9% chord.
Max camber 4.2% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 457 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122800 0.0193400
 0.0246500 0.0302800
 0.0495100 0.0432600
 0.0744100 0.0519500
 0.0993300 0.0587300
 0.1492100 0.0693000
 0.1991400 0.0755700
 0.2990900 0.0799100
 0.3991200 0.0772500
 0.4991900 0.0706900
 0.5992800 0.0629300
 0.6994000 0.0526700
 0.7995500 0.0397100
 0.8997500 0.0217600
 0.9498600 0.0119300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0126000 -.0087600
 0.0251200 -.0102100
 0.0501200 -.0108300
 0.0751100 -.0096400
 0.1000900 -.0082600
 0.1500700 -.0058900
 0.2000300 -.0027200
 0.2999600 0.0035200
 0.3999200 0.0071600
 0.4998900 0.0096000
 0.5998900 0.0094400
 0.6999100 0.0082800
 0.7999300 0.0061200
 0.8999600 0.0033600
 0.9499800 0.0014300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 457 AIRFOIL (goe457-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe457-il50,000934.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe457-il50,000540.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe457-il100,000954.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe457-il100,000556.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe457-il200,000973.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe457-il200,000572.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe457-il500,000998.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe457-il500,000593.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe457-il1,000,0009117 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe457-il1,000,0005108.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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